Book of Abstracts - GAMM 2012 - Technische Universität Darmstadt
Book of Abstracts - GAMM 2012 - Technische Universität Darmstadt
Book of Abstracts - GAMM 2012 - Technische Universität Darmstadt
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83rd Annual Scientific Conference <strong>of</strong> the International<br />
Association <strong>of</strong> Applied Mathematics and Mechanics<br />
<strong>Book</strong> <strong>of</strong> <strong>Abstracts</strong><br />
Version for use on a standalone computer<br />
<strong>Technische</strong> <strong>Universität</strong> <strong>Darmstadt</strong><br />
March 26 – 30, <strong>2012</strong><br />
Hans-Dieter Alber Cameron Tropea<br />
Unter Mitwirkung von<br />
Anke Böttcher, Dieter Bothe, Petra Fuhrmann, Peter Hagedorn, Christiane Herdler,<br />
Carsten Juretzka, Natalia Kraynyukova, Richard Markert, Anke Meier-Dörnberg,<br />
Birgit Neuthe, Martin Oberlack, Stefan Ulbrich, Nicole Wagner
Prandtl Lecture 3<br />
Prandtl Lecture<br />
Ludwig-Prandtl-Gedächtnisvorlesung Mon, 13:30–14:30<br />
Chair: Cameron Tropea dmstm–spectrum, plenary lectures<br />
Aero-Struktur-Dynamik großer Flugzeugtragflügel in schallnaher Strömung<br />
Josef Ballmann (RWTH Aachen) Schedule<br />
Das Strömungsfeld über den Tragflügeln großer Passagierflugzeuge, die mit der Machzahl Ma=0,8<br />
bis 0,85, d. h. mit 80 bis 85 % der Geschwindigkeit des Schalls in der umgebenden Luft, fliegen,<br />
ist durch lokale Überschallgebiete gekennzeichnet, die stromab durch Verdichtungsstöße abgeschlossen<br />
sind. Diese Stöße beschleunigen große Luftmengen, die sich bei Windstille ursprünglich<br />
in Ruhe befanden, in Flugrichtung und verursachen den sogenannten Wellenwiderstand, der den<br />
neben der Reibung in den Strömungsgrenzschichten der Luft an der Flugzeugoberfläche den wichtigsten<br />
Anteil des Gesamtwiderstandes und damit des Brennst<strong>of</strong>fverbrauchs im Reiseflug bildet.<br />
In dem Bestreben, diesen Widerstandsanteil durch Verminderung der Stärke der am Ende eines<br />
Überschallgebietes unvermeidlichen Stöße zu minimieren, wurden sogenannte überkritische<br />
Pr<strong>of</strong>ile der Tragflächen entwickelt, die auf der Oberseite einen großen Bereich mit nur schwacher<br />
konvexer Krümmung aufweisen und sehr dünn sind. Je schlanker aber die Pr<strong>of</strong>ile und je größer die<br />
Spannweiten der Flügel sind, desto wichtiger wird es aus Sicherheitsgründen und zur Erzielung<br />
eines wirklichkeitsnahen aerodynamischen Optimums, die Verformungen der Tragflügel im Flug<br />
schon in den aerodynamischen Entwurf einzubeziehen. Gleichzeitig gilt es, zeitabhängige dynamische<br />
Wechselwirkungen zwischen Strömungs- und Strukturkräften, etwa durch Böeneinwirkung<br />
oder Strukturschwingungen, im katastrophalen Fall Flattern oder, stark das Material ermüdend,<br />
Grenzzyklusschwingungen, schon in der Entwurfsvorhersage zu beherrschen und auszuschließen,<br />
sodass die Sicherheit und der Reisekomfort der Passagiere über eine lange Lebensdauer des Flugzeugs<br />
jederzeit gewährleistet bleiben.<br />
Die außer der Machzahl für experimentelle und rechnerische Vorhersagen wichtigste Strömungskennzahl<br />
ist die Reynoldszahl, die als Quotient aus dem Produkt der Fluggeschwindigkeit<br />
mit einer charakteristischen Abmessung des Flugzeugs dividiert durch die dynamische Viskosität<br />
des Strömungsmediums definiert ist und bei Großraumflugzeugen Werte von bis zu Re = 80 · 106<br />
erreicht. In Windkanälen für Modelle im verkleinerten Maßstab, etwa 1:30 bei „großen“ Modellen,<br />
ist das Erreichen solcher Werte nur möglich, indem man die dynamische Zähigkeit des Gases<br />
entsprechend herabsetzt. Das gelingt mit Stickst<strong>of</strong>f als Testgas durch Herunterkühlen auf minus<br />
150 o C und Erhöhen des Drucks im Windkanal auf 4 bar. Das sind auch für Versuchsmodelle sehr<br />
unwirtliche Bedingungen. Auf der Welt existieren seit jetzt etwa 20 Jahren zwei Windkanäle, in<br />
denen diese Bedingungen möglich sind, der „European Transonic Windtunnel“ (ETW) in Europa<br />
und der NTF („National Transonic Facility“) in den USA. Im Vortrag werden die Entwicklungen<br />
der theoretisch-numerischen und experimentellen Methoden der Aeroelastik seit Prandtl bis heute<br />
kurz gestreift. Vertiefter eingegangen wird auf die an der RWTH Aachen in den letzten Jahren<br />
vorangetriebenen Methodenentwicklungen für die numerische Lösung aero-struktur-dynamischer<br />
Probleme der Luftfahrt mithilfe algebraisch gekoppelter Finite-Volumen-Verfahren für das Strömungsfeld<br />
und Finite-Elemente-Methoden für die umströmte Struktur sowie die Anstrengungen<br />
zur Gewinnung aero-struktur-dynamischer Windkanaldaten im ETW bei realen Mach- und<br />
Reynoldszahlen, die zu einem Teil inzwischen zur weltweiten Nutzung für die Überprüfung numerischer<br />
Methoden für die schallnahe Aero-Struktur-Dynamik bereit gestellt wurden. In einer<br />
nach dem Vorbild der Reihe „Drag Prediction Workshop“ (DPW) unter dem Dach des AIAA neu<br />
gegründeten Reihe mit dem Titel „Aero-elastic Prediction Workshop“ (AePW) gehören sie zu den<br />
wichtigsten ersten Testfällen.
4 Plenary Lectures<br />
Plenary Lectures<br />
Plenary Lecture 1 Mon, 14:30–15:30<br />
Chair: Christian Wieners dmstm–spectrum, plenary lectures<br />
Preconditioning for PDE-constrained optimization<br />
Andy Wathen (University <strong>of</strong> Oxford) Schedule<br />
Many control problems for PDEs can be expressed as Optimization problems with the relevant<br />
PDEs acting as constraints. As is being discovered in other areas such as multi-physics, there<br />
seem to be distinct advantages to tackling such constrained Optimization problems ‘all-at-once’<br />
or with a ‘one-shot’ method. That is, decoupling <strong>of</strong> the overall problem in some loosely coupled<br />
iterative fashion appears to be a rather poorer approach than to compute on the fully coupled<br />
problem.<br />
The use <strong>of</strong> iterative methods for the relevant linear algebra is crucial here since the overall<br />
dimensions (including the Optimization and PDE) are usually very large, but matrix vector<br />
products as required in Krylov subspace methods such as MINRES are still readily computed.<br />
The work to ensure rapid convergence is in preconditioning and it is this topic that we will mostly<br />
focus on in this lecture.<br />
We will describe our general approach via block preconditioning and demonstrate its use for<br />
the control <strong>of</strong> Poisson and Stokes problems and also for the fully time-dependent heat equations.<br />
This is joint work with Tyrone Rees, Martin Stoll, Sue Thorne and John Pearson.<br />
Plenary Lecture 2 Tue, 08:30–09:30<br />
Chair: Peter Hagedorn dmstm–spectrum, plenary lectures<br />
From direct to inverse analysis in flexible multibody dynamics<br />
Olivier Brüls (University <strong>of</strong> Liège) Schedule<br />
Today, state-<strong>of</strong>-the-art simulation packages in flexible multibody dynamics allow the high-fidelity<br />
analysis <strong>of</strong> industrial mechanisms and machines in many application fields including robotics,<br />
automotive systems, aeronautics, deployable structures or wind turbines. The dynamic response<br />
<strong>of</strong> a given system can thus be evaluated in the time-domain for given load cases and given initial<br />
values. However, in many practical cases, the engineer does not have a precise knowledge <strong>of</strong> the<br />
mechanical design, the loading conditions and the initial state. This situation occurs for example<br />
in structural optimization, optimal control, experimental identification and health monitoring<br />
problems. The complexity <strong>of</strong> simulation codes and the computational cost <strong>of</strong> high-fidelity models<br />
are still important obstacles for the development <strong>of</strong> efficient resolution methods for these inverse<br />
problems. A current challenge is thus to elaborate simplified and more efficient modelling strategies<br />
in flexible multibody dynamics in order to enable the development <strong>of</strong> inverse analysis methods.<br />
The talk is divided into three parts. The first part provides an overview <strong>of</strong> available simulation<br />
techniques for flexible mechanisms with a particular emphasis on finite element-based approaches<br />
and time integration methods. Some illustrations are presented in the fields <strong>of</strong> deployable structures,<br />
vehicle dynamics and wind turbines. In the second part, optimization problems in flexible<br />
multibody dynamics are addressed and solved using gradient-based methods. Efficient methods<br />
for sensitivity analysis are discussed and special problems are treated such as the structural optimization<br />
<strong>of</strong> mechanical components or the numerical solution <strong>of</strong> inverse dynamics problems.<br />
The third part discusses a recently-developed Lie group approach which allows the formulation <strong>of</strong><br />
the equations <strong>of</strong> motion <strong>of</strong> a multibody system in a parameterization-free setting. Based on this
Plenary Lectures 5<br />
general formalism, which is characterized by an increased modularity and a reduced complexity,<br />
a large variety <strong>of</strong> Lie group solvers are foreseen not only for time integration but also for model<br />
reduction, sensitivity analysis and optimization.<br />
Plenary Lecture 3 Wed, 08:30–09:30<br />
Chair: Richard Markert S1|01–A1<br />
Physics <strong>of</strong> Sports<br />
Christoph Clanet (École Polytechnique Paris) Schedule<br />
Physics consists in identifying repeatable sequences in our environment and finding the simplest<br />
underlying laws. In these lecture, the environment is Sport. We will walk in the footprints <strong>of</strong><br />
modern precursors, JB Keller and B.Benjamin and show that Sports do entangle a large number<br />
<strong>of</strong> physical concepts. The main domains will be football, badminton and ski jump, in which we<br />
will discuss fluid mechanics, elasticity and some statistical physics.<br />
Plenary Lecture 4 Thu, 08:30–09:30<br />
Chair: Martin Oberlack S1|01–A1<br />
Multi-Scale Model Development for LES <strong>of</strong> Practical Combustion Applications<br />
Heinz Pitsch (RWTH Aachen) Schedule<br />
Modeling combustion in technical combustion devices is challenging, because <strong>of</strong> the multi-scale<br />
character, complex geometry, flow and mixing, and the multitude <strong>of</strong> different interacting processes,<br />
including turbulence, chemistry, spray formation, spray dynamics and evaporation, radiation,<br />
and pollutant formation. Here, using the example <strong>of</strong> aircraft engine combustors, the interaction<br />
<strong>of</strong> these effects in practical combustion devices will be assessed. Direct numerical simulations and<br />
large-eddy simulations will be used to demonstrate the subtle effects <strong>of</strong> liquid fuel evaporation on<br />
small-scale flame structure and large-scale combustion behavior. Based on the knowledge from<br />
these studies, suitable combustion models have been developed. The application <strong>of</strong> the combustion<br />
models in predictions <strong>of</strong> soot and nitrogen oxide emissions from aircraft engines will be discussed.<br />
Plenary Lecture 5 Thu, 09:30–10:30<br />
Chair: Dieter Bothe S1|01–A1<br />
Infinite-dimensional port-Hamiltonian systems<br />
Birgit Jacob (<strong>Universität</strong> Wuppertal) Schedule<br />
Modeling <strong>of</strong> dynamical systems with a spatial component leads to lumped parameter systems,<br />
when the spatial component may be denied, and to distributed parameter systems otherwise.<br />
The mathematical model <strong>of</strong> distributed parameter systems will be a partial differential equation.<br />
Examples <strong>of</strong> dynamical sytems with a spatial component are, among others, temperature<br />
distribution <strong>of</strong> metal slabs or plates, and the vibration <strong>of</strong> aircraft wings.<br />
In this talk we will study distributed parameter port-Hamiltonian systems. This class contains<br />
the above mentioned examples. The norm <strong>of</strong> such a system is given by the energy (Hamiltonian)<br />
<strong>of</strong> the system. This fact enables us to show relatively easy the existence and stability <strong>of</strong> solutions.<br />
Further, it is possible to determine which boundary variables are suitable as inputs and outputs,<br />
and how the system can be stabilized via the boundary.
6 Plenary Lectures<br />
Plenary Lecture 6 Thu, 11:00–12:00<br />
Chair: Klaus Hackl S1|01–A1<br />
The critical nature <strong>of</strong> plastic flow<br />
Lev Truskinovsky (École Polytechnique Paris) Schedule<br />
Steady state plastic flows have been compared to developed turbulence because the two phenomena<br />
share the inherent complexity <strong>of</strong> particle trajectories, the scale free spatial patterns and the<br />
power law statistics <strong>of</strong> fluctuations. The origin <strong>of</strong> the apparently chaotic and at the same time<br />
highly correlated microscopic response in plasticity remains hidden behind conventional engineering<br />
theories which are based on fitting functions and therefore fail to capture intermittency. To<br />
regain access to fluctuations, we study a minimal mesoscopic model whose goal is to elucidate the<br />
origin <strong>of</strong> scale free behavior in plasticity. We limit our description to fcc type crystals and leave<br />
out both temperature and rate effects. We argue that the origin <strong>of</strong> complexity in rate independent<br />
athermal plastic flows with highly mobile dislocations is marginal stability <strong>of</strong> the underlying elastic<br />
system. Our conclusions are based on a reduction <strong>of</strong> an over-damped visco-elasticity problem<br />
for a system with a rugged elastic energy landscape to an integer valued automaton. We show<br />
that already two dimensional models are adequate for describing power law statistics <strong>of</strong> avalanches<br />
and fractal character <strong>of</strong> dislocation patterning. Most remarkably, in addition to realistic values<br />
<strong>of</strong> critical exponents, a minimal 2D model generates shape functions in scaling laws which are in<br />
agreement with observations.<br />
Plenary Lecture 7 Fri, 08:30–09:30<br />
Chair: Hans-Dieter Alber S1|01–A1<br />
Looking for the hot spot: homogenization and localization <strong>of</strong> a convection-diffusion<br />
equation in a bounded domain.<br />
Gregoire Allaire (École Polytechnique Paris) Schedule<br />
This is a joint work with I. Pankratova and A. Piatnitski. Motivated by upscaling <strong>of</strong> transport phenomena<br />
in porous media, we consider the homogenization <strong>of</strong> a non-stationary convection-diffusion<br />
equation posed in a bounded domain with periodically oscillating coefficients and homogeneous<br />
Dirichlet boundary conditions. Assuming that the convection term is large, we give the asymptotic<br />
pr<strong>of</strong>ile <strong>of</strong> the solution and determine its rate <strong>of</strong> decay. In particular, it allows us to characterize<br />
the “hot spot”, i.e., the precise asymptotic location <strong>of</strong> the solution maximum which lies close to<br />
the domain boundary and is also the point <strong>of</strong> concentration. Due to the competition between<br />
convection and diffusion the position <strong>of</strong> the “hot spot” is not always intuitive as exemplified in<br />
some numerical tests.<br />
Plenary Lecture 8 Fri, 09:30–10:30<br />
Chair: Volker Mehrmann S1|01–A1<br />
Optimal Control <strong>of</strong> High-Throughput-Screening (HTS) Systems in a Dioid Algebra<br />
Jörg Raisch (TU Berlin) Schedule<br />
High-Throughput-Screening (HTS) has become an important technology to rapidly test thousands<br />
<strong>of</strong> biochemical substances. HTS plants are fully automated systems containing a fixed set<br />
<strong>of</strong> resources performing, e.g., liquid handling, storage, reading, plate handling and incubation<br />
steps. All operations which have to be conducted to analyse one set <strong>of</strong> substances are combined<br />
in a so-called batch. In order to compare screening results, the single batch time scheme, i.e., the
Plenary Lectures 7<br />
sequence and timing <strong>of</strong> activities for one batch, is usually required to be identical for all batches.<br />
In previous work, we proposed a method to determine a globally optimal (in the sense <strong>of</strong> achieving<br />
maximal throughput) solution for the resulting scheduling problem. However, this optimal<br />
schedule is generated <strong>of</strong>f-line and can therefore not react appropriately to unforeseen disturbances<br />
and delays. To handle these in a systematic manner, we have investigated methods to enhance a<br />
given <strong>of</strong>f-line schedule by appropriate feedback. It turns out that the resulting feedback synthesis<br />
problem is (non-benevolently) nonlinear when considered in the standard algebra. However, formulating<br />
the problem in a suitable dioid algebra provides a linear representation. A dioid is an<br />
idempotent semiring, with the so-called (max,+) algebra being the most well-known example. We<br />
will discuss why a different dioid, commonly referred to as M ax<br />
in [γ, δ ], is particularly suitable to<br />
model HTS problems. We will also discuss how to analytically determine a feedback control law<br />
which will start all activities as late as possible without violating the overall aim <strong>of</strong> throughput<br />
maximisation and will therefore implement a closed-loop just-in-time policy.<br />
This is the joint work with Tom Brunsch and Laurent Hardouin.<br />
Plenary Lecture 9 Fri, 11:00–12:00<br />
Chair: Ulrich Langer S1|01–A1<br />
Exponential integrators<br />
Marlis Hochbruck (KIT) Schedule<br />
In this talk we will give an overview on the construction, analysis, implementation and application<br />
<strong>of</strong> various exponential integrators. Exponential integrators are time integration schemes, which<br />
involve the evaluation or approximation <strong>of</strong> the exponential (or related) function <strong>of</strong> a suitable<br />
matrix (e.g. the Jacobian <strong>of</strong> the differential equation). Such methods have been proposed about<br />
50 years ago but for a long time have been regarded as not practical. Significant advances on the<br />
approximation <strong>of</strong> the product <strong>of</strong> a matrix function with a vector during the last decade including<br />
multiple time stepping approaches have renewed the interest in these integrators. By now it has<br />
been shown that such integrators are competitive or even outperform state <strong>of</strong> the art standard<br />
methods in certain applications.<br />
We will discuss basic ideas to construct such integrators for different applications and we<br />
will explain some convergence results for abstract partial differential equations. Moreover, we<br />
consider the approximation <strong>of</strong> matrix functions and show how these methods can be implemented<br />
in problems arising in optics and photonics.<br />
Plenary Lecture 10 Fri, 12:00–13:00<br />
Chair: Sergio Conti S1|01–A1<br />
Microstructure and effective behavior <strong>of</strong> materials<br />
Georg Dolzmann (<strong>Universität</strong> Regensburg) Schedule<br />
The importance <strong>of</strong> fine structures in solids on their elastic and plastic behavior has been recognized<br />
for a long time. Their explicit resolution, for example in numerical simulations, is a challenging<br />
problem and has inspired the search for macroscopic models which predict the overall behavior<br />
<strong>of</strong> the material without resolving all the fine scales explicitly.<br />
From the mathematical point <strong>of</strong> view, this question is usually addressed by seeking effective<br />
models in the framework <strong>of</strong> nonlinear elasticity theory based on modern methods in the calculus<br />
<strong>of</strong> variations. The scope <strong>of</strong> this presentation is to give an overview <strong>of</strong> the appropriate methods<br />
and to illustrate them for two specific model systems, namely for the elastic response <strong>of</strong> nematic
8 Plenary Lectures<br />
elastomers and the elasto-plastic behavior <strong>of</strong> single crystals.
Minisymposia MA1 – MA3 9<br />
Minisymposia MA1 – MA3<br />
Mini-MA1: Preconditioning in optimization with PDE constraints<br />
Organizers: Martin Stoll (MPI Magdeburg) Mon, 16:00–18:00<br />
Walter Zulehner (Johannes Kepler <strong>Universität</strong> Linz) dmstm–dynamicum 0.04<br />
On the preconditioning <strong>of</strong> PDE constrained shape optimization problems<br />
Volker Schulz (<strong>Universität</strong> Trier), Stephan Schmidt (Imperial College), Roland St<strong>of</strong>fel (<strong>Universität</strong><br />
Trier) Schedule<br />
Shape optimization is an aspect <strong>of</strong> optimization which is rich <strong>of</strong> applications but also requires<br />
special techniques, since global parameterizations are only viable in very restricted cases. In this<br />
talk preconditioning in two aspects will be considered: on the level <strong>of</strong> the shape Hessian as well as<br />
on the PDE level. Recent approaches are discussed and their efficacy is demonstrated for practical<br />
industrial applications.<br />
Fast Iterative Solvers for Time-Dependent PDE-Constrained Optimization Problems<br />
John Pearson (Oxford University), Martin Stoll (MPI Magdeburg), Andy Wathen (Oxford University)<br />
Schedule<br />
An area <strong>of</strong> much recent attention in applied mathematics and numerical analysis is the numerical<br />
solution <strong>of</strong> optimal control problems. In this talk, we consider in particular iterative methods for<br />
solving matrix systems resulting from time-dependent PDE-constrained optimization problems.<br />
We motivate and derive the preconditioners used, crucial to the development <strong>of</strong> which are saddle<br />
point theory, mass matrix approximation, and good approximation <strong>of</strong> the Schur complements <strong>of</strong><br />
the matrix systems we are solving. We present numerical results to demonstrate that our preconditioners<br />
yield convergence <strong>of</strong> the appropriate iterative method in few iterations for a number<br />
<strong>of</strong> problems, while only requiring the storage <strong>of</strong> matrices which are small in comparison to the<br />
matrix systems being solved.<br />
On the Preconditioning <strong>of</strong> Linear Systems Arising in Trust-Region Methods<br />
Roland Herzog, Susann Mach (TU Chemnitz) Schedule<br />
Trust-region methods are widely used for the numerical solution <strong>of</strong> nonlinear constrained and unconstrained<br />
optimization problems. Similar as line-search methods, they take turns in minimizing<br />
local models <strong>of</strong> the objective. In contrast to line-search methods, however, trust-region approaches<br />
do not require nor promote the positive definiteness <strong>of</strong> the local Hessian approximations.<br />
In this presentation, we address issues arising in the context <strong>of</strong> the preconditioned approximate<br />
solution <strong>of</strong> these local models. The talk will highlight connections between algorithmic<br />
optimization and linear algebra.<br />
A multigrid framework applied to an elliptic optimal control problem with reduced<br />
regularity<br />
Stefan Takacs, Walter Zulehner (<strong>Universität</strong> Linz) Schedule<br />
In this talk we consider the convergence theory for all-at-once multigrid methods for solving<br />
saddle point problems, like the optimality system <strong>of</strong> a PDE-constrained optimization problem. For<br />
general linear systems we identify four sufficient conditions for convergence. The analysis follows<br />
classical lines. The result may be an essential help if a parameter-dependent problem is considered,<br />
because the fact that the four sufficient conditions are satisfied with constants independent <strong>of</strong> the
10 Minisymposia MA1 – MA3<br />
parameters implies that also the bounds for the convergence rates are parameter-independent.<br />
We apply this theory to an elliptic optimal control model problem <strong>of</strong> tracking type. The new<br />
approach allows to extend previously known convergence results based on full elliptic regularity<br />
to problems with reduced regularity.<br />
Indefinite Preconditioners for PDE-constrained optimization problems<br />
Valeria Simoncini (Universita’ di Bologna) Schedule<br />
Symmetric indefinite preconditioners are being more and more employed for the efficient solution<br />
<strong>of</strong> saddle point algebraic linear systems in PDE-constrained optimization problems. In this talk<br />
we review some recent numerical and theoretical aspects that make indefinite preconditioners<br />
appealing over symmetric positive definite acceleration strategies.<br />
Preconditioning for PDE-constrained optimization using proper orthogonal decomposition<br />
Ekkehard W. Sachs, Xuancan Ye (<strong>Universität</strong> Trier) Schedule<br />
The main effort <strong>of</strong> solving a PDE constrained optimization problem is devoted to solving the<br />
corresponding large scale linear system, which is usually sparse and ill conditioned. As a result,<br />
a suitable Krylov subspace solver is favourable, if a proper preconditioner is embedded. Other<br />
than the commonly used block preconditioners, we exploit knowledge <strong>of</strong> proper orthogonal decomposition<br />
(POD) for preconditioning and achieve some interesting features. Numerical results<br />
on nonlinear test problems are presented.<br />
Mini-MA2: High-performance linear algebra on GPUs<br />
Organizers: Paolo Bientinesi (RWTH Aachen) Mon, 16:00–18:00<br />
Enrique S. Quintana-Orti (University Jaume I) dmstm–germanium2 3.02/03<br />
The implications <strong>of</strong> GPUs for parallel numerical simulation<br />
Jan-Philipp Weiss (KIT) Schedule<br />
Fast and accurate numerical simulation based on linear algebra operations relies on both efficient<br />
parallel schemes and platform-optimized parallel implementations. Due to the paradigm shift towards<br />
manycore technologies, as exemplified by GPUs, both aspects have become more intricate.<br />
Parallelism needs to be increasingly more fine-grained and has to be expressed across several system<br />
levels. Moreover, exploitation <strong>of</strong> data locality in hierarchically organized memory subsystems<br />
as well as data layout and memory access patterns are performance-critical factors.<br />
This talk details the configuration <strong>of</strong> modern GPU hardware and points out how specific capabilities<br />
<strong>of</strong> GPUs can be expressed in the application mapping procedure by related programming<br />
models. We investigate the implications <strong>of</strong> hardware-aware computing on the design and adaptation<br />
<strong>of</strong> parallel numerical methods. Furthermore, we describe an approach that takes the burden<br />
<strong>of</strong> explicit hardware knowledge from the application programmer and allows writing generic, portable<br />
and high-performance numerical solvers.<br />
Preconditioned Block-Iterative Methods on GPUs<br />
Maxim Naumov (NVIDIA) Schedule<br />
In this presentation we focus on parallel algorithms that are building blocks for the incomplete-LU<br />
preconditioned block-iterative methods on Graphics Processing Units (GPUs). In particular, we<br />
focus on the techniques and the associated trade<strong>of</strong>fs used to implement sparse matrix-vector multiplication<br />
with multiple vectors and sparse triangular solve with multiple right-hand-sides using
Minisymposia MA1 – MA3 11<br />
the CUDA parallel programming model. Finally, numerical experiments comparing the GPU and<br />
CPU implementations are also presented.<br />
Parallel Preconditioners for GPU-Multigrid Solvers<br />
Robert Strzodka (NVIDIA) Schedule<br />
GPUs perform best on regular, independent work-loads while effective preconditioners ask for<br />
complex, serially coupled computations. The extreme cases <strong>of</strong> best hardware performance on<br />
slowly converging numerical schemes or quickly converging schemes with slow serial execution are<br />
poor choices. The talk discusses how to find the middle ground by challenging the hardware with<br />
more complex data dependencies and at the same time relaxing purely serial dependencies with<br />
parallel variants. For structured matrices, we can now solve very ill-conditioned linear equation<br />
systems that were intractable with GPU hardware before.<br />
The nonequispaced FFT on graphics processing units<br />
Susanne Kunis (<strong>Universität</strong> Osnabrück) Schedule<br />
Without doubt, the fast Fourier transform (FFT) belongs to the algorithms with large impact<br />
on science and engineering. By appropriate approximations, this scheme has been generalized for<br />
arbitrary spatial sampling points. This so called nonequispaced FFT is the core <strong>of</strong> the sequential<br />
NFFT3 library and we discuss which its computational costs in detail. On the other hand, programmable<br />
graphic processor units have evolved into highly parallel, multithreaded, manycore<br />
processors with enormous computational capacity and very high memory bandwith. By means <strong>of</strong><br />
the so called Compute Unified Device Architecture (CUDA), we parallelized the nonequispaced<br />
FFT using the CUDA FFT library and a dedicated parallelization <strong>of</strong> the approximation scheme.<br />
Mini-MA3: Crystals and defects<br />
Organizers: Patrick Dondl (Durham University) Mon, 16:00–18:00<br />
Bernd Schmidt (<strong>Universität</strong> Augsburg) dmstm–helium2 3.08/09<br />
Ginzburg Landau energies for dislocations<br />
Marcello Ponsiglione (La Sapienza, Roma) Schedule<br />
In this talk I will present some variational approaches to dislocations. The purpose is to derive<br />
macroscopic Ginzburg Landau energies starting from basic discrete (or microscopic) dislocation<br />
models.<br />
Twinned martensite configurations arising as ground states <strong>of</strong> a two-well discrete<br />
Hamiltonian<br />
Georgy Kitavtsev (MPI Leipzig), Stephan Luckhaus (<strong>Universität</strong> Leipzig) Schedule<br />
In this talk we construct and analyze a two-well Hamiltonian on 2D atomic lattice considered<br />
with nonconvex interactions. Two wells <strong>of</strong> the Hamiltonian are given by two rank-one connected<br />
martensitic twins, respectively. Our combined analytical and numerical results show that the<br />
structure <strong>of</strong> ground states under appropriate boundary conditions is close to the macroscopically<br />
expected twinned configuration plus additional exponential boundary layers localized near the<br />
twinning interface.
12 Minisymposia MA1 – MA3<br />
A Force-based Hybrid Method for Solids: Theory and Numerics<br />
Pingbing Ming (Institute <strong>of</strong> Computational Mathematics and Scientific/Engineering, AMSS, Chinese<br />
Academy <strong>of</strong> Sciences), Jianfeng Lu (Courant Institute New York), Zhijian Yang (Wuhan<br />
University) Schedule<br />
We study a force-based hybrid method that couples atomistic model with Cauchy-Born elasticity<br />
model. We show the proposed scheme converges to the solution <strong>of</strong> the atomistic model with second<br />
order accuracy, as the ratio between lattice parameter and the characteristic length scale <strong>of</strong> the<br />
deformation tends to zero. Convergence is established for general finite range atomistic potential<br />
and simple lattices in three dimension. The pro<strong>of</strong> is based on consistency and stability analysis.<br />
General tools for stability analysis are developed in the framework <strong>of</strong> pseudo-difference operators.<br />
Some numerical examples will also be reported.<br />
Line-tension model as the Γ-limit <strong>of</strong> a nonlinear dislocation energy<br />
Caterina Ida Zeppieri (<strong>Universität</strong> Bonn), Lucia Scardia (TU Eindhoven) Schedule<br />
The motion <strong>of</strong> dislocations is regarded as the main cause <strong>of</strong> plastic deformations, therefore a<br />
large literature is focused on the problem <strong>of</strong> deriving plasticity models from more fundamental<br />
dislocation models. The starting point <strong>of</strong> our derivation is a semi-discrete dislocation model. The<br />
main novelty <strong>of</strong> our approach is that we consider a nonlinear dislocation energy, whereas most<br />
mathematical and engineering models are based on quadratic energies. Our choice <strong>of</strong> a nonlinear<br />
stress-strain relation guarantees that the dislocation strain energy is well defined also in the<br />
vicinity <strong>of</strong> the dislocations, eliminating the need <strong>of</strong> introducing a fictitious cut-<strong>of</strong>f radius that is<br />
typical <strong>of</strong> the linear theories. The Γ-limit <strong>of</strong> our nonlinear dislocation energy as the length <strong>of</strong> the<br />
Burgers vector tends to zero is a strain-gradient model for plasticity and has the same form as<br />
the limit energy obtained by starting from a quadratic dislocation energy. Our result, however, is<br />
obtained by starting from a more reliable physical model.
Minisymposia ME1 – ME3 13<br />
Minisymposia ME1 – ME3<br />
Mini-ME1: Homogenization from submicro to micro scales<br />
Organizers: Franz Rammerstorfer (TU Wien) Mon, 16:00–18:00<br />
Bob Svendsen (RWTH Aachen) dmstm–platinum2 2.07/08<br />
Variational Homogenization <strong>of</strong> Microstructures for Gradient-Extended Dissipative<br />
Materials with Length Scales<br />
Christian Miehe, Dominic Zäh (<strong>Universität</strong> Stuttgart) Schedule<br />
The homogenization-based scale bridging is the key ingredient <strong>of</strong> modern multiscale modeling<br />
techniques. When bridging submicro to micro scales, non-standard modeling techniques must be<br />
taken into account which account for discrete length scales. At a homogenized level, these length<br />
scales can <strong>of</strong>ten be modeled by gradient-extended dissipative continua. Typical examples are<br />
theories <strong>of</strong> strain gradient plasticity, gradient damage, phase field models <strong>of</strong> fracture and phase<br />
transformations, as well as electric polarization and magnetization in functional materials. A generic<br />
theoretical and computational approach to these problems can be constructed in an elegant<br />
format based on rate-type variational principles. This lecture provides an overview <strong>of</strong> the formulation<br />
and computational exploitation <strong>of</strong> canonical variational principles for the homogenization<br />
<strong>of</strong> gradient-extended dissipative solids. It develops rate-type and incremental minimization and<br />
saddle point principles for a class <strong>of</strong> materials which incorporate order parameter fields, whose<br />
gradients enter the energy storage and dissipation functions. In contrast to classical local continuum<br />
approaches based on locally evolving internal variables, these global parameter fields are<br />
governed by additional balance-type partial differential equations including boundary conditions.<br />
We outline a unified framework for the homogenization <strong>of</strong> first-order gradient-type standard dissipative<br />
solids. Particular emphasis is put on mixed multi-field representations, where both the<br />
order parameter fields itself as well as their dual driving force are present. These mixed variational<br />
settings are suitable for models with threshold- or yield-functions formulated in the space<br />
<strong>of</strong> driving forces. It is shown that the coupled field equations follow in a natural way as the Euler<br />
equations <strong>of</strong> minimization and saddle point principles, which are based on properly defined<br />
rate-type and incremental potentials. The unified character <strong>of</strong> the computational framework is<br />
demonstrated by a spectrum <strong>of</strong> model problems, which covers computational homogenization <strong>of</strong><br />
submicro models <strong>of</strong> plasticity, damage mechanics as well as phase field models <strong>of</strong> electric and<br />
magnetic domain evolution.<br />
Multiscale Modelling <strong>of</strong> Continua with Energetic Surfaces at the Microscale<br />
A. McBride, A. Javili, P. Steinmann (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
The objective <strong>of</strong> this presentation is to detail an application <strong>of</strong> the computational micro-to-macro<br />
transition framework that involves the surface energy theory <strong>of</strong> Gurtin and Murdoch. For this<br />
application, the microstructure contains voids with additional surface energy. The response <strong>of</strong><br />
the associated macrostructure is approximated using classical elasticity theory. Homogenisation<br />
provides a consistent methodology to link the macroscopic and microscopic scales.<br />
The motivation for endowing the surface <strong>of</strong> the voids at the microscale with their own structure<br />
is to capture the well-documented effect whereby the surface plays an ever-increasing role in<br />
the overall macroscopic response as the size <strong>of</strong> the voids decrease. Our key contribution is the<br />
numerical determination <strong>of</strong> the effective macroscopic material properties as a function <strong>of</strong> both the<br />
microscopic void size and the coupling between the microscopic bulk and surface free energies. At<br />
the microscopic scale we have a continuum with a surface structure and the constitutive laws are
14 Minisymposia ME1 – ME3<br />
presumed known. At the macroscopic scale the constitutive relations are not explicitly known;<br />
they are replaced by the results <strong>of</strong> the computations on the microscopic scale using numerical<br />
homogenisation.<br />
Key features <strong>of</strong> the application are demonstrated via a series <strong>of</strong> numerical computations using<br />
the finite element method. An interesting outcome <strong>of</strong> endowing the microstructure with one or<br />
more energetic surfaces is that the response <strong>of</strong> one microstructure relative to another is dependent<br />
on the ratio <strong>of</strong> the area <strong>of</strong> the energetic surfaces to the volume <strong>of</strong> the bulk. Thus, the microscopic<br />
response is inherently scale dependent.<br />
From Nano to Micro - Perspectives for Homogenization in Crystalline Solids<br />
J. Schröder, B. Eidel, D. Balzani, D. Brands (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
For the direct incorporation <strong>of</strong> micromechanical information into macroscopic boundary value<br />
problems, the FE 2 -method provides a suitable numerical framework. Here, an additional microscopic<br />
boundary value problem, based on evaluations <strong>of</strong> representative volume elements (RVEs),<br />
is attached to the quadrature points <strong>of</strong> the discretized macrostructure. However, relevant macroscopic<br />
problems can only be simulated if simplified microstructures are used. One approach is to<br />
construct statistically similar RVEs by minimizing least-square functionals that take into account<br />
statistical measures describing the microstructure. An application <strong>of</strong> this concept for the scale<br />
transition from nano to micro is different from micro-macro transitions, since atomistics differs<br />
from continuum mechanics in various physical aspects. Atomistic models reflect the discreteness <strong>of</strong><br />
matter, atomic interactions are nonlocal and they are concepts <strong>of</strong> energies and forces. Continuum<br />
mechanics, in contrast, considers matter as a continuum, constitutive models are typically local<br />
theories and they are a very concept <strong>of</strong> stress. Moreover, an adequate RVE for nanostructures<br />
must account for inelastic defects like dislocations, stacking faults, voids etc. in fully atomistic<br />
resolution along with highly accurate interatomic potentials. In continuum mechanics however,<br />
suchlike defects and their evolution are modelled by internal variables based on rate equations.<br />
The talk adresses perspectives for the computational homogenization <strong>of</strong> heterogeneities at submicron<br />
to micron length scales and discusses aspects to consolidate the differences in atomistics<br />
and continuum mechanics.<br />
Theoretical Aspects <strong>of</strong> a Continuum Dislocation Microplasticity Theory and Numerical<br />
Examples<br />
Thomas Böhlke, Stephan Wulfingh<strong>of</strong>f (KIT) Schedule<br />
Modern continuum approaches for microplasticity applications try to fill the gap between sizeindependent,<br />
phenomenological plasticity models for macroscopic simulations and microplasticity<br />
models based on discrete objects like ab-initio methods or Discrete Dislocation Dynamics. Besides<br />
phenomenological strain gradient plasticity models several dislocation density-based theories have<br />
emerged that account explicitly for dislocation transport and production. The kinematical theory<br />
<strong>of</strong> Hochrainer et al. [1], numerically implemented by Sandfeld et al. [2], averages the collective<br />
motion <strong>of</strong> three-dimensional discrete, connected and curved dislocation lines. The theory can be<br />
considered as a generalization <strong>of</strong> Nye’s work [4]. Besides Geometrically Necessary Dislocations<br />
it contains additional detailed information on the dislocation microstructure. As the theory is<br />
numerically expensive in three-dimensional multislip applications, a simplified version (see e.g.<br />
Sandfeld et al. [3]) <strong>of</strong> the kinematical continuum mechanical dislocation-density framework is<br />
considered in the presentation based on two evolution equations for the dislocation density ρt<br />
and the average dislocation curvature ¯ k. The dislocation velocity ν couples the dislocation field<br />
problem to the elasto-visco-plastic crystal plasticity framework via Orowan’s equation ˙γ = ρtbν,
Minisymposia ME1 – ME3 15<br />
where γ is the plastic slip. Furthermore, the kinetic coupling based on hardening approaches like<br />
the Taylor-relation τY ∼ √ ρt as well as boundary conditions are discussed. Three-dimensional<br />
model problems highlight the advantages <strong>of</strong> the dislocation based approach.<br />
[1] T. Hochrainer, M. Zaiser and P. Gumbsch, A three-dimensional continuum theory <strong>of</strong> dislocations:<br />
kinematics and mean field formulation. Philosophical Magazine 87 (2007), 1261–1282.<br />
[2] S. Sandfeld, T. Hochrainer, M. Zaiser and P. Gumbsch, Numerical implementation <strong>of</strong> a 3D<br />
continuum theory <strong>of</strong> dislocation dynamics and application to micro-bending, Philosophical<br />
Magazine 90 (2010), 3697–3728.<br />
[3] S. Sandfeld, T. Hochrainer, M. Zaiser and P. Gumbsch, Continuum modeling <strong>of</strong> dislocation<br />
plasticity: Theory, numerical implementation, and validation by discrete dislocation<br />
simulations. J. Mater. Res. 26 (2011), 623–632.<br />
[4] J. F. Nye, Some geometrical relations in dislocated crystals. Acta Metallurgica 1 (1953),<br />
153–162.<br />
On non-local and semi-discrete generalizations <strong>of</strong> continuum dislocation field theory<br />
Bob Svendsen (RWTH Aachen) Schedule<br />
Like standard continuum plasticity theory, the Volterra or continuum theory <strong>of</strong> dislocations based<br />
on linear elasticity theory is devoid <strong>of</strong> any material lengthscale or regard for the atomic structure<br />
<strong>of</strong> the material. In particular, it is well-known (e.g., [1]) that the model breaks down near the<br />
dislocation core, something which can also be related to the fact that the model has no material<br />
lengthscale. Among other things, this has led a number <strong>of</strong> workers to propose generalizations <strong>of</strong><br />
this approach in which different types <strong>of</strong> lengthscales play a role. In particular, these include (i)<br />
couple-stress elasticity, (ii) non-local elasticity, and (iii) semi-discrete approaches, e.g., the Peierls-<br />
Nabarro model. Whereas the first two are, like the Volterra model itself, purely phenomenological<br />
in nature, semi-discrete methods like the Peierls-Nabarro model <strong>of</strong>fer the chance <strong>of</strong> scale-bridging<br />
with atomistic models for dislocations. Besides a comparison <strong>of</strong> the core regularization <strong>of</strong>fered by<br />
these approaches, the purpose <strong>of</strong> the current work is to show in detail how the Volterra model<br />
represents the asymptotic limit <strong>of</strong> the Peierls-Nabarro model as the core size is allowed to vanish.<br />
In addition, the connection <strong>of</strong> the Peierls-Nabarro model with lattice models such as Frenkel-<br />
Kontorova will be examined.<br />
[1] J. P. Hirth, J. Lothe, Theory <strong>of</strong> Dislocations, 2 nd edition (1982), Wiley.<br />
Mini-ME2: Micro- and nan<strong>of</strong>luidics<br />
Organizers: Stephan Gekle (TU München) Mon, 16:00–18:00<br />
Steffen Hardt (TU <strong>Darmstadt</strong>) dmstm–spectrum<br />
Nanoscale pumping <strong>of</strong> water by AC electric fields<br />
Klaus Rinne (FU Berlin), Stephan Gekle, Douwe Jan Bonthuis (TU München), Roland Netz (FU<br />
Berlin) Schedule<br />
Using molecular dynamics simulations we present a novel mechanism for pumping <strong>of</strong> water through<br />
a carbon nanotube by time-dependent electric fields. The fields are generated by electrodes with<br />
oscillating charges in a broad GHz frequency range which are attached laterally to the tube.
16 Minisymposia ME1 – ME3<br />
The key ingredient is a phase shift between the electrodes to break the spatio-temporal symmetry.<br />
A microscopic theory based on a polarization-dragging mechanism accounts quantitatively for<br />
our numerical findings.<br />
Blood Flow through Microchannels: From Single Cells to Blood Rheology<br />
Gerhard Gompper (Forschungszentrum Jülich) Schedule<br />
The flow behavior <strong>of</strong> vesicles and blood cells is important in many applications in biology and medicine.<br />
For example, the flow properties <strong>of</strong> blood in micro-vessels is determined by the mechanical<br />
properties <strong>of</strong> red blood cells (RBCs). Blood flow is therefore strongly affected by diseases such<br />
as malaria or diabetes, where RBC deformability is strongly reduced. Furthermore, micr<strong>of</strong>luidic<br />
devices nowadays allow the manipulation <strong>of</strong> small amounts <strong>of</strong> suspensions <strong>of</strong> particles or cells.<br />
Of fundamental interest is here the relation between the flow behavior and the deformability<br />
<strong>of</strong> the blood cells, their long-range hydrodynamic interactions in microchannels, and thermal<br />
membrane undulations. We study these mechanisms in a model, which combines particle-based<br />
mesoscale simulation techniques [1] for the fluid hydrodynamics with a triangulated-surface model<br />
[2] for the membrane. The essential control parameters are the volume fraction <strong>of</strong> RBCs (tube<br />
hematocrit) and the flow velocity.<br />
In narrow channels, single RBCs in capillary flow show a transition from biconcave-disk to<br />
parachute shape with increasing flow velocity [3]. At higher volume fractions, hydrodynamic interactions<br />
are responsible for a strong deformation-mediated clustering tendency at low hematocrits,<br />
as well as several distinct flow phases at higher hematocrits [4]. For larger channels, blood behaves<br />
like a continuum fluid. As a function <strong>of</strong> shear rate, a strong shear-thinning behavior is<br />
found, which is predicted from RBC deformability and cell-cell attraction [5]. Recent progress in<br />
simulation techniques now also allows to study more complex systems, such as mixtures <strong>of</strong> RBCs<br />
and white blood cells (WBCs). WBCs may accumulate near the vessel walls, a process called<br />
margination. Flow conditions for WBC margination are predicted and discussed [6].<br />
[1] G. Gompper, T. Ihle, D.M. Kroll and R.G. Winkler, Adv. Polymer Sci. 221, 1–87 (2009).<br />
[2] G. Gompper and D.M. Kroll, in Statistical Mechanics <strong>of</strong> Membranes and Surfaces (2nd<br />
edition), p.359–426, edited by D. R. Nelson, T. Piran and S. Weinberg (World Scientific,<br />
Singapore, 2004).<br />
[3] H. Noguchi and G. Gompper, Proc. Natl. Acad. Sci. USA 102, 14159 (2005).<br />
[4] J.L. McWhirter, H. Noguchi, and G. Gompper, Proc. Natl. Acad. Sci. USA 106, 6039 (2009).<br />
[5] D.A. Fedosov, W. Pan, B. Caswell, G. Gompper, and G.E. Karniadakis, Proc. Natl. Acad.<br />
Sci. USA 108, 11772–11777 (2011).<br />
[6] D.A. Fedosov, J. Fornleitner, and G. Gompper, Phys. Rev. Lett., to appear (<strong>2012</strong>).<br />
Influence <strong>of</strong> the electric double layer on charged anisotropic particles <strong>of</strong> colloidal size<br />
Florian Keller, Willy Dörfler, Hermann Nirschl (KIT) Schedule<br />
Colloidal particles, i.e. particles with a size below 1 m, play an important role in chemical,<br />
biological and environmental engineering. Since particles in aqueous solutions normally carry a<br />
non-zero surface charge, an electric double layer around the particles develops. Due to an ambient<br />
fluid flow this double layer gets distorted and exerts an additional electrostatic force and torque on
Minisymposia ME1 – ME3 17<br />
the particle. Because <strong>of</strong> the large surface to volume ratio <strong>of</strong> colloids these forces and torques alter<br />
the particle motion and cannot be neglected. In this talk we will especially consider the influence<br />
<strong>of</strong> the electric double layer on anisotropic particles. As a model system we therefore use prolate<br />
spheroids. However the majority <strong>of</strong> the theoretical work available in the literature considers only<br />
spherical particles, while for spheroidal particles most works suffer from severe restrictions on<br />
the ion concentrations, Peclet numbers but also on the geometry. In the latter case, it is thereby<br />
<strong>of</strong>ten assumed the thickness <strong>of</strong> the spheroidal particle is small compared to its length. However<br />
in practical applications one <strong>of</strong>ten has to deal with non-spherical particles with moderate aspect<br />
ratios. In this talk we use direct numerical simulation to investigate the effects <strong>of</strong> the electric<br />
double layer on charged spheroidal particles with moderate aspect ratios in uniform flow fields<br />
as well as in shear flow. It is shown that the influence <strong>of</strong> the particle charge behaves in analogy<br />
to the case <strong>of</strong> charged spheres, while the influence <strong>of</strong> the double layer thickness largely deviates<br />
from these results and depends on the orientation <strong>of</strong> the spheroids. In a linear shear flow, we<br />
will further show that the motion <strong>of</strong> the spheroids can be compared to the motion <strong>of</strong> uncharged<br />
spheroids.<br />
Microjet formation in a capillary by laser-induced cavitation<br />
Ivo R. Peters, Yoshiyuki Tagawa, Nikolai Oudalov, Chao Sun, Devaraj van der Meer, Detlef Lohse<br />
(University <strong>of</strong> Twente) Schedule<br />
A vapor bubble is created by focusing a laser pulse inside a capillary that is partially filled with<br />
water. Upon creation <strong>of</strong> the bubble, a shock wave travels through the capillary. When this shock<br />
wave meets the meniscus <strong>of</strong> the air-water interface, a very thin jet is created that can reach<br />
speeds exceeding the speed <strong>of</strong> sound. A crucial ingredient is the shape <strong>of</strong> the meniscus, which is<br />
responsible for focusing the energy provided by the shock wave into a jet.<br />
We examine the formation <strong>of</strong> this jet numerically using a boundary integral method, where we<br />
prepare an initial interface at rest inside a tube with a diameter ranging from 50 to 500 µm. We<br />
apply a strong pressure pulse on the bubble with a typical duration <strong>of</strong> 50 ns, after which the jet<br />
forms. We investigate the influence <strong>of</strong> the contact angle, tube radius, distance <strong>of</strong> the bubble from<br />
the meniscus, and pressure amplitude on the jet formation. The jet shape and velocity obtained<br />
by the simulation compare well with experimental data, and provides good insight in the origin<br />
<strong>of</strong> the jet.<br />
Using potential flow theory we develop an approximate expression that accurately reproduces<br />
the dependencies on the above mentioned parameters. In particular, we show that the jet speed<br />
is proportional to the pressure amplitude, and the inverse <strong>of</strong> the distance between the bubble and<br />
the free surface. The model agrees well with experiment and simulation.<br />
Propulsion <strong>of</strong> Leidenfrost solids on structured and unstructured surfaces<br />
Tobias Baier, Stefan Herbert (TU <strong>Darmstadt</strong>), Guillaume Dupeux, David Quere (Ecole Polytechnique),<br />
Steffen Hardt (TU <strong>Darmstadt</strong>) Schedule<br />
Since the publication <strong>of</strong> the first work on self propelling Leidenfrost drops on ratchets by Linke<br />
et al. in 2007 [1] the mechanism for their propulsion has been debated. A number <strong>of</strong> reasons<br />
have been proposed, including viscous shear, net pressure forces due to the drop surface following<br />
the ratchets contour, thermocapillary flows, gradients in Laplace pressure, coupling <strong>of</strong> surface<br />
waves and droplet oscillations to the motion, recoil pressure or thermal creep flow. All or some <strong>of</strong><br />
these mechanisms may play a role for the net propulsion; however, the complexity <strong>of</strong> the problem<br />
including the liquid motion makes it hard to make quantitative predictions about the relative<br />
importance <strong>of</strong> the terms.<br />
A new spin was given to the field in [2] where the movement <strong>of</strong> platelets <strong>of</strong> dry ice levitating
18 Minisymposia ME1 – ME3<br />
over a hot structured surface was studied. Being a solid where internal degrees <strong>of</strong> freedom can<br />
be neglected, this system excludes many <strong>of</strong> the above mechanisms making it more amenable to<br />
analysis. We propose a mathematical model for the the propulsion <strong>of</strong> such Leidenfrost solids. We<br />
identify the sublimation rate by solving the energy equation between the ratchet and the ice coupled<br />
to a solution <strong>of</strong> the Navier-Stokes equation for the gas flow. We pursue this model at various<br />
states <strong>of</strong> rigor, from a numerical calculation using finite volume discretisation to a lubrication<br />
approximation. In particular, we make predictions about the scaling <strong>of</strong> the net propulsive force<br />
with the geometric parameters <strong>of</strong> the structured surface and the size <strong>of</strong> the platelet.<br />
Additionally, a novel mode <strong>of</strong> propulsion <strong>of</strong> Leidenfrost solids is proposed on non-structured<br />
surfaces. Evidently, a homogeneous cylindrical disc <strong>of</strong> dry ice in the Leidenfrost state on a flat<br />
surface will levitate without a net lateral force due to symmetry. However, breaking the symmetry<br />
by an inhomogeneous mass distribution must be compensated by a non-symmetric pressure<br />
distribution in the gas layer below the platelet, resulting in a slight tipping. This in turn results<br />
in a net lateral pressure force which together with the viscous forces leads to a net propulsion <strong>of</strong><br />
the platelet. We investigate this mechanism in our lubrication model.<br />
[1] H Linke, BJ Aleman, LD Melling, MJ Taormina, MJ Francis, CC Dow-Hygelund, V Narayanan,<br />
RP Taylor, and A Stout. Self-propelled Leidenfrost droplets. Phys.Rev.Lett. 96 (15),<br />
2006.<br />
[2] G Lagubeau, M Le Merrer, C Clanet, and D Quere. Leidenfrost on a ratchet. Nature Physics<br />
7 (5):395398, 2011.<br />
Analysis <strong>of</strong> thin liquid bilayers<br />
Dirk Peschka, Sebastian Jachalski, Robert Huth (WIAS Berlin), Barbara Wagner (TU Berlin),<br />
Andreas Münch (University <strong>of</strong> Oxford) Schedule<br />
This talk is about mathematical analysis <strong>of</strong> stationary states <strong>of</strong> liquid-liquid systems with negative<br />
spreading coefficient. Stationary solutions for the lubrication equation with precursor are<br />
studied using Γ-convergence. For the latter a simple pro<strong>of</strong> <strong>of</strong> existence and uniqueness <strong>of</strong> energy<br />
minimizers is given for suitable boundary conditions. We use these results to compare the different<br />
PDE formulations <strong>of</strong> the problem.<br />
Mini-ME3: Modelling <strong>of</strong> phase transformations in solids<br />
Organizers: Klaus Hackl (Ruhr-<strong>Universität</strong> Bochum) Mon, 16:00–18:00<br />
Christian Miehe (<strong>Universität</strong> Stuttgart) dmstm–vanadium2 2.02/03<br />
Martensitic transformation vs. plastic deformation in superelastic deformation <strong>of</strong><br />
NiTi<br />
Petr Šittner, Jan Pilch (Academy <strong>of</strong> Sciences <strong>of</strong> the Czech Republic, Prague), Caroline Curfs<br />
(ESRF Grenoble), Remi Delville (University <strong>of</strong> Antwerps) Schedule<br />
Simultaneous martensitic transformation and plastic deformation taking place during cyclic superelastic<br />
deformation <strong>of</strong> thin NiTi wires in tension will be discussed based on the recent experimental<br />
evidence obtained by in-situ synchrotron X-ray diffraction, electrical resistivity and ex-situ transmission<br />
electron microscopy studies <strong>of</strong> microstructures in deformed wires. The obtained results<br />
serve as a basis for dedicated simulations <strong>of</strong> NiTi superelasticity in a wide temperature range<br />
by micromechanics model <strong>of</strong> SMA polycrystal. It is found that, beyond the basic characteristics<br />
<strong>of</strong> the martensitic transformations involved and plastic yield stress <strong>of</strong> the alloy, the shape and
Minisymposia ME1 – ME3 19<br />
stability <strong>of</strong> superelastic stress-stress curves depends critically on the grain interactions i.e. on the<br />
partitioning <strong>of</strong> stress, strain and phase fractions among particularly oriented polycrystal grains.<br />
This partitioning depends significantly on the parent austenite texture <strong>of</strong> the wire and develops<br />
during superelastic cycling in case <strong>of</strong> simultaneous transformation and plasticity. As an ultimate<br />
outcome <strong>of</strong> this research, it is suggested how combination <strong>of</strong> microstructure control by the cold<br />
work/annealing, fine precipitate strengthening and texture control can be used to achieve optimized<br />
stable superelasticity <strong>of</strong> NiTi wires in tension.<br />
Variational Phase Field Modeling <strong>of</strong> Laminate Microstructure at Large Strains<br />
F. Hildebrand, C. Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
The macroscopic mechanical behavior <strong>of</strong> many materials crucially depends on the formation<br />
and evolution <strong>of</strong> their microstructure. Many materials develop laminate-type microstructure as<br />
a consequence <strong>of</strong> phase transformations. In this work, we outline theoretical and computational<br />
modeling concepts for such microstructures based on phase field approaches.<br />
Focussing on the regularization <strong>of</strong> kinematically compatible sharp interfaces, we present a new<br />
variational phase field approach to the coupled problem <strong>of</strong> mechanical deformation and dissipative<br />
phase transformation in martensitic CuAlNi. We demonstrate the capability <strong>of</strong> our formulation<br />
to predict the formation and dissipative evolution <strong>of</strong> laminate microstructure.<br />
Starting point for our approach is the discussion <strong>of</strong> the link between the sharp interface<br />
formulation and its phase field regularization which is connected to the notion <strong>of</strong> Γ-convergence.<br />
Based on these considerations, we derive a physically motivated coherence-dependent interface<br />
energy enforcing kinematical compatibility, an energetically concise bulk energy and a dissipation<br />
potential accounting for the dissipative phase boundary propagation. The results are exploited for<br />
the formulation <strong>of</strong> a regularized phase field model for elastic materials undergoing large strains and<br />
dissipative phase transformations. Finally, a suitable gradient-extended rate-type and incremental<br />
variational framework is constructed.<br />
To demonstrate the modeling capabilities and numerical solution techniques, we carry out<br />
simulations <strong>of</strong> the formation and evolution <strong>of</strong> laminate microstructure in two-phasic martensitic<br />
CuAlNi. We then increase the complexity <strong>of</strong> our framework towards the inclusion <strong>of</strong> phase transitions<br />
with envolving three or more phase variants. Finally, we outline the conceptual extension<br />
to the formation and evolution <strong>of</strong> laminate deformation microstructure in crystal plasticity.<br />
On the interrelation between dissipation and chemical energies in modeling shape<br />
memory alloys<br />
Philipp Junker, Klaus Hackl (Ruhr-<strong>Universität</strong> Bochum) Schedule<br />
Material modeling can be carried out in many different ways. We choose the principle <strong>of</strong> maximum<br />
dissipation to derive a thermo-mechanically coupled material model for shape memory<br />
alloys. The application <strong>of</strong> this modeling method requires approaches for both Helmholtz free<br />
energy and dissipation. Although there exist different ways to define an appropriate energy, all<br />
material parameters occurring here are well defined. These are elastic constants, heat capacity or<br />
entropy and enthalpy differences, for instance.<br />
A general framework how to define dissipation is well known, too, which has to be adopted depending<br />
on the expected material reaction. However, for this purpose material parameters have<br />
to be set which can hardly be measured. We present for the simulation <strong>of</strong> shape memory alloys an<br />
approach to derive this additional dissipation parameter just from the previously mentioned, well<br />
known energetic parameters. This approach allows to display exactly the experimentally observed<br />
material reaction for a purely thermal loading. An outlook to the application <strong>of</strong> this ansatz to<br />
mechanical problems is given as well as comparison to experiments.
20 Minisymposia ME1 – ME3<br />
Modeling phase transformations during mechanical loading<br />
Alexander Hartmaier, Christoph Begau, Aenne Köster, Anxin Ma (Ruhr-<strong>Universität</strong> Bochum)<br />
Schedule<br />
Different mechanisms can contribute to the plastic deformation <strong>of</strong> materials. In this work we<br />
focus our attention on plastic deformation by dislocation slip and phase transformations. These<br />
mechanisms are <strong>of</strong>ten alternative and competing for different materials under different loading<br />
conditions described by stress state, strain rate and temperature. Two illustrative examples for<br />
competing mechanisms <strong>of</strong> dislocation-based plasticity and austenite-martensite transformationinduced<br />
plastic deformation will be given:<br />
(i) Atomistic models for shape memory alloys (SMA) are used to study the competition between<br />
dislocation-based deformation <strong>of</strong> the austenitic phase and the austenite-martensite transformation<br />
that is the origin <strong>of</strong> the shape memory effect. Due to the fundamental nature <strong>of</strong> the<br />
atomistic models the competition <strong>of</strong> both mechanisms can be studied without any ad hoc assumptions.<br />
Different loading scenarios reveal that dislocation-based deformation occurs preferentially<br />
for deformation along certain crystallographic axes. However, it is also observed that dislocations<br />
can stabilize the martensite due to their eigenstress field once all external loads are removed.<br />
(ii) A continuum model for transformation induced plasticity (TRIP) steels based on the wellknown<br />
work <strong>of</strong> Olson and Cohen [1] is modified in the following aspect: a dislocation mechanism<br />
based crystal plasticity approach describes local stress and plastic shear in each slip system <strong>of</strong> face<br />
centered cubic (FCC) austenite. Thus, we estimate the shear band intersections and calculate the<br />
resulting martensite nucleation probability. To calculate the macroscopic material properties we<br />
make use <strong>of</strong> a micromechanical approach, by setting up a representative volume element (RVE),<br />
in which all phases are represented according to given volume concentrations and morphologies.<br />
Consequently, the properties <strong>of</strong> the RVE can be homogenized to yield the macroscopic mechanical<br />
properties that result from the given microstructure.<br />
By comparing both studies a way will be sketched, how continuum transformation models will<br />
be based on the results <strong>of</strong> fundamental atomistic simulations in future work.<br />
[1] G.B. Olson and M. Cohen, Kinetics <strong>of</strong> strain induced martensite nucleation, METALLUR-<br />
GICAL AND MATERIALS TRANSACTIONS A 6 (1975) 791-795.<br />
Analytical and numerical comparison <strong>of</strong> two phase field models for phase interfaces<br />
in solids<br />
Hans-Dieter Alber (TU <strong>Darmstadt</strong>), Bernd Markert (<strong>Universität</strong> Stuttgart) Schedule<br />
The propagation speed <strong>of</strong> phase interfaces in phase field models can be determined by higher<br />
order asymptotic expansions with respect to a parameter determining the width <strong>of</strong> the interface<br />
even if the width is not small. Such higher order expansions have been developed for phase field<br />
models for interfaces in solids, which consist <strong>of</strong> either one <strong>of</strong> the evolution equations<br />
or<br />
ϕt = −f(−∂ϕψ(ε, ϕ) − ν∆xϕ)<br />
ϕt = −f(−∂ϕψ(ε, ϕ) − ν∆xϕ)|∇xϕ|<br />
for the order parameter ϕ coupled to the equations <strong>of</strong> linear elasticity. We discuss these expansions<br />
and present numerical results, by which coefficients in these expansions have been determined,<br />
which cannot be computed analytically.<br />
The model which consists <strong>of</strong> the second one <strong>of</strong> these evolution equations coupled to the equations<br />
<strong>of</strong> nonlinear elasticity is studied by Hildebrandt and Miehe and will be discussed in another<br />
talk <strong>of</strong> this minisymposium.
Minisymposia YR-MA1 – MA3 21<br />
Minisymposia YR-MA1 – MA3<br />
Mini-YR-MA1: Stochastic partial differential equations (SPDEs) and applications<br />
Organizers: Alexander Litvinenko (TU Braunschweig) Tue, 10:00–12:00<br />
Claudia Schillings (<strong>Universität</strong> Trier) dmstm–dynamicum 0.04<br />
Numerical treatment <strong>of</strong> uncertainties in aerodynamic shape optimization<br />
Claudia Schillings, Volker Schulz (<strong>Universität</strong> Trier) Schedule<br />
The proper treatment <strong>of</strong> uncertainties in the context <strong>of</strong> aerodynamic shape optimization is a<br />
very important challenge to ensure a robust performance <strong>of</strong> the optimized airfoil under real life<br />
conditions. This talk will propose a general framework to identify, quantize and include stochastic<br />
distributed, aleatory uncertainties in the overall optimization procedure. Appropriate robust<br />
formulations <strong>of</strong> the underlying deterministic problem and uncertainty quantification techniques<br />
in combination with adaptive discretization approaches are investigated in order to measure the<br />
effects <strong>of</strong> the uncertainties in the input data on quantities <strong>of</strong> interest in the output. Finally, algorithmic<br />
approaches based on multiple-setpoint ideas in combination with one-shot methods as<br />
well as numerical results are presented.<br />
Uncertainty Quantification in numerical Aerodynamic via low-rank Response Surface<br />
Alexander Litvinenko, Hermann G. Matthies (TU Braunschweig) Schedule<br />
On the example from numerical aerodynamic we illustrate how uncertainties in the input data:<br />
parameters and computational domain propagate into the solution [1,3]. The mathematical model<br />
is described via a Navier-Stokes system <strong>of</strong> equations with a k-w turbulence model. The computing<br />
domain is the RAE-2822 airfoil. To reduce storage requirement and computing time, we demonstrate<br />
the rSVD based algorithm, which computes a low-rank approximation <strong>of</strong> the whole set <strong>of</strong><br />
realisations <strong>of</strong> the random solution [1,3]. This approximation allows us to compute a low-rank<br />
approximation <strong>of</strong> the response surface and then perform postprocessing (e.g. compute the mean<br />
value, variance, etc) with a linear complexity and with drastically reduced memory requirements.<br />
In [2] we <strong>of</strong>fer numerical algorithms, based on the canonical tensor format, to handle uncertainties<br />
in high-dimensional spaces.<br />
[1] A. Litvinenko, H. G. Matthies, Uncertainty Quantification in numerical Aerodynamic via<br />
low-rank Response Surface, accepted in Special Issue <strong>of</strong> the Communications in Statistics<br />
Journal devoted to SMTDA2010, (2010).<br />
[2] M. Espig, W. Hackbusch, A. Litvinenko, H. G. Matthies, and E. Zander, Efficient Analysis<br />
<strong>of</strong> High Dimensional Data in Tensor Formats, submitted in 2011 to Springer Lecture Note<br />
series for Computational Science and Engineering.<br />
[3] A. Litvinenko, H. G. Matthies, Sparse data formats and efficient numerical methods for uncertainties<br />
quantification in numerical aerodynamics,<br />
Proceedings <strong>of</strong> ECCM-2010, www.eccm2010.org/complet/fullpaper_1036.pdf, pp. 1-15, Paris,<br />
(2010).<br />
Efficient Global Response Surfaces for Aerodynamic Functions<br />
Benjamin Rosenbaum, Volker Schulz (<strong>Universität</strong> Trier) Schedule<br />
We want to approximate aerodynamic functions coming from CFD solvers like the TAU code.<br />
The solver is regarded as a black-box and we only measure relations between vector valued input
22 Minisymposia YR-MA1 – MA3<br />
and scalar output parameters (response). For these input-output relations we want to generate<br />
a surrogate model which is fast to evaluate, using only few computationally expensive CFD<br />
evaluations. The aerodynamic functions like lift or drag for an airfoil depending on inputs like<br />
the Mach number and the angle <strong>of</strong> attack α behave highly nonlinear, so that traditional response<br />
surface methods like regression models perform poorly.<br />
The statistical interpolation method called Kriging has been widely used in geostatistics since<br />
the fifities, it was introduced for computer experiments in the eighties and is nowadays applied<br />
to CFD simulation and optimization. It is a very flexible method, allowing the use <strong>of</strong> different<br />
correlation models and even the incorporation <strong>of</strong> secondary information: e.g. Cokriging makes use<br />
<strong>of</strong> the cross-correlation with a secondary variable for increasing the approximation quality, while<br />
in Gradient Enhanced Kriging derivatives <strong>of</strong> the response y(x) are additionally used. This aspect<br />
is especially significant in the CFD context, where gradient information can be relatively cheaply<br />
accessed by adjoint solvers.<br />
Since CFD evaluations consume an enormous amount <strong>of</strong> computation time, the need for an<br />
appropriate design <strong>of</strong> experiment arises. Simple space filling designs like the Latin hypercube<br />
design cannot capture critical regions <strong>of</strong> the input parameter space, while many expensive CFD<br />
evaluations are wasted on redundant samples. We investigate sequential adaptive sampling strategies,<br />
where at every stage a surrogate model is generated and assessed to find suitable locations<br />
for new samples.<br />
In order to further reduce the number <strong>of</strong> required samples, we introduce the new concept <strong>of</strong><br />
generic surrogate models. Response surfaces <strong>of</strong> a mutual problem class (like lift depending on<br />
(Ma, α) for different airfoil geometries) share mutual characteristics which we want to exploit for<br />
new testcases. Previously generated surrogate models for different airfoil geometries are stored in<br />
a sample function database and a principal component analysis is performed. For a new testcase’s<br />
sample data, a generic surrogate model is generated by fitting a linear combination <strong>of</strong> the<br />
most important components. Then the sample data is interpolated by a variable fidelity method,<br />
a Kriging-type interpolation which uses the generic surrogate model as a global trend. With this<br />
framework, the approximation error can be reduced compared to normal Kriging and globally<br />
valid surrogates can be generated from small sample sizes.<br />
A stochastic variational inequality approach to elastoplastic problem described by<br />
uncertain parameters<br />
Bojana V. Rosic, Hermann G. Matthies (TU Braunschweig) Schedule<br />
Following the principles <strong>of</strong> the theory <strong>of</strong> stochastic variational inequalities <strong>of</strong> second kind, we<br />
derive the abstract mixed variational formulation <strong>of</strong> the quasi-static elastoplasticity described by<br />
uncertain parameters, such as bulk and shear modulus, yield stress and hardening. By applying<br />
standard results <strong>of</strong> convex analysis we show the existence, uniqueness, and convergence <strong>of</strong> the<br />
solution by extending the results obtained for the corresponding deterministic formulation. Since<br />
the problem reduces to the minimisation <strong>of</strong> convex functional, we numerically solve it via stochastic<br />
closest point projection algorithm in “white noise analysis “ manner. In other words, we<br />
apply intrusive stochastic Galerkin method fundamentally based on polynomial chaos algebra. As<br />
it does not rely on sampling, the method is shown to be very robust and accurate. Finally, the<br />
method is validated on simple numerical examples in plane strain conditions by comparison with<br />
the direct integration techniques.<br />
Numerical methods for shape optimization under uncertainty<br />
Martin Pach, Rüdiger Schultz (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
We investigate the impact <strong>of</strong> uncertainty in shape optimization problems. In particular, we consi-
Minisymposia YR-MA1 – MA3 23<br />
der elastic structures under random forces. Therefor a formulation for shape optimization models<br />
with risk functions will be presented. The required numerical methods, these are level set methods<br />
and a grid generation algorithm, are discussed.<br />
Efficient approximation <strong>of</strong> the stochastic Galerkin matrix in the canonical tensor<br />
format<br />
Philipp Wähnert, Mike Espig, Wolfgang Hackbusch (MPI Leipzig), Hermann G. Matthies (TU<br />
Braunschweig) Schedule<br />
In this talk we consider the stochastic diffusion problem −∇ · (exp γ∇u) = f with zero boundary<br />
conditions where γ denotes a Gaussian random field with zero mean and given covariance<br />
function. The Stochastic Galerkin discretization permits to calculate deterministically a random<br />
field solving this partial differential equation with uncertainties. However this approach usually<br />
leads to stiffness matrices K whose size grows exponentially with the degree <strong>of</strong> freedom used<br />
by the discretization. Various attempts were made to attenuate this curse <strong>of</strong> dimensionality by<br />
using different iterative solvers which take advantage <strong>of</strong> the special block structure <strong>of</strong> the stiffness<br />
matrix and parallelization techniques for further optimizations.<br />
Our approach is to approximate the stiffness matrix K in a data sparse tensor format. This<br />
allows to perform matrix vector multiplication effectively in order to apply iterative solving techniques<br />
in high dimensions. Regarding the special structure <strong>of</strong> the truncated Karhunen-Loève<br />
expansion <strong>of</strong> exp γ and the polynomial chaos expansion <strong>of</strong> the resulting random variables it is<br />
possible to construct an approximation in the canonical tensor format. Under additional assumptions<br />
on γ we are able to pro<strong>of</strong> that the rank <strong>of</strong> this approximation does not depend exponentially<br />
on the number <strong>of</strong> degrees <strong>of</strong> freedom in the stochastic discretization.<br />
Mini-YR-MA2: Differential algebraic equations: theory, numerics and applications<br />
Organizers: Stephan Trenn (TU Kaiserslautern) Tue, 10:00–12:00<br />
Matthias Voigt (MPI Magdeburg) dmstm–germanium2 3.02/03<br />
On perturbations in the leading coefficient matrix <strong>of</strong> time-varying index-1 DAEs<br />
Thomas Berger (TU Ilmenau) Schedule<br />
Time-varying index-1 DAEs and the effects <strong>of</strong> perturbations in the leading coefficient matrix are<br />
investigated. A reasonable class <strong>of</strong> allowable perturbations is introduced. Robustness results in<br />
terms <strong>of</strong> the Bohl exponent and perturbation operator are presented. Finally, a new stability<br />
radius involving these perturbations is introduced and investigated. In particular, a lower bound<br />
for the stability radius is derived. The results are presented by means <strong>of</strong> illustrative examples.<br />
A converse Lyapunov theorem for switched DAEs<br />
Stephan Trenn, Fabian Wirth (<strong>Universität</strong> Würzburg) Schedule<br />
For switched ordinary differential equations (ODEs) it is well known that exponential stability under<br />
arbitrary switching yields the existence <strong>of</strong> a common Lyapunov function. The result is known<br />
as an “converse Lyapunov Theorem”. For switched differential algebraic equations (DAEs) such a<br />
result is not known yet in general. Recently, it was shown that a certain commutativity condition<br />
yields a quadratic Lyapunov function similar as for the switched ODE case. Since the solution <strong>of</strong><br />
switched DAEs might exhibit jumps the generalization <strong>of</strong> the converse Lyapunov Theorem is not<br />
trivial. The talk will aim to present a solution to this problem.<br />
Coupled systems as Abstract Differential-Algebraic Equations<br />
Michael Matthes (<strong>Universität</strong> zu Köln) Schedule
24 Minisymposia YR-MA1 – MA3<br />
We study so called Abstract Differential-Algebraic Equations (ADAEs) which are Differential-<br />
Algebraic Equations (DAEs) with operators acting on infinite dimensional Hilbert or Banach<br />
spaces. In applications these equations arise when coupling DAEs and partial differential equations<br />
(PDEs). Information is shared between these two systems by certain coupling operators. For<br />
example specific models in circuit simulation were already studied in the literature in the context<br />
<strong>of</strong> ADAEs or PDAEs.<br />
While theory and numerics <strong>of</strong> DAEs and PDEs were well developed in the last 20 years there<br />
are just a few results for coupled DAE-PDE systems concerning solvability and convergence. We<br />
study a general prototype class <strong>of</strong> a coupled system where the infinite dimensional part <strong>of</strong> the<br />
system is governed by a monotone operator. Investigating especially the coupling terms we give an<br />
existence and uniqueness result <strong>of</strong> this prototype system. Also the Galerkin approach is discussed<br />
as it is important for numerical applications.<br />
Numerical Methods for PDAE Constraint Optimal Control<br />
Jan Heiland, Volker Mehrmann (TU Berlin) Schedule<br />
The basis for the numerical analysis <strong>of</strong> optimal control problems governed by partial differential<br />
equations with algebraic constraints is the linear time varying differential-algebraic equation system.<br />
This is due to the fact that sooner or later a numerical solution procedure approximates the<br />
PDAE by a linearization and a space discretization.<br />
Therefore the work presented concentrates on time-varying descriptor systems and quadratic<br />
cost functionals. The associated Euler-Lagrange equations that provide necessary and sometimes<br />
sufficient conditions are given by a boundary value problem. This boundary value problem is<br />
always a differential-algebraic equation system. Thus a solution may not exist because <strong>of</strong> inconsistency,<br />
lacking smoothness <strong>of</strong> the data or singularity <strong>of</strong> the cost functional.<br />
We give conditions on the state equations and the cost functional for the existence <strong>of</strong> a<br />
solution to the Euler-Lagrange equations if one employs a Riccati ansatz. A special focus lies on<br />
semi-explicit DAEs <strong>of</strong> differentiation index 2 that may be used to formulate spatially discretized<br />
Navier-Stokes equations.<br />
We further discuss numerical approaches to the approximate solution <strong>of</strong> the so obtained differential<br />
algebraic Riccati matrix equations and the application to flow control problems.<br />
H∞-Norm Computation for Large Sparse Descriptor Systems<br />
Matthias Voigt, Peter Benner (MPI Magdeburg) Schedule<br />
In this talk we discuss an iterative algorithm for the computation <strong>of</strong> the H∞-norm <strong>of</strong> continuoustime<br />
linear-time invariant descriptor systems<br />
E ˙x(t) = Ax(t) + Bu(t), y(t) = Cx(t),<br />
with transfer function G(s) := C(sE − A) −1 B. Hereby we focus on the case where E and A are<br />
large and sparse matrices, so direct methods as described in [1] cannot be applied.<br />
Our algorithm is based on the computation <strong>of</strong> the complex structured stability radius <strong>of</strong> the<br />
matrix pencil λE − A, defined by<br />
rC(E, A, B, C) := inf {�∆� 2 : Λf(E, A + B∆C) ∩ iR �= ∅} ,<br />
and the relation<br />
1<br />
�G� = H∞ rC(E, A, B, C) .<br />
To obtain rC we compute a sequence <strong>of</strong> complex structured pseudospectral abscissae<br />
αε(E, A, B, C) := max {Re z : z ∈ Λε(E, A, B, C)}
Minisymposia YR-MA1 – MA3 25<br />
with the complex structured pseudospectrum<br />
Λε(E, A, B, C) := � z ∈ C : z ∈ Λ(E, A + B∆C) for a ∆ ∈ C m×p with �∆� 2 < ε � .<br />
Then, αrC (E, A, B, C) = 0. To compute αε(E, A, B, C) for given ε we adapt an existing iterative<br />
scheme for the computation <strong>of</strong> the unstructured stability radius <strong>of</strong> a matrix [2] to our problem.<br />
[1] P. Benner, M. Voigt: L∞-norm computation for continuous-time descriptor systems using<br />
structured matrix pencils, IEEE Trans. Automat. Control, 2011, accepted.<br />
[2] N. Guglielmi, M. L. Overton: Fast algorithms for the approximation <strong>of</strong> the pseudospectral<br />
abscissa and pseudospectral radius <strong>of</strong> a matrix, 2011, submitted.<br />
Mini-YR-MA3: Trends in model predictive control<br />
Organizers: Timm Faulwasser (<strong>Universität</strong> Magdeburg) Tue, 10:00–12:00<br />
Karl Worthmann (<strong>Universität</strong> Bayreuth) dmstm–helium2 3.08/09<br />
Introduction to Model Predictive Control<br />
Karl Worthmann (<strong>Universität</strong> Bayreuth), Timm Faulwasser (<strong>Universität</strong> Magdeburg) Schedule<br />
In recent years model predictive control (MPC) has become a very active field <strong>of</strong> research in<br />
systems and control theory. The scientific interest in MPC is fostered by the increasing needs to<br />
run industrial systems and processes both safely and efficiently. The possibility to consider nonlinear<br />
models with state and input constraints as well as the online optimization <strong>of</strong> the process<br />
performance are key features which lead to application related interest in MPC. Although many<br />
successful applications <strong>of</strong> nonlinear MPC are reported, there are still numerous open theoretical<br />
questions regarding MPC schemes with guaranteed stability and robustness properties. Furthermore,<br />
the extension to advanced control tasks is subject <strong>of</strong> ongoing research, e.g. schemes suitably<br />
designed for trajectory tracking, direct cost optimizing control, or the control <strong>of</strong> time-varying systems.<br />
In addition, the development <strong>of</strong> efficient optimization strategies, which allow for fast online<br />
solutions <strong>of</strong> the underlying optimal control problems, is <strong>of</strong> vital interest for the application <strong>of</strong><br />
nonlinear MPC.<br />
The focus <strong>of</strong> the minisymposium lies upon system theoretic as well as on algorithmic and<br />
numerical aspects <strong>of</strong> theoretically sound MPC schemes. This introductory talk presents the basic<br />
methodology <strong>of</strong> MPC and indicates some concepts for ensuring stability <strong>of</strong> the MPC closed loop.<br />
An active set solver for robust receding horizon control<br />
Johannes Buerger, Mark Cannon, Basil Kouvaritakis (University <strong>of</strong> Oxford) Schedule<br />
An efficient optimization procedure is proposed for computing a receding horizon control law for<br />
linear systems with additive disturbances. The algorithm uses an active set method based on<br />
Riccati recursions to solve the underlying dynamic programming problem associated with the<br />
min-max optimization <strong>of</strong> an H-infinity performance index. The active set at the solution is determined<br />
at each sampling instant as a function <strong>of</strong> the current system state using the first-order<br />
necessary conditions for optimality. The resulting algorithm has complexity per iteration which<br />
grows only linearly with prediction horizon length. The talk summarizes previous work (which<br />
focussed on the input constrained case) and gives extensions to the general setting including linear<br />
state constraints. This allows to ensure recursive feasibility through the use <strong>of</strong> suitable polyhedral
26 Minisymposia YR-MA1 – MA3<br />
backwards reachable sets guaranteeing that the state predictions enter a robust positive invariant<br />
terminal set. In the presence <strong>of</strong> state constraints the optimal value <strong>of</strong> the cost can be discontinuous,<br />
leading to degenerate subproblems at such points a key challenge which will be addressed<br />
in the talk.<br />
Improving the NMPC Algorithm via Sensitivity Analysis<br />
Jürgen Pannek (<strong>Universität</strong> der Bundeswehr München) Schedule<br />
Typically, model predictive control (MPC) algorithms consist <strong>of</strong> three steps: estimation <strong>of</strong> the<br />
initial state, solution <strong>of</strong> an optimal control problem over a finite horizon, and implementation <strong>of</strong><br />
the first element <strong>of</strong> the optimal control sequence. Although the state estimation problem can be<br />
quite challenging, the usual bottleneck <strong>of</strong> MPC is the solution <strong>of</strong> the optimal control problem.<br />
In particular, long prediction horizons and high dimensional systems may easily render the MPC<br />
algorithm to be unapplicable in real time. One way to deal with this issue is to use a forward<br />
prediction <strong>of</strong> the estimated initial state which allows for larger computing times but may be troubling<br />
in terms <strong>of</strong> robustness. Different from that, an analytically precomputed continuous feedback<br />
could be used as a tracking input. While the required prediction horizon for such an approach is<br />
typically short, the continuous feedback may be hard to obtain. Here, we follow the idea <strong>of</strong> using<br />
sensitivity analysis to combine the basic ideas <strong>of</strong> these two approaches: In a slow outer loop, the<br />
standard MPC algorithm is used to compute a feedback sequence and the corresponding sensitivity<br />
data. Then, in (one or more) inner loops, based on the sensitivity information a feedback is<br />
generated which utilizes the outer loop control as a feed forward for tracking. For this setting, we<br />
present stability results and suboptimality estimates <strong>of</strong> the proposed method with respect to the<br />
infinite horizon optimal control.<br />
Unconstrained Model Predictive Control and Suboptimality Estimates for Nonlinear<br />
Systems<br />
Marcus Reble (<strong>Universität</strong> Stuttgart) Schedule<br />
In this talk, we present a continuous-time version <strong>of</strong> recent results on unconstrained nonlinear<br />
model predictive control schemes. In order to guarantee asymptotic stability, we derive explicit<br />
conditions on the prediction horizon based on a controllability assumption <strong>of</strong> the system and two<br />
corresponding äbstractïnfinite-dimensional linear programs. The particular structures <strong>of</strong> both linear<br />
programs allow solutions involving only a single integration <strong>of</strong> a scalar variable. Furthermore,<br />
the setup allows to give guaranteed bounds on the performance compared to an infinite horizon<br />
optimal controller.<br />
Periodic Model Predictive Control<br />
Ravi Gondhalekar (Osaka University) Schedule<br />
Model predictive control (MPC) has proven highly effective for control <strong>of</strong> systems subject to<br />
constraints, but is usually considered in a time-invariant setting. On the other hand, periodic<br />
control has been considered for many decades, but usually in an unconstrained setting. In this<br />
talk recent advances in linear-periodic MPC are presented. The presented methods are extensions<br />
<strong>of</strong> the well-known methods for MPC <strong>of</strong> linear time-invariant (LTI) systems, both in the sense that<br />
the MPC concepts are extended from the LTI to the periodic setting, but importantly also in<br />
that when the periodic system has a period length <strong>of</strong> unity (i.e., LTI system) they reduce to the<br />
well-known LTI-MPC methods. There are three reasons why periodic MPC is useful. First, systems<br />
with periodic dynamics exist in practice, for example turbines, engines and walking robots.<br />
Second, systems with time-invariant dynamics may lead to periodic control problems, because the<br />
factors affecting the system are periodic. An example <strong>of</strong> this is building climate control. Third,
Minisymposia YR-MA1 – MA3 27<br />
periodic systems are convenient models <strong>of</strong> systems that may be time-invariant, but are subject<br />
to asynchronous timing constraints on the inputs. The talk highlights the final reason.<br />
Model Predictive Control for Constrained Trajectory Tracking<br />
Timm Faulwasser, Rolf Findeisen (<strong>Universität</strong> Magdeburg) Schedule<br />
For set-point stabilization using model predictive control approaches many solutions exist. For<br />
application relevant problems beyond set-point stabilization – like trajectory tracking and path<br />
following– only a few results with explicit stability guarantees exist.<br />
We discuss a model predictive control approach to trajectory tracking problems <strong>of</strong> constrained<br />
continuous time systems, where the reference trajectory is apriori known. To handle the timevarying<br />
nature <strong>of</strong> the tracking problem we advocate the use <strong>of</strong> time-varying level sets <strong>of</strong> Lyapunov<br />
functions as terminal regions. We present necessary and sufcient conditions for positive invariance<br />
<strong>of</strong> these sets. We show how these sets can be efficiently computed via an infinite dimensional linear<br />
programm, if a quadratic Lyapunov function is available. The applicability <strong>of</strong> the method is shown<br />
considering a nonlinear CSTR.
28 Minisymposia YR ME1 – ME3<br />
Minisymposia YR ME1 – ME3<br />
Mini-YR-ME1: Structural optimization in view <strong>of</strong> robustness and sensitivity<br />
Organizers: Martin Liebscher (DYNAmore GmbH) Tue, 10:00–12:00<br />
Uwe Reuter (TU Dresden) dmstm–platinum2 2.07/08<br />
Uncertainty in structural dynamics and aeroelasticity: modelling, propagation and<br />
identification<br />
Hamed Haddad Khodaparast (The University <strong>of</strong> Liverpool) Schedule<br />
Knowledge in the field <strong>of</strong> modelling and predicting the dynamic responses <strong>of</strong> aerostructures is<br />
constantly developing. Modelling <strong>of</strong> uncertainty is considered as one <strong>of</strong> the tools that increases<br />
confidence by providing extra information. This information may then be useful in planning physical<br />
tests. The complexity <strong>of</strong> structures together with uncertainty-based methods leads inevitably<br />
to increased computation; therefore deterministic approaches are preferred by industry and a safety<br />
factor is incorporated to account for uncertainties. However, the selection <strong>of</strong> a proper safety<br />
factor relies on engineering insight. Hence, there has been much interest in developing efficient<br />
uncertainty-based methods with a good degree <strong>of</strong> accuracy.<br />
In this lecture we first briefly introduce the methods for modelling uncertainty in the parameters<br />
<strong>of</strong> structural model. Then methods for propagation <strong>of</strong> structural uncertainty through dynamic<br />
systems are explained. Although the propagation method may be used directly for quantification<br />
<strong>of</strong> dynamic responses but an issue <strong>of</strong> very practical significance is the initial estimation <strong>of</strong> the<br />
parameter uncertainty to be propagated particularly when the uncertain parameters cannot be<br />
measured, such as damping and stiffness terms in mechanical joints or material-property variability.<br />
What can be measured is the variability in dynamic behaviour as represented by natural<br />
frequencies, mode shapes, or frequency response functions. The inverse problem then becomes<br />
one <strong>of</strong> inferring the parameter uncertainty from statistical measured data. These approaches are<br />
referred to as uncertainty identification or stochastic model updating. Two uncertain identification<br />
methods which have been already developed by the author are explained in this lecture.<br />
A combined approach <strong>of</strong> considering uncertainty in optimization tasks to efficiently<br />
identify robust designs<br />
Marco Götz, Stephan Pannier, Wolfgang Graf, Michael Kaliske (TU Dresden) Schedule<br />
The aim <strong>of</strong> almost all design tasks is to determine a robust design. In order to assess the robustness,<br />
the uncertainty <strong>of</strong> input parameters has to be taken into account. The incorporation <strong>of</strong><br />
uncertain parameters in an optimization task may succeed in an active or passive manner. In an<br />
active approach, also denoted as here-and-now strategy, the uncertainty for a respective design<br />
is known and the robustness can be assessed directly. Thereby, the numerical effort to determine<br />
a robust optimum can be tremendous. In a passive approach, also denoted as wait-and-see<br />
strategy, the optimal design is determined without a distinct knowledge about the uncertainty <strong>of</strong><br />
this design. A first good shot about an optimal robust design can be determined efficiently, but<br />
a quantification <strong>of</strong> the robustness is hindered.<br />
In this contribution, the theoretical bases <strong>of</strong> active and <strong>of</strong> passive optimization strategies are<br />
introduced. Both approaches are evaluated in detail and on the basis <strong>of</strong> the obtained results a<br />
combined approach is elaborated. In a combined approach the advantages should be intensified<br />
while the disadvantages should be reduced. Hence, a robust design can be identified in a numerically<br />
efficient way. The applicability <strong>of</strong> the presented approach is demonstrated by means <strong>of</strong><br />
examples.
Minisymposia YR ME1 – ME3 29<br />
Advanced analysis <strong>of</strong> sensitivities in parameter-free shape optimisation<br />
Nikolai Gerzen, Franz-Joseph Barthold (TU Dortmund) Schedule<br />
This contribution deals with sensitivity analysis in parameter-free shape optimisation. Sensitivity<br />
analysis is one <strong>of</strong> the most important parts <strong>of</strong> a structural optimisation algorithm. The efficiency<br />
<strong>of</strong> the algorithm mainly depends on the obtained sensitivity information. The pseudo load and<br />
sensitivity matrices which appear in sensitivity analysis are commonly used to derive and to calculate<br />
the gradients and the Hessian matrices <strong>of</strong> objective functions and <strong>of</strong> constraints. The aim<br />
<strong>of</strong> this contribution is to show that these matrices contain additional useful information which is<br />
not used in structural optimisation until now. We demonstrate the opportunities and capabilities<br />
<strong>of</strong> the new information which are obtained by singular value decomposition (SVD) <strong>of</strong> the pseudo<br />
load and sensitivity matrices and by eigenvalue decomposition <strong>of</strong> the Hessian matrix. We present<br />
some structural optimization algorithms which are based on the made observations. Furthermore,<br />
we avoid jagged boundaries in parameter-free shape optimisation by applying a density filtering<br />
technique well-known in topology optimization and obtain consistently filtered first and second<br />
order sensitivities. Numerical examples illustrate the advocated theoretical concept.<br />
Global sensitivity analysis for the efficient solution <strong>of</strong> optimization problem in design<br />
process<br />
Uwe Reuter, Zeeshan Mehmood (TU Dresden), Martin Liebscher (DYNAmore GmbH) Schedule<br />
Optimization <strong>of</strong> a structural design is a computationally extensive process. Complexity <strong>of</strong> structural<br />
optimization problems can be reduced if the relationship between the design parameters<br />
and the model response is effectively identified. This relationship is captured by the methods <strong>of</strong><br />
sensitivity analysis. Sensitivity analysis helps in identifying the most significant model parameters<br />
affecting a specific model response. In this contribution properties <strong>of</strong> certain meta-models or<br />
approximation techniques (e.g. neural networks, support vector machines) are evaluated for extracting<br />
sensitivity information directly from these models. These methods capture the non-linear<br />
relationships <strong>of</strong> the underlying input parameters to the design response. Sensitivity analysis with<br />
meta-models or approximation techniques is likely to be less computationally expensive and can<br />
be easily applied to the relevant industry problems.<br />
Assessment <strong>of</strong> robustness and sensitivity with solution spaces<br />
Markus Zimmermann, Lavinia Graff, Johannes Fender (BMW, Department <strong>of</strong> Vehicle Safety)<br />
Schedule<br />
Classical optimization methods seek a minimum or a maximum in the design space in order to<br />
find the best solution. Often, however, this solution is not best, e.g. when it is not robust or<br />
it is in conflict with other design goals. Therefore, more advanced methods like robust design<br />
optimization or multidisciplinary optimization are applied. Unfortunately, they have other disadvantages:<br />
they are computationally expensive, information on how to improve a non-robust<br />
solution is limited and for a multi-disciplinary optimization, a model that comprises all relevant<br />
disciplines must be provided, e.g. a model for a simultaneous vehicle crash and vibration analysis,<br />
which is typically not available. The alternative method proposed here identifies a solution space<br />
<strong>of</strong> a design problem in one discipline like crash analysis. The computed solution space is such<br />
that it guarantees a supercritical or subcritical output with a defined probability for all enclosed<br />
designs. For simplicity, the solution space is expressed as corridors for each input parameter. The<br />
corridors may be used to assess robustness and sensitivity or they may be combined with corridors<br />
<strong>of</strong> other disciplines their cross sections are global solution spaces. The underlying method<br />
relies on the Monte Carlo sampling technique built into an iterative scheme. Problems may be<br />
non-linear, high-dimensional and noisy. Practical applications to crash analysis are presented.
30 Minisymposia YR ME1 – ME3<br />
Topology synthesis <strong>of</strong> large-displacement, compliant mechanisms possessing optimized<br />
flexure hinges<br />
Frank Dirksen (<strong>Universität</strong> der Bundeswehr Hamburg, University <strong>of</strong> California, Berkeley), Tarek<br />
Zohdi (University <strong>of</strong> California, Berkeley), Rolf Lammering (<strong>Universität</strong> der Bundeswehr Hamburg)<br />
Schedule<br />
This paper presents the synthesis <strong>of</strong> large-displacement, path-following compliant mechanisms<br />
(CM) possessing optimized flexure hinges. A non-intuitive topology optimization algorithm based<br />
on a continuum design domain is described and applied to maximize the motion <strong>of</strong> the design<br />
CM on a user-specified output direction. Non-linear geometric effects are taken into account to<br />
ensure proper modelling <strong>of</strong> large displacements occurring in CM. A robust and efficient staggered<br />
optimization scheme, based on optimality criteria method (OC) and globally convergent method<br />
<strong>of</strong> moving asymptotes (GCMMA), is implemented to solve the optimization problem. The obtained<br />
final topology <strong>of</strong> the CM is able to follow the specified direction within the given precision<br />
limit.<br />
As in many current topology optimization methods, this procedure yields final topologies <strong>of</strong><br />
CM that include the positions <strong>of</strong> artificial (flexure) hinges but not their optimal shape leaving<br />
doubts on the physical meaning as well as an uncertainty in the manufacturing process. To overcome<br />
this drawback <strong>of</strong> optimized compliant mechanisms’ topologies, artificial hinges are replaced by<br />
real flexure hinges meeting the performance specifications given by the CM’s kinematics and/or<br />
by the intended application.<br />
Different flexure hinges were investigated beforehand in terms <strong>of</strong> relevant performance criteria<br />
such as maximum deflection range, bending stiffness, natural frequency and, most importantly,<br />
fatigue life. Explicit analytical expressions are derived and are validated by experimental data<br />
(cf. [1]). Solving these explicit expressions inversely enables to select or to design optimal flexure<br />
hinges meeting the desired performance specifications <strong>of</strong> each individual flexure hinge prior to<br />
any modeling or manufacturing efforts. Embedding the appropriately selected or designed flexure<br />
hinges results in final CM that are ready to manufacture. Thus, the synthesis and manufacturing<br />
process <strong>of</strong> compliant mechanisms can be accelerated significantly.<br />
[1] F. Dirksen, R. Lammering, On mechanical properties <strong>of</strong> planar flexure hinges <strong>of</strong> compliant<br />
mechanisms, Mechanical Sciences – Future directions <strong>of</strong> compliant mechanisms 2 (2011), 1<br />
– 109-117.<br />
Mini-YR-ME2: Advanced material modeling strategies at different scales with<br />
application to production processes<br />
Organizers: Benjamin Klusemann (RWTH Aachen) Tue, 10:00–12:00<br />
Ivaylo Vladimirov (RWTH Aachen) dmstm–spectrum<br />
A meshfree quasicontinuum formulation for scale-bridging material models based on<br />
interatomic potentials<br />
Dennis M. Kochmann, Malena I. Espanol, Michael Ortiz (Caltech) Schedule<br />
Modeling the mechanical behavior <strong>of</strong> solids at the micro- and nanometer scale is challenging as the<br />
discrete nature <strong>of</strong> the crystal becomes apparent: simulations using molecular dynamics provide<br />
the required accuracy but come with prohibitively high computational expenses severely limiting<br />
the simulation capabilities. Continuum models are much more attracting yet not suitable at those
Minisymposia YR ME1 – ME3 31<br />
scales where the continuum hypothesis breaks down. Hence, multiscale techniques are needed to<br />
bridge the scales from atomistics to the continuum.<br />
The quasicontinuum (QC) method was introduced to overcome the practical limitations <strong>of</strong><br />
classical atomistic modeling in terms <strong>of</strong> simulation time and space. The QC methodology employs<br />
a combination <strong>of</strong> full atomistic resolution in regions <strong>of</strong> high variations and an approximate<br />
continuum model in the major part <strong>of</strong> the simulation domain away from those regions. As the<br />
continuum description is based on discrete lattice statics with atomic positions constrained by an<br />
interpolation scheme, the model can be solely based on atomistic potentials without the need for<br />
phenomenological continuum models.<br />
Here, we present a novel quasicontinuum formulation that is based on a meshfree interpolation<br />
scheme (making use <strong>of</strong> local maximum-entropy shape functions) and new summation rules that<br />
involve representative atoms and additional quadrature-point sampling to result in high accuracy.<br />
In addition, we present a pro<strong>of</strong> <strong>of</strong> convergence and demonstrate sample applications <strong>of</strong> deformation<br />
processes in crystalline solids.<br />
Deformation patterning and grain boundary modeling through strain gradient crystal<br />
plasticity<br />
Tuncay Yalcinkaya (European Commission - Joint Research Centre, Institute for Energy and<br />
Transport) Schedule<br />
A rate dependent strain gradient crystal plasticity framework is presented where the displacement<br />
and the plastic slip fields are considered as primary variables. These coupled fields are determined<br />
on a global level by solving simultaneously the linear momentum balance and the slip evolution<br />
equation, which is derived in a thermodynamically consistent manner. The slip law differs from<br />
classical ones in the sense that it includes a non-convex free energy term, which enables patterning<br />
<strong>of</strong> the deformation field. The formulation <strong>of</strong> the computational framework is at least partially<br />
dual to a Ginzburg-Landau type <strong>of</strong> phase field modelling approach. The framework is enriched by<br />
incorporating a non-dissipative dislocation-grain boundary interaction potential in terms <strong>of</strong> grain<br />
boundary Burgers tensor. For the treatment <strong>of</strong> grain boundaries within the solution algorithm,<br />
an interface element is formulated. The proposed formulation is capable <strong>of</strong> capturing the effect <strong>of</strong><br />
misorientation <strong>of</strong> neighbouring grains and the orientation <strong>of</strong> the grain boundaries on slip evolution<br />
in a natural way. The numerical examples illustrate the patterning <strong>of</strong> deformation field in grains<br />
and plastic slip accumulation at the grain boundaries.<br />
Application <strong>of</strong> non-convex gradient plasticity to the modeling <strong>of</strong> stress relaxation<br />
and microstructure evolution<br />
Benjamin Klusemann, Bob Svendsen (RWTH Aachen) Schedule<br />
During loading <strong>of</strong> real (i.e., materially heterogeneous) metallic materials, local microscopic stress<br />
concentration activates individual microscopic defects (e.g., dislocations) in the material, resulting<br />
in a spatially heterogeneous plastic strain. During this process most metals form cellular<br />
dislocation structures, e.g. dislocation cells and dislocation walls. In general, this will take place<br />
in the material llong“before the macroscopic activation or yield threshold is reached.<br />
Only when a sufficient criticalnnumber <strong>of</strong> such defects are activated, do they collectively<br />
breakthrough to the macroscopic level, resulting, e.g., in macroscopic yield and macroscopic stress<br />
relaxation. As is well-known, one way to model such emergent behavior in many physical systems<br />
and contexts is with the help <strong>of</strong> phase-field methods and non-convexity. Several sources<br />
<strong>of</strong> non-convexity are known in material science, e.g., dislocation-lattice interaction, glide-system<br />
interaction or large deformation. As very simple non-convex energy forms we examine polynomialbased<br />
Landau-Devonshire type forms, as well as periodic forms such as the Frenkel form.
32 Minisymposia YR ME1 – ME3<br />
The purpose <strong>of</strong> this work is the modeling <strong>of</strong> the microstructure behavior <strong>of</strong> metals with gradient<br />
plasticity via energetic non-convexity. For this a model formulation based on continuum<br />
thermodynamics and rate-variational methods is presented. An exemplary metal which we are<br />
trying to model are TWIP steels. TWIP steels show different stages <strong>of</strong> deformation which can be<br />
related to the microstructural deformation mode. First the deformation is mainly slip dominated<br />
with pronounced strain hardening. Afterwards a non-pronounced serrated flow can be observed<br />
in the stress-strain curve which is related to the onset <strong>of</strong> deformation twinning. Finally the stressstrain<br />
curve shows serrated flow which is related to heavy twinning and twins intersection at the<br />
microstructural level. First numerical results <strong>of</strong> these effects will be given.<br />
Efficient simulation <strong>of</strong> non-linear micro-heterogeneous structures using an orderreduction<br />
approach<br />
Felix Fritzen, Thomas Böhlke (KIT), Samuel Forest (Ecole des Mines) Schedule<br />
The homogenization <strong>of</strong> physically nonlinear materials with microstructure is a challenging procedure.<br />
This is due to the path dependency <strong>of</strong> the local constitutive variables and the geometrical<br />
complexity on the small scale. In the past decade the nonuniform transformation field analysis<br />
(NTFA) has proven to give accurate predictions <strong>of</strong> the effective nonlinear response <strong>of</strong> such microheterogeneous<br />
materials in the presence <strong>of</strong> elasto-plasticity. The method belongs to the class <strong>of</strong><br />
order-reduction algorithms and uses an approximation <strong>of</strong> the space-time dependent plastic strain<br />
field via a finite-dimensional basis <strong>of</strong> spatially nonuniform basis functions determined in numerical<br />
experiments. These fields can account for the geometry and the physical properties <strong>of</strong> the<br />
examined materials. The evolution <strong>of</strong> the new internal variables determines the local and, thus,<br />
global stress response. Notably not only the effective stress but also the phase averages can be<br />
replicated with good accuracy even if anisotropic morphologies are considered.<br />
A concise review <strong>of</strong> previous order-reduction based homogenization schemes is presented and<br />
the capabilities <strong>of</strong> these method are outlined with respect to numerical savings and computational<br />
accuracy. Further, a novel order-reduction based homogenization scheme for visco-elastic<br />
composite materials is developed. Such materials occur in many engineering applications, e.g., in<br />
terms <strong>of</strong> fibre-reinforced polymers. The new method does not require a phenomenological evolution<br />
equation for the set <strong>of</strong> reduced internal variables representing the microscopic fields, which is<br />
a drawback in previous NTFA related works. A set <strong>of</strong> tools for the efficient analysis <strong>of</strong> the effective<br />
material behavior <strong>of</strong> visco-elastic composites is developed based on the presented formulation.<br />
Numerical results outline the capabilities <strong>of</strong> an order-reduction based approach to homogenization<br />
for the considered class <strong>of</strong> materials.<br />
A rate independent polycrystal model and a specific application for asymmetrically<br />
rolled aluminum sheets<br />
Ricardo Alves de Sousa (University <strong>of</strong> Aveiro) Schedule<br />
The asymmetric rolling process differs from conventional rolling through the use <strong>of</strong> different<br />
roll circumferential velocities or diameters. Using proper parameters, asymmetric rolling imposes<br />
intense shear deformations across the sheet thickness, leading not only to the occurrence <strong>of</strong> shear<br />
texture, but also to grain refinement. In fact, some shear texture components are known to improve<br />
plastic strain ratio values, and thus formability.<br />
In this work, the rate-independent polycrystal model <strong>of</strong> Gambin [2] was efficiently implemented<br />
and applied to predict texture on asymmetrical rolling. For FCC materials, this polycrystal<br />
plasticity model avoids the uniqueness issue related to the choice <strong>of</strong> the set <strong>of</strong> active slip systems
Minisymposia YR ME1 – ME3 33<br />
by applying a regularized Schmid Law. Consequently, it generates yield surfaces with smooth<br />
corners where the normal vector is always uniquely defined. Also, it doesn’t require the arbitrarily<br />
defined reference strain rate commonly used in the viscous-approximation <strong>of</strong> rate-dependent<br />
models.<br />
For validation purposes, a 1050-O sheet was asymmetrically rolled and annealed. Shear texture<br />
was obtained, as opposed to typical gamma-fiber texture obtained on sheets rolled through the<br />
conventional process. Moreover, shear texture was found to be retained after annealing. Shear<br />
tests were used to evaluate strength and formability, and the obtained experimental results were<br />
compared with numerical simulations. In the end, the accuracy <strong>of</strong> simulation results as well as<br />
the advantages <strong>of</strong> the asymmetric rolling process, when compared to conventional rolling are the<br />
main topics <strong>of</strong> discussion.<br />
[1] K. -H. Kim and D. N. Lee (2001), Analysis <strong>of</strong> deformation textures <strong>of</strong> asymmetrically rolled<br />
aluminum sheets, Acta Materialia 49, pp2583-2595.<br />
[2] Gambin, W. (2000), Plasticity and Textures, Kluwer Academic Press.<br />
[3] F.J.P. Simões, R.J. Alves de Sousa, J.J. Grácio, F. Barlat, J.-W. Yoon, Mechanical behavior<br />
<strong>of</strong> an asymmetrically rolled and annealed 1050-O sheet, International Journal <strong>of</strong> Mechanical<br />
Sciences 50:1372-1380, 2008<br />
Production simulation by means <strong>of</strong> a structure tensor-based framework <strong>of</strong> anisotropic<br />
plasticity - numerical aspects and experimental validation<br />
I. N. Vladimirov, S. Reese (RWTH Aachen) Schedule<br />
Advanced finite element simulations <strong>of</strong> sheet metal forming operations are essential nowadays for<br />
the design <strong>of</strong> tools and processes. One <strong>of</strong> the decisive factors influencing the simulation result<br />
is the material model being used. Sheet metal parts are subjected to stretching, bending and<br />
straightening during forming, and an accurate prediction <strong>of</strong> e.g. the blank springback requires the<br />
use <strong>of</strong> appropriate modelling approaches capable <strong>of</strong> describing the cyclic hardening behaviour <strong>of</strong><br />
metals. In addition, due to the inherent anisotropy <strong>of</strong> sheet metals, the material model should<br />
be able to describe initial and deformation-induced anisotropy. Sheet metals exhibit anisotropic<br />
plastic behavior due to their textured or generally orientation-dependent microstructure. Many<br />
problems in sheet metal forming arise due to the inherent sheet anisotropy. During the rolling<br />
process <strong>of</strong> the sheet, large plastic deformations take place which may induce texture and are<br />
responsible for the initial anisotropy.<br />
In this work, we discuss a finite strain continuum mechanical model combining both nonlinear<br />
isotropic hardening and nonlinear kinematic hardening. The kinematic hardening component,<br />
which is the significant factor in simulating springback, represents a continuum extension <strong>of</strong> the<br />
classical rheological model <strong>of</strong> Armstrong-Frederick kinematic hardening. The evolution <strong>of</strong> elastic<br />
anisotropy is represented by defining the Helmholtz free energy as a function <strong>of</strong> a family <strong>of</strong><br />
evolving structure tensors. In addition, plastic anisotropy is modelled via the dependence <strong>of</strong> the<br />
yield surface on the plastic deformation and on the same family <strong>of</strong> structure tensors. Exploiting<br />
the dissipation inequality leads to the interesting result that all tensor-valued internal variables<br />
are symmetric. Thus, the integration <strong>of</strong> the evolution equations can be efficiently performed by<br />
means <strong>of</strong> a form <strong>of</strong> the exponential map algorithm based on an implicit time integration scheme.<br />
It automatically satisfies plastic incompressibility in every time step, and in addition, has the<br />
advantage <strong>of</strong> preserving the symmetry <strong>of</strong> the internal variables.
34 Minisymposia YR ME1 – ME3<br />
Mini-YR-ME3: Non-standard discretization methods for multi-physics<br />
Organizers: Dirk Hartmann (Siemens AG) Tue, 10:00–12:00<br />
Thomas Richter (<strong>Universität</strong> Heidelberg) dmstm–vanadium2 2.02/03<br />
Computational Challenges in Multi-Physics Problems<br />
Dirk Hartmann (Siemens AG, Corporate Technology) Schedule<br />
Computational modelling <strong>of</strong> continuum mechanical phenomena plays an important role in many<br />
engineering disciplines as well as in many industrial developmental processes. Setting up corresponding<br />
computational studies in existing computational tools is rather complex involving four<br />
major steps: simplification <strong>of</strong> CAD geometries, generating appropriate meshes, solution <strong>of</strong> the<br />
underlying physical models, and visualization <strong>of</strong> the results. Considering problems involving different<br />
physical models the process <strong>of</strong> setting up simulations is even more complex since typically<br />
several different computational algorithms have to be coupled.<br />
In this talk, we will address two <strong>of</strong> the major challenges: an efficient handling <strong>of</strong> complex<br />
domains and the corresponding CAD and mesh generation process as well as a simplification <strong>of</strong><br />
current computational tool chains. Furthermore, we will outline a meshless particle based method<br />
for continuum mechanics, being a candidate to solve the two challenges. The presented Lagrangian<br />
particle method can efficiently realize also Dirichlet boundary conditions via appropriate<br />
interpolation schemes and thus allows an elegant formulation <strong>of</strong> multiphysics problems, e.g. fluid<br />
structure interaction problems as well as multiscale problems like crack growth. Using Multi -<br />
GPGPU architectures the method can be efficiently parallelized and thus allowing a simulation <strong>of</strong><br />
rather complex setups on Desktop PCs. The presented method is therefore a candidate to resolve<br />
two <strong>of</strong> the major challenges in computational engineering and industrial developmental processes.<br />
The Unfitted Discontinuous Galerkin method as a Multi-Physics framework<br />
Christian Engwer (Universtät Münster) Schedule<br />
We are facing an increasing complexity in the models <strong>of</strong> scientific computing. Multi-physics applications,<br />
highly non-linear processes and domains exhibiting a complex shape are only some<br />
examples <strong>of</strong> such complexity. These changes pose a big challenge to the development <strong>of</strong> scientific<br />
s<strong>of</strong>tware. On the one hand the requirements on the s<strong>of</strong>tware are growing, e.g. broader feature sets,<br />
demand for easy parallelism. On the other hand the turn over times are getting shorter, which<br />
requires shorter development times.<br />
To handle these requirements, DUNE provides a flexible framework for grid based methods for<br />
the solution <strong>of</strong> PDEs. We present an extensions <strong>of</strong> the DUNE framework to handle multi-physics<br />
and multi-domain applications. It is based on the Unfitted Discontinous Galerkin method, which<br />
provides higher order cut-cell methods based on a Discontinuous Galerkin discretization. The<br />
module allows flexible computations while still allowing an efficient, i.e. rapid, implementation <strong>of</strong><br />
new simulations. Domain boundaries are given as a level-set function, which allows computations<br />
on time-depended domains. Suitable coupling conditions are imposed along the interface.<br />
We introduce the new framework and show some brief example applications.<br />
A multiscale mesh-free modeling <strong>of</strong> particles in suspension<br />
Xin Bian, Marco Ellero, Nikolaus A. Adams (TU München) Schedule<br />
We apply the smoothed dissipative particle dynamics (SDPD)[1] method to model hard particles<br />
in suspension. SDPD is a Lagrangian mesh-free method, which is based on smoothed particle<br />
hydrodynamics (SPH) discretization <strong>of</strong> the Navier-Stokes equations and further incorporates
Minisymposia YR ME1 – ME3 35<br />
thermal fluctuations on the hydrodynamic variables in a thermodynamically consistent way. The<br />
resultant SDPD algorithm has similar formulation as another popular mesoscopic method, namely<br />
dissipative particle dynamics (DPD). Therefore SDPD is considered as a multiscale framework<br />
linking SPH to DPD[2] and it can be used as a simulation tool for fluid problems ranging from<br />
granular flow down to colloidal suspension.<br />
Rigid structures (e.g., grain, colloid, micro-channel) are modeled by frozen SDPD particles<br />
(boundary particles) and no-slip boundary condition on the interface is improved by velocity<br />
interpolation during viscous and stochastic force calculations[3]. After pairwise forces between<br />
SDPD particles are calculated, the total force and torque on the rigid structure are obtained<br />
by accumulating forces and torques exerted by surrounding solvent particles on the boundary<br />
particles. Then the dynamics <strong>of</strong> the rigid body is decoupled from the solvent by integrating a<br />
separate Newtonian equation <strong>of</strong> motion. As numerical results, dynamics <strong>of</strong> both one and multiple<br />
solid particles are simulated and compared with references.<br />
[1] P. Español and M. Revenga, Smoothed dissipative particle dynamics, Phys. Rev. E, 67(2):,<br />
026705, 2003.<br />
[2] A. Vázquez-Quesada, M. Ellero, and P. Español, Consistent scaling <strong>of</strong> thermal fluctuations<br />
in smoothed dissipative particle dynamics, J. Chem. Phys., 130(3): 034901, 2009.<br />
[3] X. Bian, S. Litvinov, R. Qian, M. Ellero, and N. A. Adams, Multiscale modeling <strong>of</strong> particle<br />
in suspension with smoothed dissipative particle dynamics, Phys. Fluids, accepted, <strong>2012</strong>.<br />
Numerical Simulations <strong>of</strong> Chemotaxis-Driven PDEs<br />
Andriy Sokolov, Stefan Turek, Robert Strehl (TU Dortmund) Schedule<br />
In the last twenty years one can observe a rapid and consistent growth <strong>of</strong> interest for biomathematical<br />
applications. Among them are modeling <strong>of</strong> tumor invasion and metastasis (Chaplain<br />
et al.), modeling <strong>of</strong> vascular network assembly (Preziosi et al.), pattern formations due to<br />
the Turing-type instability (Murray et al.) or chemotaxis-driven processes (Horstmann et al.),<br />
protein-protein interaction on the membrane (Goryachev, Bastiaens) and others. These mathematical<br />
models, presented as systems <strong>of</strong> advection-reaction-diffusion equations, can take into consideration<br />
various biological processes (e.g. transport, random walk, reaction, chemotaxis, growth<br />
and decay, etc.). In order to get an accurate numerical solution in a reasonably finite time one has<br />
to construct an efficient, fast and robust numerical scheme for a sufficiently large class <strong>of</strong> partial<br />
differential equations.<br />
In our recent research we combine the system <strong>of</strong> the generalized Keller-Segel model for multispecies<br />
with reaction-diffusion equations on (evolving in time) surfaces, which can be mathema-
36 Minisymposia YR ME1 – ME3<br />
tically written in the following form<br />
∂ui<br />
∂t =<br />
+<br />
random walk/diffusion<br />
� �� �<br />
D u i ∆ui + ∇ ·<br />
⎡ species-species interaction species-agents interaction⎤<br />
�� �� �<br />
⎢ n�<br />
� �� �� �<br />
m�<br />
�<br />
⎥<br />
⎢<br />
⎥<br />
⎢ κi,kui∇uk − χi,kui∇ck ⎥<br />
⎣<br />
⎦ +<br />
k=1,k�=i<br />
kinetics<br />
� �� �<br />
fi(c, ρ), in Ω, (1)<br />
∂cj<br />
∂t = Dc decay production<br />
� �� � � �� �<br />
m�<br />
n�<br />
j∆cj − αk,jck + βk,juk +gj(u, ρ), in Ω (2)<br />
∂ρl<br />
∂t =<br />
k=1<br />
diffusion on surface<br />
� �� �<br />
D ρ<br />
l ∆Γρl<br />
source<br />
k=1<br />
� �� �<br />
+ sl(u, c), on Γ (3)<br />
where ui(, t) (i = 1, n) and cj(, t) (j = 1, m) are some solutions (for example, species and chemical<br />
agents) defined in a domain Ω ⊂ d (d = 1, 2, 3), and ρl (l = 1, p) are solutions defined on a<br />
surface Γ(t) ⊂ Ω. By ∆Γ· we denote the Laplace-Beltrami operator on Γ. Corresponding initial<br />
and boundary conditions are prescribed.<br />
Equations (3) describe the change <strong>of</strong> concentrations or substances on a (time dependent) surface.<br />
These equations have a variety <strong>of</strong> applications in computational physics, scientific visualization,<br />
image analysis and computer graphics. For example, from the molecular biology it is known that<br />
many important and scientifically interesting processes in a cell occur on a membrane. The form<br />
<strong>of</strong> which can vary in time as a response to these processes (for example protein-protein interaction<br />
in works <strong>of</strong> Goryachev and Bastiaens). The presence <strong>of</strong> the equations (3) helps to keep track on<br />
solutions, which react on the membrane. To find both numerical solutions <strong>of</strong> the system <strong>of</strong> PDEs<br />
on a surface and the modification <strong>of</strong> a shape <strong>of</strong> the evolving in time surface is a very nontrivial<br />
task. It requires a pr<strong>of</strong>ound research and a sufficient amount <strong>of</strong> time for the algorithmic realization<br />
and programming implementation.<br />
On the other hand, the generalized Keller-Segel system for multi-species (1)–(2) is very interesting<br />
from both a mathematical and a modeling point <strong>of</strong> view, since it describes a wide range <strong>of</strong> patternforming<br />
and aggregating behavior, blow-up phenomena and stability effects. Moreover, numerical<br />
challenges require the construction <strong>of</strong> a positivity-preserving and non-oscillatory scheme, since<br />
straightforward FEM simulation <strong>of</strong> the system (1)–(2) is not possible. Also, efficient solvers<br />
for coupled nonlinear systems should be taken into account. Here, we present a new symmetric<br />
flux-corrected transport (FCT) algorithm applied to the generalized Keller-Segel model (1)–(2).<br />
Corresponding numerical simulations demonstrate a realistic behavior for chemotaxis-driven problems.<br />
We believe that the construction <strong>of</strong> a fast, efficient and robust numerical scheme for the system<br />
(1)–(3) will serve as a basis for a reliable s<strong>of</strong>tware tool to be used as a ’virtual biomathematical<br />
laboratory’ for different hierarchies <strong>of</strong> models and parameter settings in various applications<br />
<strong>of</strong> biology and medicine.<br />
A dynamic load-balancing MPI-PThreads hybrid implementation <strong>of</strong> the Optimal<br />
Transportation Meshfree (OTM) method<br />
Bo Li, Mark Stalzer, Michael Ortiz (Caltech) Schedule<br />
We present a parallel computational implementation <strong>of</strong> the Optimal Transportation Meshfree<br />
(OTM) method <strong>of</strong> Li et al. [1] and the parallel seizing contact and variational material point<br />
failure algorithms for simulating general fluid and solid flows. The OTM method <strong>of</strong> Li et al.<br />
k=1
Minisymposia YR ME1 – ME3 37<br />
combines elements <strong>of</strong> Optimal Transportation theory with local MaxEnt meshfree interpolation<br />
<strong>of</strong> the fields and material point sampling. The OTM method enforces mass transport and<br />
essential boundary conditions exactly as well as exact conservation <strong>of</strong> linear and angular momentum.<br />
The parallel implementation <strong>of</strong> the OTM method uses a multilevel distributed memory and<br />
shared memory scheme. Domain decomposition algorithms based on graph theory or geometric<br />
techniques are employed to distribute material points to separate processors. A shadow scheme<br />
is proposed to define the shared information among partitions which is synchronized by using<br />
the de facto standard message passing interfaces (MPI). To this end, the collection <strong>of</strong> material<br />
points on each processor is further partitioned based on a dynamic computational cost function<br />
as a second level parallelization with the utilization <strong>of</strong> the POSIX Threads library. The parallel<br />
approach has been applied to predict the high energy density dynamic response <strong>of</strong> materials on<br />
departmental class systems. Excellent speedup to O(10 5 ) threads is achieved in our large scale<br />
three-dimensional OTM simulations <strong>of</strong> ballistic/hypervelocity impact. We also find ideal weak<br />
scaling in our applications <strong>of</strong> concurrent multiscale computing.<br />
[1] B. Li, F. Habbal, M. Ortiz, Optimal transportation meshfree approximation schemes for fluid<br />
and plastic flows, Int. J. Numer. Meth. Engng 83(2010), 1541–1579.<br />
Fluid Structure Interaction in Fully Eulerian Coordinates<br />
Thomas Richter (<strong>Universität</strong> Heidelberg) Schedule<br />
In this contribution we present a formulation for fluid-structure interaction problems which is<br />
given in Eulerian coordinates for both sub-problems, fluid and solid. By this setting it is possible<br />
to derive a novel monolithic formulation <strong>of</strong> the coupled problem.<br />
In contract to the well-established Arbitrary Lagrangian Eulerian (ALE) coordinates - a very<br />
common basis for monolithic modeling <strong>of</strong> fluid-structure interactions - the Eulerian formulation<br />
goes without the introduction <strong>of</strong> an artificial coordinate system and artificial domain mappings.<br />
In ALE coordinates this mapping <strong>of</strong> the fluid domain <strong>of</strong>ten gives rise to problems when dealing<br />
with large deformation, free movement <strong>of</strong> the structure or even contact <strong>of</strong> the structure with<br />
parts <strong>of</strong> the boundary (topology change). While the Eulerian formulation in principal allows for<br />
such problems it brings along new difficulties connected to the Eulerian coordinate system used<br />
to describe the structural problem.<br />
We will describe the basic idea <strong>of</strong> modeling fluid-structure interactions in Eulerian coordinates<br />
and present a finite element scheme for its discretization. Further, for verification <strong>of</strong> this<br />
novel formulation, we analyze benchmark-problems in comparison to classical approaches like<br />
the Arbitrary Lagrangian Eulerian coordinates. Finally, we point out capabilities <strong>of</strong>fered by this<br />
formulation which cannot be considered in classical monolithic approaches.
38 Section 1: Multi-body dynamics<br />
Section 1: Multi-body dynamics<br />
Organizers: Peter Betsch (<strong>Universität</strong> Siegen), Bernd Simeon (TU Kaiserslautern)<br />
S1.1: Optimization <strong>of</strong> MBS Tue, 13:30–15:30<br />
Chair: Peter Betsch S2|02–C110<br />
Planned contacts and collision avoidance on optimal control problems<br />
Sigrid Leyendecker (<strong>Universität</strong> Erlangen-Nürnberg), Gwen Johnson, Michael Ortiz (Caltech)<br />
Schedule<br />
When simulating the dynamics <strong>of</strong> three-dimensional multibody systems, the treatment <strong>of</strong> contact<br />
always imposes a challenge. One simple solution is to formulate a smooth problem where the<br />
bodies are allowed to overlap by a certain amount, which is penalized via a penalty potential. Of<br />
course, the drawbacks going along with this approach <strong>of</strong> inadmissible configurations and inexact<br />
contact forces are obvious. Non-smooth formulations require the specification <strong>of</strong> a contact force<br />
that (for elastic collisions) reflects the momentum normal to a contact surface at a given time and<br />
configuration. In the context <strong>of</strong> a structure preserving time integration method (being consistent<br />
in the evolution <strong>of</strong> energy and momentum maps) that uses a predefined equidistant time grid,<br />
there is no other known procedure except for resolving the collisions in the sense that each contact<br />
time (which is likely between the nodes), configuration, and force are exactly computed, see [1].<br />
This work will show how the described alternatives for the treatment <strong>of</strong> collisions can be<br />
included in the context <strong>of</strong> optimal control problems. In the smooth formulation with a penalty<br />
potential, there arises some difficulty for the optimiser to distinguish between a contact and a<br />
control force, since both might point into the same direction. For the nonsmooth treatment, the<br />
optimal control problem formulation gives more freedom than the forward dynamics problem,<br />
since periodic boundary conditions or leaving the exact placement <strong>of</strong> time nodes (within certain<br />
bounds) to the optimiser leaves the freedom to assume that contact takes place at a certain<br />
time node without loss <strong>of</strong> generality, i.e. without fixing its physical time. A further challenge<br />
is the detection <strong>of</strong> contact for non-convex three-dimensional bodies where a new strategy based<br />
on a supporting separating hyperplane linear programming approach is used [2]. Reconfiguration<br />
and docking manoeuvres with collision avoidance and with planned collisions are considered as<br />
examples.<br />
[1] R.C. Fetecau, J.E. Marsden, M. Ortiz, and M. West. Nonsmooth Lagrangian mechanics and<br />
variational collision integrators. Siam J. applied dynamical systems, 2, 381-416, 2003.<br />
[2] G. Johnson, M. Ortiz, and S. Leyendecker. A linear programming-based algorithm for the<br />
signed separation <strong>of</strong> (non-smooth) convex bodies. Submitted for publication, 2011.<br />
Topology Optimization <strong>of</strong> Members <strong>of</strong> Elastic Multibody Systems<br />
Alexander Held, Robert Seifried (<strong>Universität</strong> Stuttgart) Schedule<br />
Lightweight techniques are applied increasingly <strong>of</strong>ten for modern machine designs in order to reduce<br />
the moving masses and therewith the energy consumption. However, as a result the stiffness<br />
<strong>of</strong> the system decreases causing undesired elastic deformations and therewith end-effector deviations.<br />
In this talk a topology optimization procedure for elastic multibody systems is presented<br />
to lower end-effector tracking errors.<br />
To capture both the large nonlinear working motion and the deformation <strong>of</strong> the bodies the<br />
system has to be modeled as elastic multibody system. In case the deformations are compara-
Section 1: Multi-body dynamics 39<br />
tively small the floating frame <strong>of</strong> reference formulation is <strong>of</strong>ten the most efficient approach. In<br />
this formulation the global nonlinear motion is described by a reference frame while the elastic<br />
deformations are described with respect to the reference frame using shape functions and elastic<br />
coordinates.<br />
In topology optimization the goal is to distribute a limited amount <strong>of</strong> mass in a reference<br />
domain such that the compliance <strong>of</strong> the structure becomes minimal under certain loads. For the<br />
presented topology optimization the Solid Isotropic Material with Penalization (SIMP) approach<br />
is used. However, since the global shape functions are obtained from finite element models by<br />
modal analysis, the SIMP approach is slightly adapted to avoid localized modes. To solve the<br />
large scale optimization problem efficiently the Method <strong>of</strong> Moving Asymptotes is applied.<br />
The established optimization workflow resembles the equivalent static loads method. Thereby<br />
a series <strong>of</strong> transient simulations is performed. After each transient simulation a set <strong>of</strong> equivalent<br />
static loads is derived and an improved design is determined. In doing so the highly expensive<br />
sensitivity analysis <strong>of</strong> the design variables in the time domain is avoided. To lower tracking errors,<br />
the displacement fields are selected at the time points at which the highest end-effector deviations<br />
occur.<br />
The results show that topology optimization can be successfully employed to optimize the<br />
design <strong>of</strong> elastic members <strong>of</strong> elastic multibody systems. More precisely the system is stiffened<br />
with respect to the dynamical loads <strong>of</strong> a specified motion. Thereby the number <strong>of</strong> global shape<br />
functions should be selected carefully since they determine the representable displacement fields<br />
and therewith the quality <strong>of</strong> the optimization results.<br />
Trajectory Planning and Optimization <strong>of</strong> Mechanisms with Redundant Kinematics<br />
for Manufacturing Processes with Constant Tool Speed<br />
Andreas Scholz, Francisco Geu Flores, Andrés Kecskeméthy (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
The present paper deals with the optimal path planning for kinematically redundant mechanisms<br />
in manufacturing processes which require constant tool speed along given paths on the workpiece.<br />
A three-stage optimization method is introduced that allows for the computation <strong>of</strong> the<br />
mechanisms optimal design and its control by discretizing the problem and transforming it into a<br />
nonlinear constrained optimization problem which can be solved using standard SQP algorithms.<br />
The method is presented by means <strong>of</strong> a planar serial robot with three rotational degrees <strong>of</strong> freedom<br />
θ ∈ R 3 and an auxiliary mechanism with one rotational degree <strong>of</strong> freedom ϕ ∈ R about<br />
an axis normal to the robot‘s working plane. The tool is mounted at the end effector, whereas<br />
the workpiece is fixed to the auxiliary mechanism. Since it is required that the tool traverses<br />
a prescribed path S on the workpiece with a given, constant velocity ˙s and angle <strong>of</strong> attack ψ,<br />
the motion <strong>of</strong> the system is defined by the motion ϕ(t) <strong>of</strong> the auxiliary mechanism. The goal is<br />
to compute the optimal control ϕ(t) as well as the optimal initial pose <strong>of</strong> the mechanism with<br />
respect to the robot‘s inertial coordinate system which allow for a maximal constant tool velocity<br />
˙s subject to the maximally allowed angular displacements, velocities, and accelerations at the<br />
robot‘s actuators. The control ϕ(t) is parameterized by an interpolating quadratic spline with m<br />
spline parameters. The optimal set <strong>of</strong> parameters and the initial pose <strong>of</strong> the mechanism relative<br />
to the robot are sought by means <strong>of</strong> a three step optimization method. The first stage consists<br />
in searching for a feasible initial guess by minimizing the standard deviation <strong>of</strong> the joint angles<br />
during the motion using only few spline segments and a small value for ˙s. In the second stage,<br />
the number <strong>of</strong> spline segments is refined while ˙s remains unmodified. The third stage consists <strong>of</strong><br />
a sequence <strong>of</strong> optimization runs with increasing tool speed ˙s at each intermediate step. Hereby, ˙s<br />
is increased in small increments such that the optimizer is always able to find a feasible solution
40 Section 1: Multi-body dynamics<br />
and ˙s approaches asymptotically its maximal value. The three stage optimization method yields<br />
good convergence properties, allowing for the determination <strong>of</strong> the minimal process cycle time.<br />
A Hamiltonian conserving indirect optimal control method for multibody dynamics<br />
Ralf Siebert, Peter Betsch (<strong>Universität</strong> Siegen) Schedule<br />
In the past, a lot <strong>of</strong> effort has gone into the development <strong>of</strong> structure-preserving time-stepping<br />
schemes for forward dynamic problems. This is due to the superior numerical stability <strong>of</strong> these<br />
integrators. Guided by previous developments in the design <strong>of</strong> energy-momentum integrators for<br />
forward dynamic problems, a Hamiltonian conserving indirect optimal control method will be<br />
introduced. For the state equations, a midpoint evaluation or a consistent variant there<strong>of</strong> will be<br />
applied. Based on this specific discretization <strong>of</strong> the state equations, a discretization <strong>of</strong> the costate<br />
equations will be introduced, which is based on the notion <strong>of</strong> a discrete derivative and which<br />
leads to the algorithmic conservation <strong>of</strong> the discrete Hamiltonian. As in the forward dynamic<br />
case, it can be expected, that a Hamiltonian conserving method will yield superior numerical<br />
stability properties. Therefore, the newly developed method will be compared with a previously<br />
introduced direct transcription method. We will test the newly proposed method with some<br />
numerical examples, which are, for example, the optimal control <strong>of</strong> a 3-link manipulator. Therein,<br />
the control effort, which is necessary for moving the multibody system from one configuration to<br />
another, will be minimized.<br />
About identifying inertia and friction parameters in mechanisms<br />
Johannes Rutzmoser, Markus Roßner, Thomas Thümmel, Heinz Ulbrich (TU München) Schedule<br />
Mechanisms in general are transmissions with speed droop and continuous and non-continuous<br />
motion. They are widely used in processing machines. For identifying the inertia parameters, which<br />
are the crucial parameters for the dynamics <strong>of</strong> the system, the eigenmotion <strong>of</strong> the mechanism can<br />
be utilized for contributing to an objective function in an optimization.<br />
This methodology is shown at a crank rocker mechanism test rig, where the inertia parameters<br />
are identified in a first step. The experimentally created pseudo-eigenmotion is compared with<br />
the ideal eigenmotion <strong>of</strong> the multibody simulation model. With numerical optimization the error<br />
between experiment and simulation is minimized by varying the unknown inertia parameters. In<br />
order to improve accuracy, the sensitivity <strong>of</strong> the different parameters with respect to the indicator<br />
functions is evaluated and regarded in the optimization.<br />
In a second step the friction parameters <strong>of</strong> the joints are identified with transient operations<br />
<strong>of</strong> the machine. Therefore, force- and speed-dependent friction laws are used. Covering noncontinuous<br />
motion <strong>of</strong> the mechanism components, boundary lubrication regimes are considered<br />
in the speed-dependent model. Further comparisons <strong>of</strong> different settings in experiment and simulation<br />
show that a speed-dependent friction model describes the observed speed <strong>of</strong> the test rig<br />
quite well.<br />
S1.2: Analytical Mechanics Tue, 16:00–18:00<br />
Chair: Christian Hesch S2|02–C110<br />
An Approach for Decomposition <strong>of</strong> Finite Rotations<br />
Clementina Mladenova (Institute <strong>of</strong> Mechanics, Bulgarian Academy <strong>of</strong> Sciences) Schedule<br />
The presentation <strong>of</strong> rigid body displacements is an old mechanical problem but <strong>of</strong> a great importance<br />
in solving different real tasks. In geometrical and computational mechanics rigid body<br />
kinematics is considered through vectors and matrices approaches. In this aspect the rotation
Section 1: Multi-body dynamics 41<br />
group in three dimensional space may be described combining our knowledge from analytical mechanics,<br />
vector analysis, algebra and differential geometry. Here is the place to mention that the<br />
different parameterizations <strong>of</strong> the rotation group SO(3) influence on the efficiency <strong>of</strong> the kinematic<br />
and dynamic models as at one rigid body so in multibody mechanical systems. The analytical<br />
representations <strong>of</strong> any rotation can be expressed by defining its action on vectors, quaternions<br />
or spinors. On the other hand the parameterizations <strong>of</strong> the rotations are: Eulerian angles in the<br />
classical 3-1-3 sense and all other combinatons like: 3-2-3, 3-2-1, 1-2-3 and etc., are known as<br />
Bryant angles, Eulerian parameters, Cayley-Klein parameters and etc. To find the resultant axis<br />
and angle <strong>of</strong> rotation after two, three or more finite partial rotations is a problem very important<br />
in multibody mechanics. But the inverse problem, namely, to decompose a finite rotation into<br />
three partial rotations about prescribed axis is a more difficult one and it is very important in<br />
motion planning in the group <strong>of</strong> rotations and inverse kinematic problem at a manipulator system<br />
as well. The present paper gives explicit formulae in solving this problem using vector-like<br />
parameterization <strong>of</strong> rotation group. In the first part the notion vector-parameter is introduced<br />
and its properties are given. After that the above-mentioned problem is solved and exemplified<br />
in concrete settings. The method is realized analytically using the computer algebra system Mathematica.<br />
Cases <strong>of</strong> Complete Integrability in Transcendental Functions in Dynamics and Certain<br />
Invariant Indices<br />
Maxim V. Shamolin (Institute <strong>of</strong> Mechanics, Lomonosov Moscow State University) Schedule<br />
The results <strong>of</strong> this work appeared in the process <strong>of</strong> studying a certain problem on the rigid body<br />
motion in a medium with resistance, where we needed to deal with first integrals having nonstandard<br />
properties. Precisely, they are not analytic, not smooth, and on certain sets, they can<br />
be even discontinuous. Moreover, they are expressed through a finite combination <strong>of</strong> elementary<br />
functions. However, the latter circumstances allowed us to carry out a complete analysis <strong>of</strong> all<br />
phase trajectories and show those their properties which have a roughness and are preserved for<br />
systems <strong>of</strong> a more general form having certain symmetries <strong>of</strong> latent type.<br />
This work is the study <strong>of</strong> the problem <strong>of</strong> 2D- and 3D- motion <strong>of</strong> a symmetric rigid body that<br />
interacts with the medium only through a plane part (cavitator) <strong>of</strong> its exterior surface too. In<br />
constructing the force field, we use the information about the properties <strong>of</strong> streamline flow around<br />
under quasistationarity conditions, and the medium motion is not studied in this case. In contrast<br />
to the previous works where the dependence <strong>of</strong> the force moment on the body angular velocity<br />
is neglected, in this work, in accordance with experiment, we take into account the effects <strong>of</strong><br />
influence <strong>of</strong> the rotational derivatives <strong>of</strong> hydro-aero-dynamical forces in components <strong>of</strong> the body<br />
angular velocity.<br />
The multiparameter family <strong>of</strong> system phase portraits on the two- and threedimensional cylinder<br />
wich characterized the invariant indices was obtained.<br />
Vibrations <strong>of</strong> rotating systems with an infinite number <strong>of</strong> degrees <strong>of</strong> freedom.<br />
Artur Wirowski (Technical University <strong>of</strong> Lodz) Schedule<br />
The subject <strong>of</strong> the paper is a system an infinite number <strong>of</strong> electrically charged beams, which<br />
interact each other by electrostatic forces. Each beam is simply supported at the center <strong>of</strong> gravity<br />
and thus has one degree <strong>of</strong> freedom, it is possible to its rotation around the fulcrum. All <strong>of</strong> beams<br />
are arranged one above another thus creating electrostatic forces interconnected system with an<br />
infinite number <strong>of</strong> degrees <strong>of</strong> freedom.<br />
Aim <strong>of</strong> this study is to describe the forced vibration <strong>of</strong> such a system. In this paper, starting<br />
from a single beam equilibrium equation derived continuous equation <strong>of</strong> motion <strong>of</strong> this system. Is
42 Section 1: Multi-body dynamics<br />
considered the impact <strong>of</strong> additional assumptions on the form <strong>of</strong> the resulting equations <strong>of</strong> motion,<br />
such as small angles <strong>of</strong> rotation plates and their uniform distribution. After taking into account<br />
these simplifications, the equation is obtained analogous to the equation <strong>of</strong> vibrating string:<br />
where γ, θ are constant, M(x, t) is external moment.<br />
1<br />
γ2 ∂2φ ∂t2 − ∂2φ = θM(x, t) (1)<br />
∂x2 The equation (1) is solved for the sample boundary-initial conditions. The paper presents and<br />
discussed the results. In the summary also shows the possible practical applications <strong>of</strong> the present<br />
theoretical model and the planned directions <strong>of</strong> further research the author.<br />
[1] G. Genta, Dynamics <strong>of</strong> rotating systems, Mechanical Engineering Series,<br />
Springer Science+Buisness, NY USA (2005).<br />
[2] P. Blanchard, R.L. Devaney, G.R. Hall, Differential Equations, Thompson, (2006)<br />
The moons perigee and plumb-in line<br />
Dmitry G. Kiryan (Institute <strong>of</strong> Problems <strong>of</strong> Mechanical Engineering, RAS), Georgy V. Kiryan<br />
(The Main Astronomical Observatory, RAS) Schedule<br />
In this paper we have established a functional relationship between deflection <strong>of</strong> a gravitational<br />
field line and lunar perigee location. Physical nature <strong>of</strong> the process inducing the Chandler wobble<br />
has been shown. We have proved that the Chandler wobble results from a combination <strong>of</strong> two<br />
types <strong>of</strong> motion: additional rotation <strong>of</strong> the Earth and cyclic motion <strong>of</strong> the Moon around the Earth.<br />
We suggest here a physical model <strong>of</strong> the Earths interior structure as a system <strong>of</strong> two separate<br />
masses: the Core and the Earth. The cause-and-effect relationship between the lunar perigee<br />
coordinates and the Core location within the Earth has been revealed. The results obtained fit<br />
well the presently available data from astronomical and gravimetrical observations.<br />
S1.3: Control <strong>of</strong> MBS Tue, 16:00–18:00<br />
Chair: Hartmut Bremer S2|07–109<br />
Feedforward Control <strong>of</strong> Multibody Systems by Rheonomic Constraints<br />
Werner Schiehlen, Robert Seifried, Thomas Gorius, Steffen Raach (<strong>Universität</strong> Stuttgart) Schedule<br />
Controlling nonlinear multibody systems usually the inverse dynamics approach is used, e.g.<br />
[1-3]. The feedforward control scheme is simply computed from the equations <strong>of</strong> motion, and<br />
complemented by a linear feedback approach to compensate measurement errors and parameter<br />
variations. From a mechanical point <strong>of</strong> view the feedforward control can also be introduced using<br />
the prescribed motion as a rheonomic constraint. Then, a kinematically determined multibody<br />
system has to be analysed.<br />
In this paper the constraint forces and torques due to rheonomic constraints for kinematically<br />
determined systems without any degree <strong>of</strong> freedom are discussed, see also [4]. Matrix methods are<br />
presented for the design <strong>of</strong> the feedforward control. As an example a assembly device is considered<br />
and simulations <strong>of</strong> the results achieved are shown.<br />
[1] Blajer, W.; Schiehlen, W.: Walking Without Impacts as a Motion/Force Control Problem.<br />
Journal <strong>of</strong> Dynamic Systems, Measurement, and Control, Trans. ASME 114, 660 – 665,<br />
1992.
Section 1: Multi-body dynamics 43<br />
[2] Spong, M.W.; Hutchinson, S.; Vidyasagar, M.: Robot Modeling and Control. Wiley, Hoboken,<br />
2006.<br />
[3] Liu Fan; Er Meng Joo: Linear and Nonlinear PD-type Control <strong>of</strong> Robotic Manipulators for<br />
Trajectory Tracking. Industrial Electronics and Applications, 2009. (ICIEA 2009). 4th IEEE<br />
Conference, 25 – 27 May 2009, 3442 – 3447.<br />
[4] Schiehlen, W.; Eberhard, P.: <strong>Technische</strong> Dynamik. 3. Auflage, B.G. Teubner, Wiesbaden,<br />
<strong>2012</strong>.<br />
Modeling and Quasi-Static Trajectory Control <strong>of</strong> a Self-Balancing Two-Wheeled Vehicle<br />
F. Johannes Kilian, Hubert Gattringer, Hartmut Bremer (<strong>Universität</strong> Linz) Schedule<br />
This paper deals with the kinematical and dynamical model as well as a quasi-static trajectory<br />
controller <strong>of</strong> a self-balancing two-wheeled vehicle. This mobile robot is about 50cm tall, autonomous,<br />
unstable and driven by two wheels and therefore used for transport purposes. Due to the<br />
nonholonomic contraints only few modeling techniques are feasible. In this contribution several<br />
modeling methods are compared, followed by the derivation <strong>of</strong> various control strategies.<br />
A partial feedback linearization in combination with a LQR controller is applied to stabilize<br />
the inclination angle <strong>of</strong> the robot. The quasi-static trajectory controller, which is based on the<br />
kinematical model, uses a flatness based approach in order to remain along the desired path.<br />
Continous curvature paths, composed by clothoids, are used to demonstrate good performance<br />
results in simulation and experiment.<br />
Recursive Methods in Modeling and Control <strong>of</strong> Modular Robotic Systems<br />
Bernhard Oberhuber, Hubert Gattringer, Hartmut Bremer (<strong>Universität</strong> Linz) Schedule<br />
This paper addresses the dynamical modeling and control <strong>of</strong> reconfigurable modular robots. The<br />
modular actuators (brushless DC motors with Harmonic Drive gears) for the robots under consideration<br />
are connected by rigid links. This way the robot can be assembled in different configurations<br />
by rearranging these components. For dynamical modeling the Projection Equation in<br />
Subsystem representation is used, taking advantage <strong>of</strong> its modular structure. Due to the lack <strong>of</strong><br />
position sensors at the gearbox output shaft, deflections caused by the elasticities in the gears<br />
can not be compensated by the PD motor joint controller. Therefore, a correction <strong>of</strong> the motor<br />
trajectory is needed, which can be calculated as part <strong>of</strong> a flatness based feed-forward control using<br />
the exact model <strong>of</strong> the robot. With the recursive approach proposed in this paper the concept <strong>of</strong><br />
reconfigurability is retained. For validation a redundant articulated robot arm with seven joints<br />
is regarded and results are presented.<br />
Natural co-ordinates for control applications<br />
Nicolas Sänger, Peter Betsch (<strong>Universität</strong> Siegen) Schedule<br />
Natural coordinates have emerged to be well-suited for both rigid and flexible multibody dynamics.<br />
Especially the combination <strong>of</strong> structural elements and energy-momentum consistent time<br />
stepping schemes leads to superior numerical stability as well as an automatable assembly, resulting<br />
in both excellent run-time behaviour as well as moderate modelling effort (see [1]). Incorporation<br />
<strong>of</strong> modern methods for finite-element simulations, such as mortar methods for contact or<br />
domain decomposition both for structural elements as well as continuum elements is straightforward<br />
([2]).
44 Section 1: Multi-body dynamics<br />
Augmentation techniques allow a systematic integration <strong>of</strong> both mechanical and non-mechanical<br />
quantities for simulation (see [3] and [4]), which makes this approach suitable especially for emulation<br />
and simulation <strong>of</strong> mechatronic systems. We will present an approach for evaluating forward<br />
control strategies with flexible multibody systems.<br />
[1] Sänger, N. ; Betsch, P.: A nonlinear finite element framework for flexible multibody<br />
dynamics: Rotationless formulation and energy-momentum conserving discretization . In:<br />
Bottasso, C.L. (Hrsg.) ; Masarati, P. (Hrsg.); Trainelli, L. (Hrsg.): Proceedings <strong>of</strong> the<br />
ECCOMAS Thematic Conference on Multibody Dynamics. Politecnico di Milano, Milano,<br />
Italy, 25-28 June 2007<br />
[2] C. Hesch and P. Betsch. A mortar method for energy-momentum conserving schemes in<br />
frictionless dynamic contact problems.Int. J. Numer. Meth. Engng, 77(10):1468–1500, 2009.<br />
[3] Bottasso, C.L. ; Croce, A.: Optimal Control <strong>of</strong> Multibody Systems Using an Energy<br />
Preserving Direct Transcription Method. In: Multibody System Dynamics 12 (2004), Nr. 1,<br />
S. 17–45<br />
[4] Betsch, P. ; Uhlar, S.: Energy-momentum conserving integration <strong>of</strong> multibody dynamics.<br />
In: Multibody System Dynamics 17 (2007), Nr. 4, S. 243–289<br />
Comparative study on control concepts <strong>of</strong> a robot manipulator with multiplelink/joint<br />
flexibilities<br />
Peter Staufer, Hubert Gattringer, Hartmut Bremer (<strong>Universität</strong> Linz) Schedule<br />
If one is dealing with active vibration suppression on a highly nonlinear flexible system, various<br />
techniques are needed. On the one hand a suitable dynamic model <strong>of</strong> the system is required.<br />
And on the other hand intelligent model based control concepts are necessary for active vibration<br />
damping. We deal with a basic model, where the flexibilities are approximated with linear springs<br />
and dampers, a so called lumped element model (LEM). For the control design a two degree <strong>of</strong><br />
freedom control scheme is suggested for solving the tracking problem, based on the LEM. The<br />
most important benefit using this control concept is that the feedforward part can be designed<br />
independent from the feedback part. Hereby the feedforward control is based on the flatness<br />
approach. For the feedback control several strategies are studied using acceleration- and gyrosensor<br />
measurements. Moreover the basis for the latter one is a linearization along the trajectory, where<br />
a tracking error system is obtained.<br />
The contribution is completed with a validation by measurements with a very fast trajectory on<br />
an articulated robot with two flexible links and three elastic joints.<br />
Application <strong>of</strong> one-dimensional piezoelectric structure in numerical control <strong>of</strong> a biomechanical<br />
system<br />
Pawel Olejnik, Jan Awrejcewicz (Technical University <strong>of</strong> Lodz) Schedule<br />
A biomechanical model <strong>of</strong> human chest with a sensor attached to the chest’s posterior surface is<br />
subject to an impulsive action <strong>of</strong> external impact force. The sensor is taken into consideration<br />
as a one-dimensional dynamical system <strong>of</strong> a piezoelectric energy harvester. Investigations focus<br />
on application <strong>of</strong> a controlled function <strong>of</strong> reaction that would minimize deformation <strong>of</strong> the chest<br />
cave caused by the impact loading. Because <strong>of</strong> difficulties appeared in measurement <strong>of</strong> the impact<br />
force exciting in the system it is proposed to measure displacement <strong>of</strong> the chest’s posterior surface<br />
x5 by means <strong>of</strong> the piezoelectric energy harvester. The one-dimensional dynamical system <strong>of</strong> a
Section 1: Multi-body dynamics 45<br />
piezoelectric energy harvester (supplement <strong>of</strong> the controlled system) produces a measurement<br />
signal used in a scheme <strong>of</strong> active control.<br />
The system <strong>of</strong> equations <strong>of</strong> the biomechanical part <strong>of</strong> the model is as follows:<br />
˙xi = xi+4 , ˙x4 = x7 + ¯ k −1<br />
23 ¯c23(x2 − x4) , ˙x5 = m1 −1� k12(x2 − x1) � ,<br />
˙x6 = m2 −1� k12(x1 − x2) − k23(x2 − x3) − ¯ k23(x2 − x4) − c23(x6 − x7) � , (1)<br />
˙x7 = m3 −1� k23x2 − (k23 + ks)x3 + c23x6 − (c23 + ¯c23 + cs)x7 + ¯c23x8 − u � ,<br />
where: i = 1 . . . 3, m1 . . . m3 denote the separated point masses <strong>of</strong> the model, ¯c = [c23, c ′ 23, cs], ¯ k =<br />
[k12, k23, k ′ 23, ks] are the vectors <strong>of</strong> system stiffness and damping (respectively), ¯xd(t) = [x1 . . . x4]<br />
is the vector <strong>of</strong> system displacements in each direction, ¯xv(t) = [x5 . . . x8] is the vector <strong>of</strong> system<br />
velocities, but with regard to the introduced rheological description <strong>of</strong> the model the massless<br />
point reduces dimension <strong>of</strong> the system to 7. Thus, object <strong>of</strong> control (the plant) is described by an<br />
odd-dimension system state vector, means ¯x = [¯xd, x5 . . . x7].<br />
The piezoelectric element has mass mp and is connected to a resistor. Its dynamics is described<br />
by a set <strong>of</strong> three first-order differential equations constituting basic electromechanical coupling<br />
between y1, v and x5:<br />
˙y1 = y2 , ˙y2 = −kpmt −1 y1 + θv − ˙x5 , ˙v = −θcp −1 y2 − cpR −1 v , (2)<br />
where: kp - effective stiffness, mt - approximate total mass <strong>of</strong> the piezoelectric system, R - leakage<br />
resistance, y1(t) - distance between the pro<strong>of</strong> mass and the base, θ - electromechanical coupling,<br />
v(t) - voltage through the piezoelement.<br />
Preliminary computations confirm that the additional piezoelectric system generate useful<br />
signal <strong>of</strong> measurement. Reduction <strong>of</strong> deformation <strong>of</strong> the idealised chest has been obtained after<br />
utilisation <strong>of</strong> active control based on minimization <strong>of</strong> the performance index <strong>of</strong> LQR method.<br />
S1.4: New Developments in MBS Methodology Wed, 13:30–15:30<br />
Chair: Bernd Simeon S2|02–C110<br />
Bridging Particle Swarm Optimization and Swarm Robotics from A Multibody Point<br />
<strong>of</strong> View<br />
Peter Eberhard, Qirong Tang (<strong>Universität</strong> Stuttgart) Schedule<br />
Particle Swarm Optimization (PSO) originally appears as a typical optimization algorithm and<br />
it has been applied to many areas due to its robustness and simple applicability without the need<br />
for cumbersome derivative calculations. In this study we want to bridge some gaps between PSO<br />
and swarm robotics using a multibody point <strong>of</strong> view.<br />
On the one hand the particles in PSO are moving independently in the search space exchanging<br />
some information according to their update formulae. This is somehow quite similar to the robots<br />
search scenario. If one particle is replaced by one robot then the PSO search for the minimum<br />
<strong>of</strong> an objective function can be mapped to a scenario <strong>of</strong> swarm robots searching targets in an<br />
environment. Of course in this case the particles possible motion is determined not only by the<br />
PSO update, but also by the robots mechanical properties and their drives. Thus, the PSO was<br />
extended to a mechanical PSO in order to consider the feasible dynamics, the inertia, and also<br />
the finite size <strong>of</strong> the robots to avoid collisions during their search.<br />
On the other hand, although groups <strong>of</strong> robots can give a super behavior in a swarm compared<br />
to simple individuals, it is still a challenge to guide the whole group <strong>of</strong> robots to search targets<br />
systematically using conventional methods. This is because a group <strong>of</strong> robots needs heavily simultaneous<br />
localization and mapping. Therefore, one can bring the mechanical PSO to generate
46 Section 1: Multi-body dynamics<br />
the search trajectory as the main guidance for robots by benefiting from PSO’s powerful search<br />
ability. Then the robots further perform fine tuning for obstacle avoidance and mutual avoidance<br />
locally.<br />
Based on above consideration, some tests were performed with both simulations and experiments<br />
using a group <strong>of</strong> physical robots (the Festo Robotinos).<br />
A modular and efficient approach to computational modeling and sensitivity analysis<br />
<strong>of</strong> robot and human motion dynamics<br />
Martin Friedmann, Janis Wojtusch, Oskar von Stryk (TU <strong>Darmstadt</strong>) Schedule<br />
In this paper a new class library for the computation <strong>of</strong> the forward multi-body system dynamics<br />
<strong>of</strong> robots and biomechanical models <strong>of</strong> human motion is presented. By the developed modular modeling<br />
approach the library can be flexibly extended by specific modeling elements like joints with<br />
specific geometry or different muscle models and thus can be applied efficiently for a number <strong>of</strong><br />
dynamic simulation and optimization problems. The library not only provides several methods for<br />
solving the forward dynamics problem (like articulated body or composite rigid body algorithms)<br />
which can transparently be exchanged. Moreover, the numerical solution <strong>of</strong> optimal control problems,<br />
like in the forward dynamics optimization <strong>of</strong> human motion, is significantly facilitated by<br />
the computation <strong>of</strong> the sensitivity matrix with respect to the control variables. Examples are<br />
given to demonstrate the efficiency <strong>of</strong> the approach.<br />
On the Analysis <strong>of</strong> Multibody Systems in the Presence <strong>of</strong> Uncertainties<br />
Nico-Philipp Walz, Michael Hanss (<strong>Universität</strong> Stuttgart) Schedule<br />
As in other areas <strong>of</strong> simulation technology, the models <strong>of</strong> multibody systems (MBS), used to<br />
compute large motions <strong>of</strong> mechanical systems, are continuously improving. In particular, the application<br />
<strong>of</strong> elastic multibody systems (EMBS) has gained much attention in recent years, aiming<br />
at a better prediction <strong>of</strong> the dynamical behavior <strong>of</strong> mechanisms with significant elasticity, such<br />
as light-weight structures.<br />
However, while models are becoming more detailed and more complex, the identification <strong>of</strong><br />
the corresponding model parameters becomes more challenging in equal measure. The identified<br />
parameters may exhibit a high level <strong>of</strong> uncertainty, and exact values for their quantification<br />
can hardly be provided. This non-determinism in numerical models arises as a consequence <strong>of</strong><br />
different sources: natural variability or scatter, which is <strong>of</strong>ten referred to as aleatory uncertainties,<br />
as well as so-called epistemic uncertainties, which arise from a lack <strong>of</strong> information, vagueness in<br />
system definition, or simplification and idealization as it usually appears in modeling procedures<br />
to achieve manageable models. Hence, even apparently well modeled MBS may exhibit inherent<br />
uncertainties due to imprecise data, imperfect knowledge or deficiencies in modeling.<br />
While aleatory uncertainties have successfully been taken into account by the use <strong>of</strong> probability<br />
theory, the additional modeling <strong>of</strong> epistemic uncertainties still remains a challenging topic. As<br />
a practical approach to solve this limitation, a novel methodology to an advanced modeling <strong>of</strong><br />
MBS is presented, which allows for the inclusion <strong>of</strong> uncertainties from the very beginning <strong>of</strong> the<br />
modeling procedure. This approach is based on fuzzy arithmetic, a special field <strong>of</strong> fuzzy set theory,<br />
where the uncertain values <strong>of</strong> the model parameters are represented by so-called fuzzy numbers,<br />
reflecting in a quite intuitive and plausible way the blurred range <strong>of</strong> possible parameter values. As<br />
a result <strong>of</strong> this advanced modeling technique, more comprehensive system models can be derived<br />
which outperform the conventional, crisp-parameterized models by providing simulation results<br />
that reflect both the system dynamics and the effect <strong>of</strong> the uncertainties. Additionally, the special<br />
fuzzy arithmetical approach is able to compute measures <strong>of</strong> influence which quantify the effect<br />
<strong>of</strong> each individual uncertain model parameter on the overall uncertainty <strong>of</strong> the system output.
Section 1: Multi-body dynamics 47<br />
Thus, the dynamical behavior <strong>of</strong> the MBS can be rated with respect to the robustness <strong>of</strong> the<br />
mechanism with respect to uncertainties in the model parameters.<br />
The methodology is illustrated by an exemplary application which reveals that the presented<br />
well-thought-out inclusion <strong>of</strong> presumably limiting uncertainties can provide significant additional<br />
benefit.<br />
Hybrid coordinate approach for the modelling and simulation <strong>of</strong> multibody systems<br />
Christian Becker, Peter Betsch, Marlon Franke, Ralf Siebert (<strong>Universität</strong> Siegen) Schedule<br />
The underlying parametrization in terms <strong>of</strong> applicable coordinates for the description <strong>of</strong> multibody<br />
dynamics influences the structure <strong>of</strong> the governing equations <strong>of</strong> motion and the ensuing numerical<br />
evaluation. Up to now, this fact has led to a rotationless formulation based on direction cosines,<br />
representing the foundation for an energy-momentum consistent time stepping scheme. Next to<br />
exhibiting superior numerical stability properties, this scheme has proven itself by providing an<br />
uniform framework for the implementation <strong>of</strong> multibody systems.<br />
The present work deals with the incorporation <strong>of</strong> an additional angular coordinate into the<br />
aforementioned formulation in the case <strong>of</strong> fast spinning rotationally symmetric bodies. The idea <strong>of</strong><br />
this approach is to achieve higher precision whenever the preferred axis <strong>of</strong> rotation coincides with<br />
the axis <strong>of</strong> symmetry. For this purpose, a distinction has been made between a carried and a bodyfixed<br />
coordinate system, regarding the transition from the initial to the actual body configuration.<br />
Moreover the additional coordinate needs to be enforced by an additional conjugated constraint.<br />
An outstanding characteristic <strong>of</strong> this approach is to which extent the advantageous structure<br />
<strong>of</strong> the underlying differential-algebraic equations is being preserved. To investigate further the<br />
numerical properties <strong>of</strong> this approach, a representative numerical example <strong>of</strong> a spacecraft, equipped<br />
with reaction wheels, will be dealt with.<br />
S1.5: Contact Problems Wed, 16:00–18:00<br />
Chair: Robert Seifried S2|02–C110<br />
The Maxwell-Contact<br />
Kilian Grundl, Thomas Cebulla, Thorsten Schindler, Heinz Ulbrich (TU München) Schedule<br />
Contact models are used to compute contact forces between bodies in multibody systems (MBS).<br />
There are two alternative approaches. The unilateral constraint contact and the unilateral regularized<br />
contact. Both are decoupled contact models, i.e. the contact forces do not depend on other<br />
contacts <strong>of</strong> the MBS.<br />
This work introduces a new contact model, i.e. the Maxwell-Contact, to couple multiple contact<br />
points quasi-statically. Maxwell’s reciprocal theorem is the basis to derive the underlying equations.<br />
It assumes a linear elastic body and states that the deformation at a point i is influenced by<br />
a force at a point j in the same way as the deformation at j is influenced by a force at i. This<br />
influence is expressed with influence coefficients.<br />
The contact model uses several contour pairings, i.e. contact points defined by the kinematics<br />
<strong>of</strong> two contours. These kinematics determine a rigid distance between the two contours. The deformations<br />
<strong>of</strong> both contours depend on all contact forces <strong>of</strong> all contour pairings that are part<br />
<strong>of</strong> the Maxwell-Contact. Regarding all contact points, a linear matrix-vector equation follows. It<br />
expresses the (elastic) distances �g due to the rigid distances �˜g and the contact forces � λ <strong>of</strong> the<br />
single contour pairings:<br />
�g = �˜g + C � λ (1)<br />
where C is the matrix <strong>of</strong> the influence coefficients that couples the contour pairings.
48 Section 1: Multi-body dynamics<br />
The (elastic) distance as well as the contact force <strong>of</strong> each contour pairing is constrained. Both have<br />
to be equal or greater than zero. Furthermore, both have to satisfy a complementarity condition:<br />
a force acts only for distances equal to zero and vice versa the force has to be zero for positive<br />
distances:<br />
�0 ≤ �g ⊥ � λ ≥ �0 (2)<br />
where ≤ and ≥ are used element by element. Equations (1) and (2) build the Maxwell Force Law,<br />
i.e. a linear complementarity problem. The contact forces are its solution. Two solution approaches<br />
are considered. The Lemke algorithm solves the system directly by intelligently testing all possible<br />
solutions. Iterative schemes (e.g. a Newton method) use a reformulated system <strong>of</strong> nonsmooth<br />
equations for the solution. A combination <strong>of</strong> both approaches is used to get a robust solution<br />
process.<br />
The contact model is implemented into the multibody simulation framework MBSim. It is used<br />
in an academic example to validate the fundamental properties, i.e. a variable stiffness and a<br />
coupling <strong>of</strong> the contacts due to the Maxwell-Contact.<br />
Self-excited vibrations <strong>of</strong> deformable multibody systems due to friction: Explanation<br />
with the help <strong>of</strong> two point masses and a belt<br />
Christian Maier, Christoph Glocker (ETH Zürich) Schedule<br />
The aim <strong>of</strong> the present work is the stability analysis <strong>of</strong> a spatial system with 36 degrees <strong>of</strong><br />
freedom done by an eigenvalue analysis. The system consists <strong>of</strong> a cube and a cuboid [1]. Each <strong>of</strong><br />
these blocks is discretised by one finite element. The goal <strong>of</strong> the work is to examine the conditions<br />
under which self-excitation is possible due to friction. In a first step a simplified planar mechanical<br />
system is investigated, which can be solved analytically. It consists <strong>of</strong> two point masses on top <strong>of</strong><br />
a belt, where the belt is moving at a constant velocity. The calculated results are presented in<br />
this paper. The belt system is characterised by three degrees <strong>of</strong> freedom. The belt is horizontally<br />
movable and is furthermore coupled by a spring-damper element to the environment. The point<br />
masses are supported like mathematical pendulas with elastic bars, where elasticity is taken into<br />
account by spring-damper elements. The point masses are connected to each other by again<br />
a spring-damper element. One <strong>of</strong> the point masses is additionally coupled to the environment<br />
by an identical element. The motivation for using the above mentioned coupling elements is to<br />
have the possibility to model visco-elasticity. The contact behaviour between the point masses<br />
and the belt are modelled by Signorini’s law in normal direction and by Coulomb friction in<br />
tangential direction. The friction coefficient is defined to be constant and independent <strong>of</strong> any<br />
relative velocity <strong>of</strong> the contact. The normal contacts between the two point masses and the belt<br />
are closed and remain closed. In order to allow self-excited vibrations caused by friction, additional<br />
constraints for the values <strong>of</strong> the friction coefficient for the belt system are deduced. These results<br />
can be used to explain self-excited vibrations due to friction. Furthermore they are the basis for<br />
additional calculations related to the stability behaviour <strong>of</strong> the spatial model. Finally the results<br />
are compared to those <strong>of</strong> the spatial model [1] and in that context used to be verified.<br />
[1] Ch. Maier, Ch. Glocker. Deformable multibody systems with impacts and Coulomb friciton<br />
Multibody Dynamics 2011 ECCOMAS, Bruxelles 2011.<br />
Structure Preserving Simulation <strong>of</strong> Monopedal Jumping<br />
Michael W. Koch, Sigrid Leyendecker (<strong>Universität</strong> Erlangen-Nürnberg) Schedule
Section 1: Multi-body dynamics 49<br />
This work considers the structure preserving simulation <strong>of</strong> three-dimensional multibody dynamics<br />
with contacts. We use a variational integrator, based on a discrete version <strong>of</strong> the Lagrange-<br />
D’Alembert principle and thus yielding a symplectic-momentum method, for the forward dynamics<br />
simulation. Since one <strong>of</strong> our main goals is structure preservation and geometric correctness,<br />
we have to solve the non-smooth problem including the computation <strong>of</strong> the contact configuration,<br />
time and force instead <strong>of</strong> relying on a smooth approximation <strong>of</strong> the contact problem via a penalty<br />
potential.<br />
In contrast to technically oriented monopedal jumpers, e.g. actuated by extender wheels, the<br />
model <strong>of</strong> a three-dimensional monopedal jumper in use here is inspired by the human locomotor<br />
system. The dynamics <strong>of</strong> the interconnected rigid bodies yields a constrained mechanical systems.<br />
Investigated contact formulations cover the theory <strong>of</strong> perfectly elastic, partly plastic and perfectly<br />
plastic contacts, where the last one means that the foot <strong>of</strong> the jumper stays in contact to the<br />
ground for a certain period <strong>of</strong> time. While the contact stays closed, the discrete equations <strong>of</strong><br />
motion include a contact force and constraints, whose function is to avoid penetration. As soon<br />
as this contact force changes its orientation (meaning that it would prevent the foot from lifting<br />
<strong>of</strong>f the ground), the contact constraints are released. Thus, the last contact configuration and the<br />
contact release time are determined to guarantee a realistic dynamical behaviour.<br />
A Comparison <strong>of</strong> Rolling Contact on Roller-Coaster Rails Between Penalty Methods<br />
and Exact Event-Controlled Impact Detection.<br />
Christian Malessa, Andres Kecskemethy (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
In this paper, two different formulations for the wheel/rail contact problem including clearance<br />
are investigated. The first method, called here the continuous penalty function method, is the<br />
continuous numerical integration, with contact forces arising from step to step as the wheels<br />
penetrate the rails. The second method, termed here the switching penalty function method,<br />
is to register event objects that monitor the distances between wheels and rails in the freefly<br />
phase as well as the impact phase and to stop the integration at the exact time where a<br />
phase changes occurs by a root solver, after which the integrator is re-started with the phases<br />
switched. In the continuous penalty function method, the penetration is computed, and, when<br />
negative, a corresponding repelling force is established according to a spring model (no damping is<br />
considered). In the switching penalty force method, the penetration is registered as a zero-crossing<br />
function within the integration method (in this case we used Lsodar), and, when the function<br />
features a change <strong>of</strong> sign between the start and end values <strong>of</strong> an integration step, a zero-crossing<br />
root finding algorithm is started, which determines the exact time <strong>of</strong> switch condition. Once the<br />
switching time is determined, the integrator is started with the spring contact model, using as<br />
initial condition the integrator variables at the time <strong>of</strong> switching. In contact, the penetration<br />
is registered as a zero-crossing function as well its zero is used for switching back from contact<br />
to free-fly phase. It can be shown that the new proposed switching method keeps the energy<br />
almost constant, whereby the continuous method shows energy dissipation. Due to the energy<br />
comparison, friction and damping has been neglected in the simulation model. A comparison <strong>of</strong><br />
computational time and energy conservation between the two methods showed that the switching<br />
penalty force method not only is clearly more efficient than the continuous penalty force methods,<br />
but also that it is more accurate, as can be seen from the unrealistic energy loss in the continuous<br />
penalty force method, while the switching penalty force method reproduces correctly conservation<br />
<strong>of</strong> energy. Further work will consider friction at the contacts as well as rolling wheel effects, from<br />
which an accurate model for the better understanding <strong>of</strong> vibrations for roller-coaster cars on rails<br />
can be established.
50 Section 1: Multi-body dynamics<br />
S1.6: Numerical Methods Thu, 13:30–15:30<br />
Chair: Peter Betsch S2|02–C110<br />
Spurious oscillations in generalized-α time integration methods<br />
Martin Arnold (<strong>Universität</strong> Halle-Wittenberg), Olivier Brüls (University <strong>of</strong> Liège), Alberto Cardona<br />
(Universidad Nacional Litoral - Conicet, Santa Fe, Argentina) Schedule<br />
Classical ODE and DAE time integration methods from system dynamics have been applied<br />
successfully for more than two decades to constrained systems in multibody dynamics. For large<br />
scale systems, Newmark type integrators are considered to be an interesting alternative in terms<br />
<strong>of</strong> numerical effort and stability. In the present paper we study the time integration <strong>of</strong> constrained<br />
mechanical systems<br />
M(q)¨q = −g(q, ˙q, t) − B ⊤ (q)λ , Φ(q) = 0<br />
by a generalized-α time integration method<br />
with<br />
qn+1 = qn + h ˙qn + (0.5 − β)han + βhan+1<br />
˙qn+1 = ˙qn + (1 − γ)han + γhan+1<br />
(1 − αm)an+1 + αman = (1 − αf)¨qn+1 + αf ¨qn ,<br />
M(qn)¨qn = −g(qn, ˙qn, tn) − B ⊤ (qn)λn , Φ(qn) = 0<br />
and appropriate parameters αf, αm, β, γ, see [1] and the recent extension to constrained systems<br />
in a Lie group setting [2].<br />
The order condition γ = 0.5 + αf − αm guarantees second order convergence in the classical<br />
case as well as for the Lie group integrator [3]. A potential drawback <strong>of</strong> the methods are spurious<br />
transient oscillations <strong>of</strong> the constrained forces that result from an order reduction in the transient<br />
phase. We present a strict mathematical analysis <strong>of</strong> this phenomenon and show how to avoid the<br />
spurious oscillations by perturbed starting values ˙q0, a0.<br />
[1] J. Chung and G. Hulbert: A time integration algorithm for structural dynamics with improved<br />
numerical dissipation: The generalized-α method. ASME Journal <strong>of</strong> Applied Mechanics,<br />
60:371–375, 1993.<br />
[2] O. Brüls and A. Cardona: On the use <strong>of</strong> Lie group time integrators in multibody dynamics.<br />
J. Comput. Nonlinear Dynam., 5:031002, 2010.<br />
[3] O. Brüls, A. Cardona, and M. Arnold: Lie group generalized-α time integration <strong>of</strong> constrained<br />
flexible multibody systems. Mechanism and Machine Theory, in press, 2011. DOI: 10.1016/<br />
j.mechmachtheory.2011.07.017<br />
High-order time integration methods in molecular dynamics<br />
Florian Niederhöfer, Jens Wackerfuß (TU <strong>Darmstadt</strong>) Schedule<br />
The mechanical behaviour <strong>of</strong> molecular structures can be described by a system <strong>of</strong> stiff differential<br />
equations, which can not be solved analytically. Several numerical time integration schemes can<br />
be find in the literature. The aim <strong>of</strong> this talk is to give a survey <strong>of</strong> partitioned Runge-Kutta<br />
methods applied in molecular dynamics. This class <strong>of</strong> methods includes a wide range <strong>of</strong> explicit<br />
and implicit, single- and multi-stage, symplectic and non-symplectic, low- and high-order time
Section 1: Multi-body dynamics 51<br />
integration schemes. Also most <strong>of</strong> the classical methods like explicit and implicit Euler, explicit and<br />
implicit midpoint rule, Störmer-Verlet and Newmark are also partitioned Runge-Kutta methods.<br />
The schemes are implemented in a finite element code which can serve as a numerical plattform<br />
for molecular dynamics [1]. To evaluate the different methods several criteria are formulated and<br />
analyzed. The visualization <strong>of</strong> the simulations is another tool to compare the different methods.<br />
The effectiveness <strong>of</strong> the methods are demonstrated by means <strong>of</strong> several numerical simulations.<br />
[1] Wackerfuß, J., Molecular mechanics in the context <strong>of</strong> the finite element method, International<br />
Journal for Numerical Methods in Engineering, Volume 77, Issue 7, Pages 969-997, 2009<br />
Convergence Study <strong>of</strong> Explicit Co-Simulation Approaches with Respect to Subsystem<br />
Solver Settings<br />
Robert Schmoll, Bernhard Schweizer (<strong>Universität</strong> Kassel) Schedule<br />
Coupling different subsystem simulators can be accomplished by a co-simulation [1]. For this<br />
purpose, the subsystem solvers are coupled by appropriate input and output variables. In order to<br />
analyze the stability <strong>of</strong> the coupled simulation, not only the coupling technique must be taken into<br />
account, but also the subsystem integrators. One the one hand, the stability <strong>of</strong> the co-simulation<br />
is influenced by the extrapolation <strong>of</strong> the coupling variables and the macro-step size. On the other<br />
hand, the numerical errors arising from the subsystem solvers may directly affect the coupled<br />
simulation. The focus <strong>of</strong> this paper lies on the question, how the subsystem solvers influence the<br />
co-simulation. Therefore, numerical studies regarding the numerical stability and the convergence<br />
order have been carried out by using a co-simulation test model [2]. We restrict ourselves to explicit<br />
co-simulation techniques, based on a zero-stable applied-force coupling approach [3]. Furthermore,<br />
stability and convergence are examined for the case that an explicit macro-step size controller is<br />
applied [4].<br />
[1] M. Valasek, Modeling, simulation and control <strong>of</strong> mechatronical systems, in: Simulation Techniques<br />
for Applied Dynamics, CISM Courses and Lectures Vol. 507 (Springer, 2008), 75 -<br />
140.<br />
[2] M. Busch and B. Schweizer, Numerical stability and accuracy <strong>of</strong> different co-simulation techniques:<br />
Analytical investigations based on a 2-d<strong>of</strong> test model, in: The 1st Joint International<br />
Conference on Multibody System Dynamics, (Lappeenranta, Finland, 2010).<br />
[3] R. Kübler and W. Schiehlen, Two Methods <strong>of</strong> Simulator Coupling, Mathematical and Computer<br />
Modelling <strong>of</strong> Dynamical Systems 6 (2000), 93 - 113.<br />
[4] M. Busch and B. Schweizer, An explicit approach for controlling the macro-step size <strong>of</strong> cosimulation<br />
methods, in: 7th European Nonlinear Dynamics Conference, (Rome, Italy, 2011).<br />
Alternative approaches to the incorporation <strong>of</strong> control constraints in multibody dynamics<br />
Yinping Yang, Peter Betsch (<strong>Universität</strong> Siegen) Schedule<br />
Control constraints can be used to prescribe the motion in the inverse dynamics <strong>of</strong> multibody<br />
systems. If the number <strong>of</strong> control inputs is lower than the degrees <strong>of</strong> freedom, this kind <strong>of</strong> mechanical<br />
system is called underactuated system. The solution <strong>of</strong> such partly specified system is a
52 Section 1: Multi-body dynamics<br />
challenging task due to the underactuation property. The description <strong>of</strong> underactuated systems<br />
can be based on either minimal coordinates or redundant coordinates. The resulting governing<br />
equations show the form <strong>of</strong> differential-algebraic equations (DAEs) with a mixed set <strong>of</strong> holonomic<br />
and control constraints. The index <strong>of</strong> the DAEs may exceed three and alternative projection<br />
methods will be applied to reduce the index to three. Numerical examples are used to compare<br />
the alternative projection methods.<br />
A discrete Cosserat rod model taking into account the effect <strong>of</strong> torsion warping<br />
suitable for the dynamic simulation <strong>of</strong> wind turbine rotor blades<br />
Holger Lang (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
In our talk, we present a non-standard discretisation scheme for Cosserat rods. The discrete Cosserat<br />
model is — as the continuum one itself — geometrically exact; in particular, it satisfies<br />
the axiom <strong>of</strong> objectivity: The discrete internal strain measures are invariant with respect to rigid<br />
body motions. The key to receive objectivity is the use <strong>of</strong> finite quotients (instead <strong>of</strong> differences)<br />
in order to discretise the curvature <strong>of</strong> the rod. Finite quotients are obtained naturally, if one uses<br />
quaternions and spherically linear ansatz functions.<br />
In contrast to the standard finite element approach, where the primary unknowns are situated<br />
on the nodes <strong>of</strong> the grid, we use a staggered grid: Here the translatory and rotatory degrees <strong>of</strong><br />
freedom are ordered in an alternating fashion. This ansatz yields a decisive advantage: For the<br />
evaluation <strong>of</strong> the internal shearing energy, it is not necessary to interpolate the rotations onto the<br />
Gauss point within the element.<br />
On the one hand, the right-hand side <strong>of</strong> the equations <strong>of</strong> motion becomes significantly cheaper.<br />
On the other hand — interesting from the numerical point <strong>of</strong> view — the shearing modes and<br />
frequencies <strong>of</strong> the continuum model are approximated consistently. (The latter is not the case for<br />
example, if one uses linear shear flexible rod elements in ABAQUS.)<br />
For the time integration <strong>of</strong> the equations <strong>of</strong> motions, we use integrators that are well established<br />
in multibody dynamics simulation, e.g. DASSL/DASPK or RADAU5. With these, we arrive at<br />
computational times below the real time barrier, if we use the model for the simulation <strong>of</strong> flexible<br />
cables and hoses. The model is nowadays used by the industry in assembly simulations.<br />
If, in addition, one takes into account possible warping <strong>of</strong> the cross sections, e.g. due to<br />
assymetric, open or hollow pr<strong>of</strong>iles, an extended continuous version <strong>of</strong> the Cosserat rod model is<br />
obtained, which exhibits coupling <strong>of</strong> shearing and torsion. Of course, this effect has a considerable<br />
influence on the defection <strong>of</strong> the rod centreline.<br />
An enhancement <strong>of</strong> our discrete model is able to cover these effects for wind turbine rotor<br />
blades up to the accuracy that is required by the manufacturer. For that reason and because <strong>of</strong><br />
its low complexity, the new modified discrete model is well suited for MBS simulations in wind<br />
turbine industry.<br />
S1.7: Applications Thu, 16:00–18:00<br />
Chair: Bernd Simeon S2|02–C110<br />
Modeling and Simulation <strong>of</strong> Ride Dynamics <strong>of</strong> High-Rise Elevators<br />
Michael Beitelschmidt (TU Dresden), Heinz Widmer (Schindler Aufzüge AG Ebikon) Schedule<br />
Elevators in high-rise buildings ascend altitudes <strong>of</strong> several hundred meters and achieve a maximum<br />
velocity <strong>of</strong> more than ten meters per second. During technical development the ride quality<br />
and the safety under extreme load conditions are subject <strong>of</strong> investigation. The numerical simulation<br />
<strong>of</strong> a normal ride <strong>of</strong> the cabin or <strong>of</strong> special load cases is an important assistance for this<br />
issue. The simulation model presented covers the whole movement in riding direction <strong>of</strong> cabin and
Section 1: Multi-body dynamics 53<br />
counterweight, the rotation <strong>of</strong> all pulleys and traction sheaves, vertical movements <strong>of</strong> compensating<br />
pulleys, control <strong>of</strong> electrical drives, and at least the longitudinal movement <strong>of</strong> the ropes.<br />
The elastic conveying ropes <strong>of</strong> high-rise elevators have a weight within the range <strong>of</strong> the cabin or<br />
the counterweight respectively. Therefore, the ropes can be modeled neither as massless springs<br />
nor as rigid bodies. The rope model established in the simulation system makes use <strong>of</strong> the theory<br />
<strong>of</strong> the longitudinal dynamics <strong>of</strong> a onedimensional elastic continuum. Because <strong>of</strong> the change <strong>of</strong><br />
length during ride, a mixed Eulerian-Lagrangian ansatz for the ropes to cover different boundary<br />
conditions at the rope ends is used. Stick-slip <strong>of</strong> the ropes at the contact to the sheaves is included<br />
in the system as well as a simplified model for slack rope which can occur under extreme load<br />
situations. The simulation model is a versatile system implemented in Matlab using its object<br />
oriented programing facilities. The bodies mentioned above and several types <strong>of</strong> force elements<br />
including driving torque control and rheonomic kinematical excitation elements for different purposes<br />
are implemented. All elements have hooks and eyes for their connection to neighboring<br />
elements. This leads to a tree-structured multi-body system topology, which is suitable for any<br />
elevator system. Different elevator system topologies, e.g. simple setups with or without connecting<br />
rope, additional rope systems for overspeed limiting or even more complex setups resembling<br />
block and tackle configurations can be assembled easily. The presentation covers the modeling <strong>of</strong><br />
the systems elements, the compilation to a multibody system using the hookeye logic, numerical<br />
aspects, and simulation results compared to measurements <strong>of</strong> real rides in the hoistway.<br />
A Discrete Element Model for Degradation <strong>of</strong> Ballast Tracks<br />
Christian Ergenzinger, Robert Seifried, Peter Eberhard (<strong>Universität</strong> Stuttgart) Schedule<br />
Track settlement due to degradation <strong>of</strong> ballast is a severe issue in railway operation. The dynamics<br />
<strong>of</strong> trains are frequently modeled using multibody systems. However, the simulation <strong>of</strong> track<br />
dynamics and especially consideration <strong>of</strong> degradation effects such as breakage <strong>of</strong> stones requires<br />
other approaches. The Discrete Element Method, which can be regarded as a special case <strong>of</strong> a<br />
multibody system, is suitable to model these effects. In the Discrete Element Method the system<br />
comprises many thousand rigid bodies, which are <strong>of</strong>ten called particles. The interaction <strong>of</strong> these<br />
particles is governed by unilateral and bilateral penalty forces, respectively.<br />
In this contribution, a model is presented that considers interaction and failure <strong>of</strong> individual<br />
ballast stones. The stones themselves consist <strong>of</strong> breakably bonded particles on a meso-scale. The<br />
granular solid generated by bonding <strong>of</strong> adjacent particles <strong>of</strong> a dense packing is calibrated to<br />
granite, which is a typical material for railway ballast. Uniaxial and confined compression tests<br />
are used to evaluate strength and failure modes. In a second step, a number <strong>of</strong> tangent planes<br />
on ellipsoids <strong>of</strong> appropriate size and aspect ratios are used to define angular ballast stones. The<br />
strength <strong>of</strong> these stones is determined by compression between parallel platens. From statistical<br />
evaluation <strong>of</strong> a number <strong>of</strong> simulations, it is found that based on calibration <strong>of</strong> the material strength<br />
in compression tests, the strength <strong>of</strong> the stones in the model compares well to experimental results<br />
from literature. Finally, aggregates <strong>of</strong> ballast stones are constructed. Strength and failure <strong>of</strong> these<br />
aggregates are assessed in exemplary load cases such as oedometric compression or indentation<br />
<strong>of</strong> a sleeper into a railroad ballast bed.<br />
Influence <strong>of</strong> Internal Actuator Properties <strong>of</strong> Active Anti-Roll Systems on the Vehicle<br />
Driving Behaviour<br />
Thomas Mirwaldt, Manfred Harrer (Dr. Ing. h.c. F. Porsche AG, Weissach), Peter Eberhard<br />
(<strong>Universität</strong> Stuttgart) Schedule<br />
Active anti-roll systems - as part <strong>of</strong> vehicle chassis - are able to adapt their system behaviour to<br />
the current driving situation. It is possible to vary between comfortable or sportive setups. The
54 Section 1: Multi-body dynamics<br />
forces applied to the chassis are determined by ECU-controlled actuators. These ECU includes a<br />
global chassis control which generates set points for an internal actuator feed back control. The<br />
set points are calculated by measured vehicle states.<br />
It has been proven useful to go for a model based design method for the development <strong>of</strong> such<br />
complex systems. This method consists <strong>of</strong> simulation models in combination with system testrig<br />
results. Thus, it is possible to achieve early model based predictions about the pre-designed<br />
system. It also gives basic information for the following control strategy synthesis. Test-rigs are<br />
development tools that achieve objective precise system measurements and whose results are used<br />
to verify the simulation models.<br />
The final system application always takes place in the real car. Typically it consists <strong>of</strong> a<br />
manual parameter adjustment which is based on driver’s subjective criteria. An objective and<br />
efficient way to setup system parameters is given by an implementation <strong>of</strong> numerical optimization<br />
routines. Hence, these routines enable an automated calibration <strong>of</strong> the anti-roll system. The<br />
optimization objectives consist <strong>of</strong> drive comfort criteria as well as factors which describe sportive<br />
driving behaviour. The current states are calculated online from vehicle measurement variables.<br />
With regard to a global vehicle behaviour optimization it is not sufficient to consider global<br />
chassis control parameters only. The dynamic actuator setup and the internal feed back control<br />
set the boundary conditions for the superior body control. The influence <strong>of</strong> these internal actuator<br />
properties on the global chassis control and thus on the vehicle optimization objectives will be<br />
illustrated.<br />
Stability <strong>of</strong> vehicles under nonstationary crosswind excitation<br />
Xiaoyu Zhang, Carsten Proppe (KIT) Schedule<br />
Abstract: Strong crosswind gusts have great influence on the stability <strong>of</strong> railway and road vehicles,<br />
they may lead to accidents and also to a discomfort for the road vehicle driver. Risk assessment<br />
for overturning <strong>of</strong> railway and road vehicles is usually calculated based on the stationary situation<br />
or at least on wind-tunnel experiments that are carried out with a static vehicle model. Nonstationary<br />
excitation due to wind turbulence occurs if the vehicle accelerates or decelerates. Increasing<br />
vehicle speed relative to wind speed will move the energy content in spectrum to a higher frequency<br />
range. It has been realized that nonstationary wind turbulence has a great influence to<br />
vehicles especially when the vehicle speed is high. Thus in order to assess the overturning risk in<br />
a more realistic way, a nonstationary wind model together with its interaction with the vehicle<br />
should be taken into consideration.<br />
This paper proposes a nonstationary turbulence wind model for the investigation <strong>of</strong> crosswind<br />
stability <strong>of</strong> ground vehicles. A wind model with nonstationary turbulence as well as the wind<br />
effects to the moving vehicle in a nonstationary situation (acceleration/deceleration) are described.<br />
Nonstationary aerodynamic forces are considered together with the interaction between the<br />
moving vehicle system and the wind turbulence. Failure probabilities are computed and reliability<br />
analyses are carried out.<br />
Keywords: Vehicles, crosswind stability, nonstationary excitation, reliability analysis.<br />
Zur Wechselwirkung in Elastomerlagern und deren Auswirkung auf das Fahrverhalten<br />
von PKW<br />
Christian Lohse, Matthias Kröger (TU Bergakadmie Freiberg) Schedule<br />
Die Steifigkeit und Dämpfung von Fahrwerkslagern beeinflussen direkt das Fahrverhalten und den<br />
Fahrkomfort. Der Konstrukteur versucht im Entwicklungsprozess die optimale Lösung für den<br />
Zielkonflikt von gutem dynamischen Verhalten inbesondere bei Kurvenfahrt und hohem Kom-
Section 1: Multi-body dynamics 55<br />
fort zu finden. Als Stellgrößen zur Beeinflussung dienen hier die Lagersteifigkeit und -dämpfung,<br />
welche nach den Vorgaben des Lastenheftes für das Bauteil in allen relevanten Beanspruchungsrichtungen<br />
definiert werden. Der Parameter Steifigkeit wird dabei durch die Geometrie ( Form<br />
des enthaltenen Elastomers und die etwaige Verwendung von Zwischenblechen) sowie durch das<br />
verwendete Material beeinflusst. Durch die gezielte Wahl des Werkst<strong>of</strong>fs kann auch die Dämpfung<br />
und somit das Schwingungsverhalten eingestellt werden. Als gängige Größe für die Beschreibung<br />
der Dämpfung hat sich in den letzten Jahren der Verlustwinkel etabliert.<br />
Im Einsatz wird davon ausgegangen, dass die Kennlinien konstant bleiben und keiner Veränderung<br />
unterliegen. Überlagerungen von eingeleiteten Kräften und Momenten beeinflussen jedoch<br />
die Lagersteifigkeit in den einzelnen Raumrichtungen. Diese Kopplungen können durch ein allgemein<br />
gültiges Elastizitätsgesetz beschrieben werden und finden nur in einer vollständigen, für das<br />
Bauteil, spezifischen Steifigkeitsmatrix Berücksichtigung. Die Kenntnis dieser Kopplungen und<br />
die damit verbundenen Änderungen der Steifkeitskennlinien sind für virtuelle Untersuchungen<br />
aus dem Grund der Genauigkeitserhöhung von Simulationen wünschenswert.<br />
In experimentellen Untersuchungen an einem ausgewählten Elastomerlager sind die, für eine FEA<br />
notwendigen, Kennlinien bestimmt worden. Anschließend wurde ein Finite-Elemente-Modell erarbeitet,<br />
das die Bestimmung der Matrizenelemente erlaubt. Für darauf aufbauende Untersuchungen<br />
kam eine, in der Praxis gängige, Mehrkörpersimulationss<strong>of</strong>tware zum Einsatz. Es wurden Untersuchungen<br />
an einem starrkörperbasierenden Zwei-Spur-Fahrzeugmodell mit hohem fahrwerkspezifischen<br />
Detaillierungsgrad durchgeführt, in das elastische Fahrwerkslager, auf Grundlage eines<br />
speziellen Elementtyps, eingebracht wurden.<br />
[1] Heißing B., Ersoy M., Gies S.; Fahrwerkhandbuch; Springerverlag; 2011<br />
[2] Matschinsky W.; Radführung der Straßenfahrzeuge; Springerverlag; 2007<br />
[3] Leister G.; Fahrzeugreifen und Fahrwerkentwicklung; Vieweg Teubner Verlag; 2008<br />
[4] Gross D., Hauger W., Schröder J., Wall. W. A.; <strong>Technische</strong> Mechanik; Springerverlag; 2007<br />
Perspectives on constructive and functional optimizing <strong>of</strong> a serial robot with four<br />
degrees <strong>of</strong> liberty destined for special applications<br />
Petrisor Silviu Mihai, Barsan Ghita (Nicolae Balcescu Land Forces Academy, Sibiu, Romania)<br />
Schedule<br />
Serial-modular robots are mainly built from translation, rotation and orientation modules, prehension<br />
devices and connectors. By differently assembling these modules, various robot architectures<br />
result, adequate to operations within military industrial applications. Modulisation implies<br />
building a number <strong>of</strong> standard modules, common to the same robot family, which, thoroughly<br />
combined, would lead to a variety <strong>of</strong> constructions in terms <strong>of</strong> complexity and application.<br />
With this as a starting point, the authors <strong>of</strong> this paper managed, within the Advanced Logistics<br />
Technologies Laboratory <strong>of</strong> the Nicolae Bălcescu Land Forces Academy from Sibiu, Romania, to<br />
develop a mathematical algorithm, to ideate and design three modules (basic, arm and prehension<br />
device), which, combined and taking into account the actual mechanical application, would result<br />
in the modeling and configuration <strong>of</strong> a TTRT robot.<br />
This paper deals with aspects on the dynamic modulation <strong>of</strong> the robots mechanical structure,<br />
using Langrangian formalism, choosing the adequate DC servomotors, translation modules<br />
constituting the TTRT robot, the constructive solution and modeling the three translation subassemblies<br />
<strong>of</strong> the studied robot, with the intention that, in the end, based on a dynamic-organologic
56 Section 1: Multi-body dynamics<br />
algorithm, a functional optimization <strong>of</strong> the robot be brought out within a workcell destined for<br />
special applications, so that the energetic consumption be as low as possible. This paper also<br />
presents the organological calculi and solutions for the efficient design <strong>of</strong> modules specific to<br />
mechanical structures <strong>of</strong> industrial serial-modular robots.
Section 2: Biomechanics 57<br />
Section 2: Biomechanics<br />
Organizers: Markus Böl (TU Braunschweig), Oliver Röhrle (<strong>Universität</strong> Stuttgart)<br />
S2.1: Multi-Phasic Modelling in Biomechanics Tue, 13:30–15:30<br />
Chair: Tim Ricken S1|03–23<br />
Multiphasic Modelling <strong>of</strong> Human Brain Tissue for Intracranial Drug Infusion Studies<br />
Arndt Wagner, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
A direct intracranial infusion <strong>of</strong> a therapeutic solution into the extra-cellular space <strong>of</strong> human<br />
brain tissue is a promising medical application for the effective treatment <strong>of</strong> malignant brain<br />
tumours [1]. The advantage <strong>of</strong> this method, in comparison with an intra-vascular medication, is<br />
the targeted delivery with a circumvention <strong>of</strong> the blood-brain barrier (BBB), which prohibits the<br />
passing <strong>of</strong> therapeutic macro-molecules across the vascular walls into the brain parenchyma.<br />
The prediction <strong>of</strong> the resulting therapeutic distribution by a numerical simulation is challenging,<br />
since the spreading is affected by the complex nature <strong>of</strong> living brain tissue. Therefore, a macroscopic<br />
continuum-mechanical model is established within the Theory <strong>of</strong> Porous Media (TPM), proceeding<br />
from a homogenisation <strong>of</strong> the underlying micro-structure [2]. The biphasic four-constituent<br />
model consists <strong>of</strong> an elastically deformable solid skeleton (composite <strong>of</strong> tissue cells and vascular<br />
walls), which is perfused by two mobile but separated liquid phases, the blood plasma and the<br />
overall interstitial fluid (treated as a two-component mixture <strong>of</strong> the liquid solvent and the dissolved<br />
therapeutic solute). The strongly coupled solid-liquid-transport problem is simultaneously<br />
approximated in all primary unknowns using mixed finite elements (uppc-formulation) and solved<br />
in a monolithic manner with an implicit time-integration scheme.<br />
This numerical investigation allows the computational study <strong>of</strong> several conditions influencing the<br />
irregular distribution <strong>of</strong> infused drugs, observed in clinical studies. Therefore, the micro-structural<br />
perfusion characteristics in the extra-cellular space <strong>of</strong> the white-matter tracts are considered by a<br />
spatial diversification <strong>of</strong> the anisotropic permeability tensors, provided by Diffusion Tensor Imaging<br />
(DTI). Furthermore, Magnetic Resonance Angiography (MRA) enables the in vivo location<br />
<strong>of</strong> blood vessels within the brain tissue. Finally, the selection <strong>of</strong> appropriate material parameters<br />
has a crucial influence on the drug distribution pr<strong>of</strong>il and further occurring effects beyond.<br />
[1] R.H. Bobo, D.W. Laske, A. Akbasak, P.F. Morrison, R.L. Dedrick, E.H. Oldfield, Convectionenhanced<br />
delivery <strong>of</strong> macromolecules in the brain, PNAS 91 (1994), 2076 – 2080.<br />
[2] A. Wagner, W. Ehlers, Continuum-mechanical analysis <strong>of</strong> human brain tissue, Proc. Appl.<br />
Math. Mech. 10 (2010), 99 – 100.<br />
A Scale Bridging Model For Sinusoidal Liver Perfusion<br />
Daniel Werner, Tim Ricken (TU Dortmund), Uta Dahmen, Olaf Dirsch (<strong>Universität</strong>sklinikum<br />
Jena) Schedule<br />
In this talk we will discuss a three-scale finite element model for sinusoidal liver perfusion. Starting<br />
from the macro-scale we use information about blood pressure and blood flux, gathered and<br />
obtained by our collaborators in T. Preusser’s group from the Fraunh<strong>of</strong>er Institute, as boundary<br />
conditions for our simulation. Regarding the micro-scale, we incorporate a coupled ODE model,<br />
provided by the group <strong>of</strong> H.-G. Holzhütter from the Charité Berlin, to describe the metabolism<br />
in a singular liver cell. The combination <strong>of</strong> the macro- and the micro- scale leads to a coupled
58 Section 2: Biomechanics<br />
multiphase simulation on the meso-scale, which is based on a 2-D model for sinusoidal liver<br />
perfusion [1].<br />
Since the liver is composed <strong>of</strong> a fluid (blood) that flows through a solid biological structure<br />
(tissue), the liver can be described as a multiphase material. Multiphase materials consist <strong>of</strong> two<br />
or more interacting components with strong coupling between solid deformation, fluid pressure,<br />
and fluid flow. Due to the consistent theoretical framework and its proven applicability, the<br />
Theory <strong>of</strong> Porous Media (TPM) is chosen as the underlying framework for this project. After<br />
giving a short motivation and introduction to the TPM, we will present numerical examples to<br />
demonstrate our model’s ability to provide information about stresses, strains, blood flow and<br />
pressure, concentrations, sinusoidal organization, and remodeling from the micro- to macro- scale.<br />
[1] T. Ricken, U. Dahmen, O. Dirsch, A Multiphase Model for remodeling in liver lobes during<br />
resection, Biomechanics and Modeling in Mechanobiology 9 (2010), 435 – 450.<br />
A Biphasic Approach for the Simulation <strong>of</strong> Growth Processes in S<strong>of</strong>t Biological Tissues<br />
Incorporating Damage-Induced Stress S<strong>of</strong>tening<br />
Thomas Schmidt, Daniel Balzani (<strong>Universität</strong> Duisburg-Essen), Tim Ricken, Daniel Werner (TU<br />
Dortmund) Schedule<br />
In the context <strong>of</strong> cardiovascular diseases such as cardiac hypertrophy growth processes play a<br />
predominant role. Myocardial tissues can be characterized as a multiphase material containing<br />
a solid phase which can mechanically be characterized as a fiber-reinforced material, and a fluid<br />
phase which is assumed to transport nutrients required for the growth process. The passive behavior<br />
<strong>of</strong> myocardial tissues shows a strain s<strong>of</strong>tening which is found to be a result <strong>of</strong> microscopic<br />
damage, see [1] and which thus strongly influences the overall mechanical behavior during growth.<br />
In this contribution a multiphase model, cf. [2], is proposed for the simulation <strong>of</strong> growth processes<br />
which occur in myocardial tissues based on the theory <strong>of</strong> porous media. The solid phase is modeled<br />
by applying the approach proposed in [3], which is formulated in terms <strong>of</strong> the concept <strong>of</strong> internal<br />
variables and continuum damage mechanics. The fiber damage is represented by a scalar-valued<br />
damage variable and remanent strains in fiber direction due to supra-physiological loading situations<br />
can be captured. Numerical Examples are given in order to show the performance <strong>of</strong> the<br />
proposed model.<br />
[1] J.L. Emery, J.H. Omens, and A.D. McCulloch: Strain S<strong>of</strong>tening in Rat Left Ventricular<br />
Myocardium, Transactions <strong>of</strong> the ASME - Journal <strong>of</strong> Biomechanical Engineering, 119:6–12,<br />
1997.<br />
[2] T. Ricken and J. Bluhm: Remodeling and Growth <strong>of</strong> Living Tissue - A Multiphase Approach,<br />
Archive <strong>of</strong> Applied Mechanics, 80/5:453-465, 2010.<br />
[3] D. Balzani, S. Brinkhues, and G.A. Holzapfel: Constitutive Framework for the Modeling <strong>of</strong><br />
Damage in Collagenous S<strong>of</strong>t Tissues with Application to Arterial Walls, Computer Methods<br />
in Applied Mechanics and Engineering, submitted.<br />
Towards a Method for Parameter Estimation <strong>of</strong> Articular Cartilage<br />
and a Staggered Procedure for Synovial Fluid-Cartilage Interaction<br />
J<strong>of</strong>frey Mabuma, Bernd Markert, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule
Section 2: Biomechanics 59<br />
Up to now, the interaction mechanisms between cartilage and synovial fluid within diarthrodial<br />
joints are not yet fully understood. These joints are able to function effectively over the lifetime <strong>of</strong><br />
an individualeven under very high loads, which requires minimal wear <strong>of</strong> cartilage. In particular,<br />
the reason for the extremely low coefficients <strong>of</strong> friction has still to be explained.The goal <strong>of</strong><br />
this contribution is to numerically investigate the interaction between articular cartilage and<br />
synovial fluid in diarthrodial joints. In this connection, we already developed an appropriate<br />
continuum model <strong>of</strong> the articulating tissue layers as highly anisotropic [1] and heteregeneously<br />
[3] charged biphasic solid-fluid aggregates based on the Theory <strong>of</strong> Porous Media (TPM) [2]. The<br />
next step is now concerned with the calibration <strong>of</strong> the previously elaborated model. To this<br />
end, a sensitivity analysis is performed to identify the relevant constitutive parameters under<br />
physiological loading conditions. The remaining parameters are then obtained using a direct<br />
search algorithm. In order to solve the complex contact problem at the interface between synovial<br />
fluid and articular cartilage, a sequential solution algorithm is applied, in which the fluid and<br />
cartilage domains are iteratively calculated until equilibrium is reached. The applied staggered<br />
method considers, on the one hand, a synovial fluid flow formulation described by the Reynolds<br />
equation and, on the other hand, the continuum-mechanical description <strong>of</strong> the cartilage layers.<br />
Moreover, the simulations are performed on 3-d hip-joint geometries reconstructed from MRI<br />
data.<br />
[1] Markert B., Ehlers W. & Karajan N.: A general polyconvex strain-energy function for fiberreinforced<br />
materials. Proceedings in Applied Mathematics and Mechanics 5 (2005), 245-246.<br />
[2] Ehlers W., Markert B. & Röhrle O.: Computational continuum biomechanics with application<br />
to swelling media and growth phenomena. <strong>GAMM</strong>-Mitteilungen 32, (2009), 135-156.<br />
[3] Wilson W., Huyghe J. M. and Van Donkelaar C.: A Composition-based cartilage model for the<br />
assessment <strong>of</strong> compositional changes during cartilage damage and adaptation. Biomechanics<br />
and Modeling in Mechanobiology 6 (2007), 43-53.<br />
A biphasic transverse isotropic FEM model for cartilage<br />
Daniel Albrecht, Tim Ricken (TU Dortmund), David M. Pierce (TU Graz), Gerhard A. Holzapfel<br />
(TU Graz; Royal Institute <strong>of</strong> Technology (KTH)) Schedule<br />
In this talk we discuss cartilage, a multi-phase material composed <strong>of</strong> fluids and electrolytes.<br />
From the mechanical point <strong>of</strong> view, cartilage is a porous, incompressible material combined with<br />
transversely isotropic solid and fluid behavior. Moreover, in studying cartilage it is essential to<br />
account for the poro-viscosity <strong>of</strong> the porous matrix as well as material viscoelasticity <strong>of</strong> the<br />
collagen fibers.<br />
In order to describe this complex material, and the resulting mechanical behavior, we propose<br />
a homogenized mixture model based on the theory <strong>of</strong> porous media which allows for a coupled<br />
description <strong>of</strong> the solid-fluid interaction. The transverse isotropic behavior <strong>of</strong> the solid impacts<br />
both the stress response and the internal fluid permeability, which is modeled by using an invariant<br />
formulation <strong>of</strong> the Helmholtz free energy and a transverse isotropic permeability. The latter is<br />
modeled by using an invariant formulation <strong>of</strong> Helmholtz free energy and a transverse isotropic<br />
permeability function. Fluid permeability is further influenced by the inhomogenous, dispersed<br />
fiber fabric <strong>of</strong> the solid and an intrafibrillar portion that can not be „squeezed out“ from the tissue.<br />
The collagen fibers show both a principal orientation distribution within cartilage (superficial,<br />
middle and deep zones are commonly identified) and a local dispersion (the fiber fabric is locally<br />
composed <strong>of</strong> dispersed fibers).
60 Section 2: Biomechanics<br />
Representative numerical examples are shown and compared to experimental data from cartilage<br />
mechanics in the literature.<br />
[1] Pierce, D.M., Ricken, T., Holzapfel, G.A. 2011. A Hyperelastic Biphasic Fiber-Reinforced Model<br />
<strong>of</strong> Articular Cartilage Considering Distributed Collagen Fiber Orientations: Continuum<br />
Basis, Computational Aspects and Applications. In: Computer Methods in Biomechanic and<br />
Biomedical Engineering, submitted for publication<br />
S2.2: Skeletal Muscle Modelling Tue, 16:00–18:00<br />
Chair: Markus Böl S1|03–23<br />
Elastic properties <strong>of</strong> muscle tissue: comparison <strong>of</strong> an inverse finite element approach<br />
and homogeneous deformation<br />
Roland Kruse, Christine Weichert, Markus Böl (TU Braunschweig) Schedule<br />
The passive elastic properties <strong>of</strong> skeletal muscle tissue are important for the simulation <strong>of</strong> surgical<br />
procedures and to find mechanically compatible materials. The parameters <strong>of</strong> a chosen material<br />
model have to be identified by measurements. Two approaches were compared in this study, both<br />
based on compressive tests on cuboid samples <strong>of</strong> the soleus muscle <strong>of</strong> domestic rabbits: On the<br />
one hand, a finite element model <strong>of</strong> the samples has been created using surface shape information<br />
from a three-dimensional camera system and the test, including the friction between the sample<br />
and the sample holder, has been simulated. On the other hand, homogeneous deformation has<br />
been assumed so that the sample could be represented by a single cube with known cross-sectional<br />
area and height, and without friction effects. In both cases, the optimal parameters were deduced<br />
by minimizing the difference between observed and predicted load-deflection curves, for three<br />
orientations <strong>of</strong> the muscle fibers. The results indicate, firstly, that the chosen model is able to<br />
describe the behavior <strong>of</strong> the muscle tissue well, and, secondly, that there can be a quite severe<br />
differences between the two procedures as a consequence <strong>of</strong> the ”homogeneous deformation” assumption.<br />
In conclusion, though the inverse finite element method is very time consuming, it is still<br />
recommended because it better takes into account the experimental conditions and consequently<br />
is expected to yield more realistic parameter estimates.<br />
Numerical investigations <strong>of</strong> muscle contraction by using an optical measurement<br />
technique<br />
Maike Sturmat, Christine Weichert, Tobias Siebert, Markus Böl (TU Braunschweig) Schedule<br />
For a better understanding <strong>of</strong> essential mechanical muscle properties during contraction we proposed<br />
a new approach in this paper by using an optical measurement technique. A method has<br />
been developed to measure the three-dimensional shape during the contraction process. In doing<br />
so, the surface <strong>of</strong> an ex situ isolated rabbit soleus muscle has been coated by a special technology<br />
whereby the optical three-dimensional deforming analysis system was able to detect deformation<br />
changes on the muscle surface. Thus, a three-dimensional geometry model could be reconstructed<br />
for several deformation states. Hence, the region <strong>of</strong> less deformation could be determine as tendon<br />
tissue due to the fact that tendon has certainly a higher stiffness than muscle tissue. The complex<br />
architecture <strong>of</strong> muscle fibres has a huge influence <strong>of</strong> the whole muscle deformation. Therefore,<br />
the fascicle distribution has been taken into account by scanning the muscle via a special manual<br />
digitising technique.<br />
In a second step a recently developed numerical model [1] has been validated by these optical<br />
data for two contraction modes, namely isometric and isotonic. Main idea <strong>of</strong> the numerical model
Section 2: Biomechanics 61<br />
was a non-additive decomposition <strong>of</strong> the free energy function into an active and passive part. The<br />
transversal isotropic muscle behaviour has been described by a hyperelastic constitutive law whereas<br />
the activation could be inserting by a single parameter. The ability <strong>of</strong> the proposed modelling<br />
approach has been shown by three-dimensional numerical experiments.<br />
[1] A. E. Ehret, M. Böl, M. Itskov, A continuum constitutive model fort the active behaviour <strong>of</strong><br />
skeletal muscle, Journal <strong>of</strong> the Mechanics and Physics <strong>of</strong> Solid 59 (2011), 625 – 636.<br />
A neuronal-recruited geometrical model <strong>of</strong> skeletal muscle<br />
Thomas Heidlauf, Oliver Röhrle (<strong>Universität</strong> Stuttgart) Schedule<br />
Mathematical models <strong>of</strong> neurophysiology and continuum biomechanics are combined to include<br />
mechanisms <strong>of</strong> motor unit recruitment and rate coding in a geometrical model <strong>of</strong> skeletal muscle.<br />
Couplings between the models occur at the neuromuscular junction and through afferent sensory<br />
neurons that emerge from muscle spindles.<br />
Neurophysiological models [1] describe how the motoneuron pool in the central nervous system<br />
(CNS) operates as an ensemble to control force. Muscle force production in these models is<br />
based on simple analytical equations that do not involve any spatial components. On the other<br />
hand, continuum-biomechanical models <strong>of</strong> skeletal muscle [2] focus on the generation <strong>of</strong> force.<br />
The biochemical reactions that lead from excitation <strong>of</strong> a muscle fibre to its contraction and force<br />
generation are in continuum models <strong>of</strong>ten described by cellular models <strong>of</strong> systems biology [3].<br />
Geometrical aspects, such as complex fibre architectures or local motor unit distributions, can be<br />
adequately represented in three-dimensional (3D) continuum models.<br />
Various couplings between the models or within the models are required, whereat the individual<br />
models or sub-models are based on different dimensionalities (0D, 1D, and 3D), and different<br />
length and time scales. In this contribution, we demonstrate how such couplings can be efficiently<br />
implemented within a parallel-computing architecture considering the example <strong>of</strong> the open-source<br />
s<strong>of</strong>tware library OpenCMISS [4].<br />
The aim <strong>of</strong> the development <strong>of</strong> such a model is to answer questions <strong>of</strong> neurophysiology that involve<br />
spatial components <strong>of</strong> the muscular system.<br />
[1] J.L. Dideriksen, F. Negro, D. Farina, Motor Unit Recruitment Strategies and Muscle Properties<br />
Determine the Influence <strong>of</strong> Synaptic Noise on Motor Output Variablitlty, submitted.<br />
[2] O. Röhrle, J.B. Davidson, A. Pullan, Bridging scales: a three-dimensional electromechanical<br />
finite element model <strong>of</strong> skeletal muscle, SIAM Journal on Scientific Computing 30 (2008),<br />
2882–2904.<br />
[3] P. Shorten, P. O‘Callaghan, J.B. Davidson, T. Soboleva, A mathematical model <strong>of</strong> fatigue in<br />
skeletal muscle force contraction, Journal <strong>of</strong> Muscle Research and Cell Motility 28 (2007),<br />
293–313.<br />
[4] C. Bradley et al., OpenCMISS: A multi-physics & multi-scale computational infrastructure<br />
for the VPH/Physiome project, Progress in Biophysics and Molecular Biology 107 (2011),<br />
32–47.<br />
Optimal control simulations <strong>of</strong> human arm motion<br />
Ramona Maas, Sigrid Leyendecker (<strong>Universität</strong> Erlangen-Nürnberg) Schedule
62 Section 2: Biomechanics<br />
The simulation <strong>of</strong> ordinary, athletic or pathologic human motion has been in the focus <strong>of</strong> several<br />
investigations for a long time. Simulating such motions usually yields boundary value problems,<br />
like moving the body from a predefined initial to a given final configuration, that can not be<br />
solved via forward dynamics simulation. Furthermore, one has to account for the natural linking<br />
<strong>of</strong> joint movements in a coordinated way which is typical for human motion. This is frequently<br />
treated via linear relations between the single velocities [1].<br />
Another approach is to assume that human movements are optimally controlled by the central<br />
nervous system in the sense that a physiologically motivated cost function is minimised during<br />
the motion [1]. We follow this approach and use a method called DMOCC (Discrete mechanics<br />
and optimal control for constrained systems [2]) to simulate such problems. Since DMOCC is a<br />
structure preserving method, the resulting trajectories are consistent in the evolution <strong>of</strong> momentum<br />
maps and show good energy behaviour.<br />
We apply the method to simulations <strong>of</strong> arm movements, in particular to the simulation <strong>of</strong> steering<br />
(torque or muscle actuated) and extend it to include parameter optimisation to investigate an<br />
optimal steering environment.<br />
[1] J. Friedman and T. Flash. Trajectory <strong>of</strong> the index finger during grasping. Exp. Brain Res<br />
196 (2009), 497-509.<br />
[2] S. Leyendecker, S. Ober-Blöbaum, J.E. Marsden and M. Ortiz. Discrete Mechanics and Optimal<br />
Control for Constrained Systems. Optim Contr Appl Met 31 (2010), 505-528.<br />
Coupling 3D and 1D Skeletal Muscle Models<br />
Michael Sprenger, Oliver Röhrle, Syn Schmitt (<strong>Universität</strong> Stuttgart) Schedule<br />
This work introduces a modelling framework for skeletal muscle mechanics that couples a threedimensional<br />
(3D) continuum-mechanical-based Finite Element (FE) model [1] to a one-dimensional<br />
(1D) lumped-parameter Hill model. In this regard, this is a methodological approach which incorporates<br />
different skeletal muscle models to realise simulations, which are at a present state still<br />
computationally not feasible. The new model framework enables to investigate systems, which<br />
are able to consider both local force distributionwhile incorporating movement patterns <strong>of</strong> (parts<br />
<strong>of</strong>) the musculoskeletal system.<br />
State <strong>of</strong> the art computer models simulating the muscle activities during posture or movement<br />
are based on Multibody Simulations (MBS) incorporating 1D lumped-parameter Hill muscles [2].<br />
Due to the simplicity <strong>of</strong> such models, they cannot account for local and geometrical effects such<br />
as the muscle’s shape, the interaction <strong>of</strong> muscles with its surrounding tissues, local activation<br />
principles, or the muscle fibre distribution. Simulating (parts <strong>of</strong>) the musculoskeletal system with<br />
full 3D continuum-mechanically based skeletal muscle models [1], which can take into account<br />
such structural and functional information, are currently not feasible due to limited computational<br />
power.<br />
Here, we present, based on the upper limp, an overall modelling framework that couples 3D<br />
FE models with MBS. This is justified as geometrical measures, like muscle force direction and<br />
muscle force lever arms, have a strong influence on the mechanical state and movement pattern<br />
in MBS [3]. The coupling is achieved through a nested iteration procedure, where MBS deliver<br />
an initial guess to FE simulations. The FE model improves the physiological reliability <strong>of</strong> MBS<br />
by providing detailed geometrical information.<br />
[1] O. Röhrle, A.J. Pullan, Three-dimensional finite element analysis <strong>of</strong> muscle forces during<br />
mastication, Journal <strong>of</strong> Biomechanics 40 (2007), 3363–3372.
Section 2: Biomechanics 63<br />
[2] M. Günther, H. Ruder, Synthesis <strong>of</strong> two-dimensional human walking: a test <strong>of</strong> the λ-model,<br />
Biological Cybernetics 8 (2003), 89–106.<br />
[3] M. A. Nussbaum, D.B. Chaffin, C. J. Rechtien, Muscle Lines-<strong>of</strong>-Action Affect Predicted<br />
Forces in Optimization-Based Spine Muscle Modeling, Biomechanics 28 (2003), 401–409.<br />
Modeling and Control <strong>of</strong> hair-shaped Vibrissae as biological Sensors<br />
Carsten Behn, Tonia Schmitz, Hartmut Witte, Klaus Zimmermann (TU Ilmenau) Schedule<br />
The reception <strong>of</strong> vibrations is a special sense <strong>of</strong> touch, important for many insects and vertebrates.<br />
Scorpions, cats and rats use a sophisticated sensory systems (sensilla or vibrissae) to acquire tactile<br />
information about their surroundings. Vibrissae, located in the mystacial pad, are either used<br />
passively to sense environmental forces (wind, contact with an obstacle) or actively, when they<br />
are rhythmically moved to scan objects or surfaces. Inspired by this biological sensory system,<br />
several types <strong>of</strong> mechanical models are developed based on ndings in the literature. We present<br />
three models with a stiff rod-like vibrissa, taking into account the viscoelastic support in the<br />
mystacial pad (follicle-sinus complex and skin). The muscles (extrinsic and intrinsic) enabling the<br />
animals to whisk actively are simulated by adaptive control algorithms. Numerical simulations<br />
with chosen perturbation forces show that specic control variables contain adequate information<br />
on the force to be identied. All models represent a single vibrissa <strong>of</strong> the mystacial pad, we do not<br />
model a field <strong>of</strong> vibrissae. Therefore, these models can be transferred to model a carpal vibrissa,<br />
too.<br />
S2.3: General Biomechanics Wed, 13:30–15:30<br />
Chair: Arndt Wagner S1|03–23<br />
Model-based therapy - new methods <strong>of</strong> model reduction for non-linar mechanics<br />
Annika Radermacher, Stefanie Reese (RWTH Aachen) Schedule<br />
The constantly rising requirements for simulations <strong>of</strong> biomechanical problems yield numerical<br />
models with increasing number <strong>of</strong> degrees-<strong>of</strong>-freedom. Due to significant nonlinearity computational<br />
effort increases constantly. Simulations which serve for surgery training or online support<br />
demand minimal computational time possibly even in real time. A real time simulation without<br />
a significant loss <strong>of</strong> accuracy would be very valuable. To achieve this and to minimize the computational<br />
effort model reduction is needed. The Functional Endoscopic Sinus Surgery (FESS) is a<br />
minimally invasive surgery, which removes blockage from the nasal cavity. A training program or<br />
an online support would help the surgeon by supplying import data like stress and displacements<br />
during the process. We can generally differentiate between two ways <strong>of</strong> model reduction methods:<br />
the singular value decomposition (SVD)-based methods and the Krylov-based methods. These<br />
methods were developed and are widely used for solving linear problems. There exist concepts to<br />
expand these methods to nonlinear problems. A general method for model reduction in nonlinear<br />
solid mechanics, in particular, is not available yet. This contribution discusses the performance<br />
and efficiency <strong>of</strong> three SVD-based methods for nonlinear structuralproblems: the modal basis, the<br />
load dependent Ritz and the proper orthogonal decomposition (POD) method. A complex biomechanical<br />
model with nonlinear behavior will be investigated. It turns out that the performance<br />
<strong>of</strong> the POD is very promising. It significantly reduces the effort within a good agreement to the<br />
unreduced results.
64 Section 2: Biomechanics<br />
Modelling and simulation <strong>of</strong> injecting acrylic bone cement into osteoportic vertebral<br />
bones within percutaneous vertebroplasty<br />
Sebastian Kolmeder, Alexander Lion (<strong>Universität</strong> der Bundeswehr München), Ralf Landgraf, Jörn<br />
Ihlemann (TU Chemnitz) Schedule<br />
According to the world health organisation osteoporosis is among the most important diseases<br />
worldwide. People affected by osteoporosis <strong>of</strong>ten suffer from severe back pain and fractured vertebral<br />
bones due to decreasing bone density. Vertebroplasty is a common clinical procedure, whereat<br />
osteoporotic vertebral bones are stabilised by means <strong>of</strong> an acrylic glue called bone cement. Therefore<br />
initially liquid bone cement is injected through a biopsy needle into the porous vertebral<br />
bone. The cement penetrates the cavities, cures by an exothermal polymerisation and strengthens<br />
the vertebral body within the spinal column [1]. However, this operation technique is accompanied<br />
by risks like cement leakage and heat necrosis as well as long term load redistribution in the<br />
spinal column [2].<br />
In order to obtain a better physical understanding <strong>of</strong> the process <strong>of</strong> vertebroplasty and to reduce<br />
the complications, a detailed thermomechanical-chemical coupled material model <strong>of</strong> acrylic bone<br />
cement has been developed [3]. The flow behaviour <strong>of</strong> bone cement is modelled incompressible<br />
and purely viscous but depending on shear rate and temperature. An evolving internal state<br />
variable is used to represent the dissolution <strong>of</strong> liquid monomer within polymer powder, the two<br />
initial components <strong>of</strong> bone cement. This temperature dependent dissolution also effects the viscosity.<br />
Moreover, the heat transfer equation <strong>of</strong> the model includes temperature dependent material<br />
properties, such as specific heat capacity and thermal conductivity. Based on an extended experimental<br />
data pool the developed model is adapted and parameterised.<br />
For true in detail simulations an accurate geometrical model is indispensable. To this end a human<br />
vertebral body, affected by osteoporosis, was scanned by a micro CT apparatus and further<br />
converted to a surface tesselation language file, which can be processed by standard meshing tools.<br />
The open source CFD toolbox OpenFOAM was chosen to handle this injection simulation task,<br />
because <strong>of</strong> free accessibility <strong>of</strong> the program code and its sophisticated meshing tool. To implement<br />
the described material model, the volume <strong>of</strong> fluid solver interFoam was used as a foundation<br />
and extended by a heat transfer equation and a transport and evolution equation regarding the<br />
dissolution process.<br />
Having accomplished the injection simulation, the distribution <strong>of</strong> bone cement within the geometry,<br />
i.e. the vertebral body and the temperature field can be passed to a finite element simulation,<br />
that takes into account the internal stresses and temperature field during the main curing process.<br />
First results encourage the objective <strong>of</strong> simulating the procedure <strong>of</strong> vertebroplasty in detail, but<br />
<strong>of</strong> course have to be validated.<br />
ACKNOWLEDGEMENTS: The authors would like to thank Pr<strong>of</strong>. Dr. Cornelia Kober and Helena<br />
Lebsack from HAW Hamburg as well as Pr<strong>of</strong>. Dr. med. Thomas R. Blattert from OFK Schwarzach<br />
for making geometric data available. This research project is funded by the German Research<br />
Foundation (DFG).<br />
[1] M. E. Jensen, A. J. Evans, J. M. Mathis, D. F. Kallmes, H. J. Cl<strong>of</strong>t, J. E. Dion, Percutaneous<br />
polymethylmethacrylate vertebroplasty in the treatment <strong>of</strong> osteoporotic vertebral<br />
body compression fractures: technical aspects, Am. J. Neuroradiol 18 (1997), 1897 – 1904.<br />
[2] P.F. Heini, U. Berlemann, M. Kaufmann, K. Lippuner, C. Fankhauser, P. v. Landuyt, Augmentation<br />
<strong>of</strong> mechanical properties in osteoporotic vertebral bones: a biomechanical investigation<br />
<strong>of</strong> vertebroplasty with different bone cements Eur Spine J. 10 (2001), 164 –
Section 2: Biomechanics 65<br />
171.<br />
[3] S. Kolmeder, A. Lion, R. Landgraf, J. Ihlemann, Thermophysical properties and material<br />
modelling <strong>of</strong> acrylic bone cements used in vertebroplasty, J. Therm Anal Calorim 105<br />
(2011), 705 – 718.<br />
Marker based in-vivo analysis <strong>of</strong> 3D spinal motion during gait using spline curves<br />
Dietmar Rosenthal, Andres Kecskeméthy (<strong>Universität</strong> Duisburg-Essen), Harald Hefter (<strong>Universität</strong>sklinikum<br />
Düsseldorf), Alejandro A. Espinoza Orias, Gunnar Andersson, Markus A. Wimmer<br />
(Rush University Medical Center, Chicago, IL) Schedule<br />
We propose a numerical framework for the fitting <strong>of</strong> a 3D spline curve model to measured marker<br />
positions that is less sensitive to skin artifacts. We consider for this a quintic B-spline curve<br />
representation <strong>of</strong> the posterior vertebral line<br />
r(u) =<br />
nS�<br />
ciNi,5(u) (1)<br />
i=0<br />
with control points ci and normalized quintic basis functions Ni,5 corresponding to a specific knot<br />
vector û, see [2]. The curve is related to a set <strong>of</strong> nM measured skin markers Mj by introducing<br />
movable ’sliders’ Sj with a perpendicular lever <strong>of</strong> fixed length dj attached to the curve. The sliders<br />
are allowed to move along and around the curve to account for skin motion. Let s denote the arclength<br />
parameter <strong>of</strong> a curve. The fitting result is given as the curve minimizing the deformation<br />
energy functional, defined as the elastic energy stored between a given reference curve rref(s) and<br />
the sought curve r(s):<br />
�<br />
f(c0, ..., cnS ) = kκ(s)(κref(s) − κ(s)) 2 �<br />
ds + kτ(s)(τ ∗ ref(s) − τ ∗ (s)) 2 ds (2)<br />
Ω<br />
such that (a) the tips <strong>of</strong> the sliders Sj, � Mj coincide with the measured positions Mj and (b) the<br />
curve length agrees with subject anatomy. In (2), κ denotes Euclidian curvature and<br />
Ω<br />
τ ∗ (s) = (1 − exp(−||r ′ (s) × r ′′ (s)|| 4 ) · τ(s) (3)<br />
denotes the modified torsion with Frenet-Serret torsion τ associated to r(s) and rref(s). The scalar<br />
functions kκ(s) and kτ(s) in (2) define the local stiffness properties along the curve, modeled as<br />
splines with the same parameter domain Ω as r. Some sample evaluations are compared with<br />
published results.<br />
[1] Berthonnaud, E.; Fougier, P.; Hilmi, R.; Labelle, H.; Dimnet, J.: Relationship Between Sagittal<br />
Spinal Curves and Back Surface Pr<strong>of</strong>iles Obtained With Radiographs. Journal <strong>of</strong><br />
Mechanics in Medicine and Biology, Vol. 10, No. 2,pp. 313–325, 2010.<br />
[2] De Boor, C.: A Practical Guide to Splines. New York: Springer, 2001.<br />
Study <strong>of</strong> the biomechanical behaviour <strong>of</strong> structurally stable/unstable motion segments<br />
<strong>of</strong> the sheep spine<br />
Strampe M, St<strong>of</strong>fel M, Weichert D (RWTH Aachen), Sellei R, Pape H-C (<strong>Universität</strong>sklinikum<br />
Aachen) Schedule
66 Section 2: Biomechanics<br />
The effects <strong>of</strong> damage <strong>of</strong> intervertebral discs on their biomechanical behaviour and the factors<br />
favouring the progression <strong>of</strong> instability are studied. Healthy and damaged movement segments<br />
are analyzed experimentally and numerically. The aim is to represent and predict the effects <strong>of</strong><br />
tissue damage and changes in the spine by comparison with healthy segments. Since the intervertebral<br />
disc acts as a mechanical damper, relaxation tests are performed in addition to pressure<br />
experiments. The experiments are carried out in a bioreactor with tempered nutrient solution.<br />
A cultivation period in the bioreactor allows detecting cell viability, solute diffusion rates and<br />
gene expression <strong>of</strong> the discs. Numerically, the nonlinear, viscoelastic, anisotropic and diffusiondependent<br />
behaviour <strong>of</strong> the intervertebral disc is modelled with the FE-program Abaqus, using<br />
a modular material law as a UMAT subroutine. With the measurement results, the relevant<br />
parameters can be determined so that the mechanical behaviour <strong>of</strong> intervertebral discs can be<br />
simulated.<br />
3D Analysis <strong>of</strong> Stresses within Molars during Natural Clenching<br />
Harnoor Saini, Oliver Röhrle (<strong>Universität</strong> Stuttgart) Schedule<br />
Teeth are subjected to some <strong>of</strong> the highest physiological loads during clenching and biting. The<br />
highest loads occur in the region about the first molars [1]. Clinically, this is reflected by the higher<br />
incidence <strong>of</strong> cuspal-fractures in posterior teeth, more specifically at the maxillary and mandibular<br />
first molars [2]. Cuspal-fractures <strong>of</strong> natural and restored teeth cause a significant amount <strong>of</strong> nonrestorable<br />
tooth damage [3], which subsequently require complete dental implantation. Analysis<br />
<strong>of</strong> internal stresses and strains within molars, can provide insight into designing more robust<br />
dental implants. Currently, stress analyses have not implemented a combination <strong>of</strong> 3D geometric<br />
descriptions with naturally captured masticatory movements.<br />
The aim <strong>of</strong> this study is to analyse internal stresses and strains in mandibular and maxillary<br />
molars during natural masticatory movements, which were recorded with 6 degrees <strong>of</strong> freedom.<br />
The investigation was performed by simulating a real world clenching experiment via the use <strong>of</strong> a<br />
quasi-static FE model, implemented in a commercially available FE-s<strong>of</strong>tware. Three-dimensional<br />
models <strong>of</strong> the opposing first and second molars were generated along with a model <strong>of</strong> the rubber<br />
piece used in the real world experiment. In the first step, teeth were taken as rigid and rubber<br />
as hyperelastic. Captured clenching movements were then applied to the mandibular molars, and<br />
contact pressures calculated at each time increment. In a second step, assuming no dissipation<br />
<strong>of</strong> energy, the contact pressures will be applied as boundary conditions to the now deformable<br />
maxillary and mandibular molars. The resulting internal stress and strain distributions should<br />
provide insight into the deformation behavior <strong>of</strong> the molars during clenching.<br />
[1] Bates JF, Stafford GD, Harrison A. Masticatory function – a review <strong>of</strong> the literature. J Oral<br />
Rehabil 2 (1975), 281-301.<br />
[2] Bader JD, Martin JA, Shugars DA. Incidence rates for complete cusp fracture. Community<br />
Dent Oral Epidemiol 29 (2001), 346-353.<br />
[3] McDaniel RJ, Davis RD, Murchison DF, Cohen RB. Causes <strong>of</strong> failure among cuspal-coverage<br />
amalgam restorations: a clinical survey. J Am Dent Assoc 131 (2000), 173-177.<br />
S2.4: Modelling Vibrations <strong>of</strong> Tools Wed, 16:00–18:00<br />
Chair: Roland Kruse S1|03–23
Section 2: Biomechanics 67<br />
Vibrations action <strong>of</strong> the trilling machine MA750 on the human operator hand<br />
Mariana Arghir, Mariana Rus, Sorin Constantin Macovescu (Technical University <strong>of</strong> Cluj-<br />
Napoca) Schedule<br />
Work includes identifying and analyzing vibrations produced by a trilling machine within space<br />
work. To identify vibration is used a special method, which has not been used so far in identifying<br />
vibrations, with the action on the human body. For obtaining a very good identification <strong>of</strong><br />
the human body vibrations has been used the Moiré projection method. General conditions were<br />
applied human hand operator during working hours on a trilling machine, with different speeds<br />
<strong>of</strong> main shaft. Human operator has been informed <strong>of</strong> action risks vibration on his hand and he<br />
has accepted experiment. In the paper are presented successively two methods <strong>of</strong> measuring <strong>of</strong><br />
the vibrations: the Moiré projection method and conventional method <strong>of</strong> measuring with the vibrometer.<br />
Because Moiré projection method was not used until this moment from the another<br />
researchers for the human body vibrations, was necessary to realize the calibration <strong>of</strong> the method<br />
with an experimental device made by the authors <strong>of</strong> this paper. The successive operations for<br />
applying this method were possible using a signal generator, an amplificatory device <strong>of</strong> the signal,<br />
a system <strong>of</strong> illumination, a computer having a corresponding s<strong>of</strong>tware for the analyzing the databases<br />
<strong>of</strong> the results. The Moiré projection method used human operator during processing parts<br />
on the trilling machine has gave results comparable to conventional method <strong>of</strong> measuring using<br />
a vibrometer with three-axial accelerometer. The results in the both situation were in the same<br />
order <strong>of</strong> unit scale, and in this situation the optical method named Moiré projection method can<br />
be considered a valid method for the human vibrations measurements without surface taste. The<br />
Moiré projection method can be used to the vibrations measurement with success because this is<br />
a method without contact.<br />
[1] Borza, Dan, Nicolae, Mechanical vibration measurement by high-resolution time-averaged<br />
digital holography, Measurement Science & Technology, vol. 16, No. 9, Pages 1853-1864,<br />
ISSN: 0957-0233, 2005.<br />
[2] Borza, Dan, Nicolae, Evolutions in Full-field Optoelectronic Coherent Metrology as Applied<br />
in Numerical Model Validation, Microscopy and Vibroacoustics, Automation, Quality and<br />
Testing, Robotics, IEEE International Conference on Volume 2, Pages: 99 104, Cluj-Napoca,<br />
Romania, 2006.<br />
[3] Runcan, Mariana, Arghir, Mariana, La technique Moiré de projection, Acta Technica Napocensis,<br />
Series: Applied Mathematics and Mechanics, Vol. IV, Nr. 51, pag. 117-120, ISSN:<br />
1221-5872, Cluj-Napoca, 2008.<br />
Vibrating Portable Machine-Tools Acting on Human Operator<br />
Anamaria Gligor, Alina-Sabina Țepeş-Bobescu, Mariana Arghir (Technical University <strong>of</strong> Cluj-<br />
Napoca) Schedule<br />
This paper is designed to be an information to the public about the importance <strong>of</strong> vibration<br />
action <strong>of</strong> portable machine-tools on the human body and particularly on the hand-arm system.<br />
Mechanical vibrations are non-periodic motions <strong>of</strong> a material system around a static or dynamic<br />
equilibrium position. Generally in the production <strong>of</strong> vibrations interfere forces <strong>of</strong> inertia (seeking<br />
to bring the mobile in static or dynamic equilibrium position), elastic forces, resistance forces<br />
(given by friction and can be an outside or inside force for the system) and disturbing forces<br />
(acting from the outside and maintaining oscillatory motion). An excessive exposure to vibration<br />
can cause blood circulation disorders in hands (ex: Reynauds phenomenon), the alteration <strong>of</strong>
68 Section 2: Biomechanics<br />
the neurological and musculoskeletal functions <strong>of</strong> the hands and arms (carpal tunnel syndrom).<br />
Machine tools in operation expose those who use them to mechanical vibrations transmitted by<br />
hand this affects the comfort, efficiency and in some cases the security <strong>of</strong> the human operator.<br />
Exposure to vibration can vary widely from one operation to another, due to the use <strong>of</strong> different<br />
machines or powered tools or because <strong>of</strong> different operating modes <strong>of</strong> a powered tool or a machine<br />
and this paper is mainly aimed to do a comparison between different vibrating powered tools.<br />
Exposure to harmful vibrations can lead to health problems and disorders, especially in the upper<br />
joints and dorsal region <strong>of</strong> the human body. A detailed understanding <strong>of</strong> the undesirable effects <strong>of</strong><br />
vibration on the human body is essential to achieve administrative and technical prevention. In<br />
modern times, vibration studies become more frequent, decisive for the many machines, vehicles,<br />
construction.<br />
[1] SR EN ISO 5349-1, Mechanical vibration. Measurement and evaluation <strong>of</strong> human exposure<br />
to vibration through hand. Part 1: General requirements. 2003.<br />
[2] SR EN ISO 5349-2, Mechanical vibration. Measurement and evaluation <strong>of</strong> human exposure<br />
to vibration through hand. Part 2: Practical guidance for measurement at the workplace.<br />
2003.<br />
[3] SR ISO 2631 -1, Mechanical vibration and shock. Assessment <strong>of</strong> human exposure to wholebody<br />
vibration. Part 1: General requirements.<br />
[4] Harris, C., M., Harris’ shock and vibration handbook, ISBN: 0-07-137081-1, 2002.<br />
The Study <strong>of</strong> Psychoacoustic Effects <strong>of</strong> Noise Emitted by the Machine Tools Structure<br />
Alina-Sabina Țepeş-Bobescu, Florin Țepeş-Bobescu, Anamaria Gligor, Mariana Arghir (Technical<br />
University <strong>of</strong> Cluj-Napoca) Schedule<br />
Cause-effect relationship between noise and hearing loss is considered relevant to human health in<br />
the workplace. Psychoacoustics can be described as the study <strong>of</strong> how people react to sound, hearing<br />
and perception. Any noise problem may be described in terms <strong>of</strong> a sound source, a transmission<br />
path and a receiver. If complaints arise from the work place, then regulations should be satisfied,<br />
but to minimize hearing damage compensation claims, the goal <strong>of</strong> any noise-control program<br />
should be to reach a level <strong>of</strong> no more than 85 dB(A) [1]. By [5], specific occupational noise effects<br />
are hearing loss and deafness. Occupational hearing loss represents permanent decrease in hearing<br />
threshold at a frequency <strong>of</strong> 4000 Hz, including more than 30 dB, type <strong>of</strong> perception, generally<br />
bilateral and symmetric, without involving conversational frequencies. Occupational deafness is<br />
based on a permanent hearing loss at low conversational frequencies, the arithmetic mean <strong>of</strong> the<br />
three frequencies deficits exceeding 25dB. This paper provides ways for the prediction <strong>of</strong> noise<br />
radiated by the single part structure <strong>of</strong> the machine-tool using vibration measurement and an<br />
estimation method for the hearing deterioration or hearing impaired individual people. There are<br />
the following conclusions: noise and vibration have a close physical relationship; noise induced<br />
permanent threshold shift values depending on frequencies, exposure time, the noise exposure<br />
level, LEX,8h; exposure time <strong>of</strong> noise is longer even the risk <strong>of</strong> hearing impairment is greater.<br />
[1] Mariana, Arghir, ş.a., Monitorizarea zgomotului traficului rutier, EDP, 644 pag., ISBN 978-<br />
973-30-2314-2, Bucureşti, 2008<br />
[2] SR ISO/TR 7849:1995 Acoustics- Estimation <strong>of</strong> airborne noise emitted by machinery using<br />
vibration measurement
Section 2: Biomechanics 69<br />
[3] STAS 1999:1996 Acoustics-Determination <strong>of</strong> occupational noise exposure and estimation <strong>of</strong><br />
noise induced hearing impairment<br />
[4] ***www.scribd.com/doc/29247889/7-Bioacustica-MG<br />
S2.5: Growth and Remodelling I Thu, 13:30–15:30<br />
Chair: Ellen Kuhl S1|03–175<br />
A network model for the EPS matrix <strong>of</strong> microbial bi<strong>of</strong>ilms<br />
Alexander E. Ehret, Antonio Bolea Albero, Markus Böl (TU Braunschweig) Schedule<br />
Microbial bi<strong>of</strong>ilms exist on a multitude <strong>of</strong> surfaces and interfaces. While some <strong>of</strong> these bacterial<br />
colonies play vital roles for human health and ecology, others pose severe health risks and cause<br />
large problems in industrial processes [1-3]. Generally, a bi<strong>of</strong>ilm is considered as immobilised cells<br />
which are embedded in a matrix <strong>of</strong> extracellular polymeric substances (EPS) produced by these<br />
cells themselves [1,3]. Although not the only possible component <strong>of</strong> EPS, many bi<strong>of</strong>ilms contain<br />
highly hydrated gel-forming polysaccharide networks [4].<br />
In the present contribution, the latter characteristic is exploited in order to model the mechanical<br />
behaviour displayed by microbial bi<strong>of</strong>ilms. As a particular example, the relatively well<br />
explored networks formed by bacterial alginates are considered. The polysaccharide molecules<br />
are represented by worm-like chains and incorporated into a suitable network description. The<br />
effects <strong>of</strong> crosslinking and swelling on the mechanical behaviour <strong>of</strong> this polysaccharide network<br />
are studied. Finally, the model is discussed in comparison with recent rheological and stress-strain<br />
data <strong>of</strong> bi<strong>of</strong>ilms.<br />
[1] W.G. Characklis, K.C. Marshall, Bi<strong>of</strong>ilms: A basis for an interdisciplinary approach, in: W.G.<br />
Characklis, K.C. Marshall (eds.) Bi<strong>of</strong>ilms, John Wiley & Sons, New York (1990), pp. 3 –<br />
15.<br />
[2] H.-C. Flemming, J. Wingender, Bi<strong>of</strong>ilme – die bevorzugte Lebensform der Bakterien, Biologie<br />
in unserer Zeit 31 (2001), 169 – 180.<br />
[3] R.M. Donlan, J.W. Costerton, Bi<strong>of</strong>ilms: Survival Mechanisms <strong>of</strong> Clinically Relevant Microorganisms,<br />
Clin. Microbiol. Rev. 15 (2002), 167 – 193.<br />
[4] H.-C. Flemming, J. Wingender, The bi<strong>of</strong>ilm matrix, Nat. Rev. Microbiol. 8 (2010), 623 – 633.<br />
Theoretical and experimental investigation <strong>of</strong> cartilage replacement material for medical<br />
applications<br />
Bei Zhou, Marcus St<strong>of</strong>fel, Dieter Weichert, Björn Rath (RWTH Aachen) Schedule<br />
S<strong>of</strong>t tissues are commonly applied in surgery to replace the injured articular cartilage. Many<br />
biological researches were carried out through mechanical and histological experiments. They<br />
focus on the function, degeneration and regeneration <strong>of</strong> the articular cartilage and fibrocartilage.<br />
In the present work a theoretical material model, which takes elasticity and deformation dependent<br />
diffusion into account, is proposed to identify the mechanical properties <strong>of</strong> s<strong>of</strong>t tissues during the<br />
remodeling process. This approach includes experimental investigation <strong>of</strong> the s<strong>of</strong>t tissue implants<br />
and numerical simulation. Through simulating the stress-relaxation response <strong>of</strong> materials under
70 Section 2: Biomechanics<br />
unconfined compression by means <strong>of</strong> finite element method based on an optimization algorithm,<br />
material parameters can be identified. For a widely application, this material model was validated<br />
with different experimental method, specimens with different dimensions and different kinds <strong>of</strong><br />
s<strong>of</strong>t tissues.<br />
Mechanical modeling <strong>of</strong> medical mesh implants at the meso-scale<br />
Barbara Röhrnbauer, Gerald Kress, Edoardo Mazza (ETH Zürich) Schedule<br />
The present study aims at developing a physically based mechanical model for medical mesh<br />
implants at the mesoscale. Medical mesh implants are knitted two-dimensional fiber-networks<br />
used for s<strong>of</strong>t body tissue support, such as in case <strong>of</strong> a prolapse. At the mesoscale, the geometry<br />
and the local kinematics <strong>of</strong> a representative unit cell are mapped in an abstracted, but still<br />
physically relevant description. Such a model allows to understand the interplay between local<br />
deformation patterns and the resulting global anisotropic and nonlinear force response. It is<br />
expected to provide design criteria for mesh implant optimization, not only accounting for the<br />
global mechanical behavior but also for local mesh-tissue interactions.<br />
A representative unit cell is modeled as a 20 degree <strong>of</strong> freedom system based on multi-body<br />
theory. It is composed <strong>of</strong> discrete force elements, such as translational and rotational springs.<br />
The system equations are the projected Newton-Euler equations, reducing for the static case to<br />
a simple equilibrium <strong>of</strong> active forces and constraint forces. There are 21 parameters to adjust the<br />
force laws <strong>of</strong> the whole model. These parameters can be related to the mechanical behavior <strong>of</strong><br />
single elements at the micro-scale, involving stretching and bending <strong>of</strong> filaments. An experimental<br />
study has been conducted subjecting the dry mesh to cyclic load cases <strong>of</strong> uniaxial stress and<br />
uniaxial strain respectively, in four different loading directions.<br />
Single sets <strong>of</strong> parameters can be found simulating the global force and kinematic response <strong>of</strong><br />
all eight experimental load cases in an appropriate way. Moreover, preconditioning effects, i.e. an<br />
alteration <strong>of</strong> the force response due to cyclic loading are adequately described based on an altered<br />
reference configuration. Preconditioning <strong>of</strong> the meshes is thus interpreted as a mainly geometry<br />
related phenomenon, caused by a load history dependent inelastic deformation <strong>of</strong> each unit cell.<br />
Analysis at different length scales allows to link macroscale phenomena <strong>of</strong> mesh implants to<br />
mechanical contributions <strong>of</strong> single elements at the mesoscale. With respect to mesh design control,<br />
the mechanical properties <strong>of</strong> these elements have to be translated to material and structural<br />
properties at the microscale, such as filament material and diameter or knitting pattern.<br />
Red Blood Cell Shape Transformations<br />
Stefan Wolf, Justyna Czerwinska (ARTORG Center, <strong>Universität</strong> Bern) Schedule<br />
Several red blood cell (RBC) diseases such as sickle cell anaemia and spherocytosis are related<br />
to the shape and the deformability <strong>of</strong> RBCs. Furthermore, it has been reported that RBC ageing<br />
is connected to stiffening and the loss <strong>of</strong> volume and area. The vesicles acquire shapes for which<br />
appropriate constraints are minimal. The global energy <strong>of</strong> a vesicle shape is related to osmotic<br />
pressure, lipid densities, constraints on the area, the volume and the area-difference in elasticity.<br />
Several energy models [1] were studied for the evolution <strong>of</strong> the vesicle curvature such as: the minimal<br />
local curvature, the spontaneous curvature, the bilayer couple, the area-difference-elasticity<br />
and their combinations.<br />
The information about the shape <strong>of</strong> the lowest energy for given parameters can be obtained<br />
by solving the Euler-Lagrange equations or by using trail shapes which could be obtained by numerical<br />
simulations. For that purpose we have used the finite element simulations. The different<br />
red blood cell shapes can then be grouped in the phase space diagram and we plot the trajectories<br />
related to the deformation <strong>of</strong> the different shapes . Furthermore, the effect <strong>of</strong> the different
Section 2: Biomechanics 71<br />
energy models on the phase space trajectories is analysed. These results are compared with the<br />
experimental data for optical tweezers stretching [2,3].<br />
[1] U. Seifert, Configurations <strong>of</strong> Fluid Membranes and Vesicles, Adv. Phys. 46 (1997), 13 – 137.<br />
[2] M. Dao, C.T. Lim, S. Suresh , Mechanics <strong>of</strong> the Human Red Blood Cell Deformed by Optical<br />
Tweezers, J. Mech. Phys. Solids. 51 (2003), 2259 – 2280.<br />
[3] D. A. Fedosov, B. Caswell, G. E. Karniadakis, A Multiscale Red Blood Cell Model with<br />
Accurate Mechanics, Rheology, and Dynamics, Biophys. J. 98 (2010), 2215 – 2225.<br />
Investigation <strong>of</strong> regenerative tissues for replacing the Bruch’s membrane<br />
W. Willenberg, M. St<strong>of</strong>fel, D. Weichert, A.-K. Salz, G. Thumann (RWTH Aachen) Schedule<br />
Age-related macular degeneration (AMD) is one <strong>of</strong> the leading causes <strong>of</strong> blindness in developed<br />
countries. One <strong>of</strong> the contributing factors appears to be alterations <strong>of</strong> Bruch’s membrane such as<br />
change in elasticity and filtration properties. According to medical research it will be a promising<br />
approach to transplant cells as pre-formed monolayers on an artificial substratum. For this reason,<br />
in the present study, artificial substratums in form <strong>of</strong> collagen foils are investigated numerically<br />
and experimentally. Consequently, animal specimens and collagen foils are studies first in material<br />
tests. Based on the measured phenomena a structural and material model are proposed taking<br />
into account elastic material behaviour and diffusion properties. After implementation into a finite<br />
element code simulation results are compared to measurements. In order to investigate the<br />
remodeling process in the replacement material, a bioreactor is developed. Hereby, mechanical<br />
stimulations are subjected to cultivated cellular collagen samples while the load history and reaction<br />
forces are measured during the cultivation period.<br />
S2.6: Growth and Remodelling II Thu, 16:00–18:00<br />
Chair: Alexander Ehret S1|03–175<br />
The mechanics <strong>of</strong> growing skin<br />
Ellen Kuhl, Alexander Zollner, Adrian Buganza Tepole (Stanford University) Schedule<br />
Tissue expansion is a common surgical procedure to grow extra skin through controlled mechanical<br />
over-stretch. It creates skin that matches the color, texture, and thickness <strong>of</strong> the surrounding<br />
tissue, while minimizing scars and risk <strong>of</strong> rejection. Despite intense research in tissue expansion<br />
and skin growth, the biomechanical and mechanobiological mechanisms behind skin growth<br />
remain unclear. Here, we show that a continuum mechanics approach, embedded in a customdesigned<br />
finite element model, informed by medical imaging, provides valuable insight into the<br />
biomechanics <strong>of</strong> skin growth. In particular, we model skin growth using the concept <strong>of</strong> an incompatible<br />
growth configuration. We characterize its evolution in time using a second-order growth<br />
tensor parameterized in terms <strong>of</strong> a scalar-valued internal variable, the in-plane area growth [1].<br />
When stretched beyond the physiological level, new skin is created, and the in-plane area growth<br />
increases. We simulate tissue expansion on a patient-specific geometric model, and predict stress,<br />
strain, and area gain [2]. Our results may help the surgeon to prevent tissue over-stretch and<br />
make informed decisions about expander geometry, size, placement, and inflation. We anticipate<br />
our study to open new avenues in reconstructive surgery, and enhance treatment for patients with<br />
birth defects, burn injuries, or breast tumor removal.
72 Section 2: Biomechanics<br />
[1] Buganza Tepole A, Ploch CJ, Wong J, Gosain AK, Kuhl E. Growing skin: A computational<br />
model for skin expansion in reconstructive surgery. J Mech Phys Solids, 2011;59:2177-2190.<br />
[2] Zollner AM, Buganza Tepole A, Gosain AK, Kuhl E. Growing skin: Tissue expansion in<br />
pediatric forehead reconstruction. Biomech Mod Mechanobio, doi:10.1007/s10237-011-0357-<br />
4.<br />
A continuum model for free growth in living materials<br />
Antonio Bolea Albero, Alexander E. Ehret, Markus Böl (TU Braunschweig) Schedule<br />
Living materials can grow in volume in two different ways: following a predefined process or<br />
depending on the current state <strong>of</strong> the body. In bodies that have a set growth path, we can<br />
observe residual stresses that appear if the boundary conditions or loads do not fit with its path.<br />
In the other kind <strong>of</strong> volume growth, the tissue has a feed-back that behaves depending on a<br />
growth kinetic. We can find this growth behaviour for example in muscles (they increment their<br />
mass if we train them) or in bi<strong>of</strong>ilms. Bi<strong>of</strong>ilms grow isotropically if there are no boundaries or<br />
loads, in other case, the bi<strong>of</strong>ilm will follow a more favourable growth direction.<br />
We focus in this work on the growth kinetic for isotropically growing materials. An adaptive<br />
algorithm is used in order to satisfy the boundary conditions <strong>of</strong> the system, trying to stay in<br />
a stress free state if no external loads are applied, but keeping the volume growth defined by a<br />
growth kinetic. The proposed model based on a modified multiplicative split <strong>of</strong> the deformation<br />
gradient into a growth part and an elastic part. The growth part will be isotropic if the elastic<br />
deformations are favourable, otherwise the growth will find a more comfortable direction. Several<br />
three-dimensional examples based on different growth kinematics are presented and discussed<br />
using the numerical model.<br />
Growth and Remodelling <strong>of</strong> Biological Tissue: A Biphasic Porous Media Description<br />
Robert Krause, Bernd Markert, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
In the context <strong>of</strong> the Theory <strong>of</strong> Porous Media (TPM) [1], a continuum-mechanical model is<br />
introduced to describe the complex fluid-structure interaction in biological tissue on the macroscale.<br />
The tissue is treated as an aggregate <strong>of</strong> two immiscible constituents, where the cells and the<br />
extracellular matrix (ECM) are summarised to the solid phase, and the fluid phase summaries<br />
the extracellular fluids and its components. Growth and remodelling processes are described<br />
on the macro-scale by a distinct mass exchange that also causes a change <strong>of</strong> the constituents’<br />
material properties. To guarantee the compliance with the entropy principle, the growth energy<br />
is introduced as an additional quantity [2]. It measures the average <strong>of</strong> chemical energy available<br />
for cell metabolism and, thus, controls the growth and remodelling processes.<br />
In addition to a purely mechanical description, systems-biological control mechanisms are included<br />
into the model by an evaluation <strong>of</strong> a systems-biological cell interaction model at every integration<br />
point <strong>of</strong> the finite-element mesh.<br />
To set an example, the remodelling <strong>of</strong> a human femur under physiological loading conditions is<br />
implemented and numerically solved. Thereby, tailored programs are used for the mechanical and<br />
the systems-biological simulation. The execution <strong>of</strong> the different programs and the data exchange<br />
between the programs is controlled via Scientific Workflows.<br />
[1] W. Ehlers: Challenges <strong>of</strong> porous media models in geo- and biomechanical engineering including<br />
electro-chemically active polymers and gels. Int. J. Adv. Eng. Sci. Appl. Math. 1 (2009),<br />
1–24.
Section 2: Biomechanics 73<br />
[2] W. Ehlers, R. Krause, B. Markert: Modelling and remodelling <strong>of</strong> biological<br />
tissue in the framework <strong>of</strong> continuum biomechanics. PAMM 11 (2011), 35–38.<br />
On the global dynamics <strong>of</strong> the dePillis- Radunskaya tumor growth model<br />
Konstantin E. Starkov (Instituto Politecnico Nacional, CITEDI), Alexander P. Krishchenko<br />
(Bauman Moscow State Technical University) Schedule<br />
In this work we examine dynamical properties <strong>of</strong> one cancer tumor growth model with help <strong>of</strong><br />
studies <strong>of</strong> a localization <strong>of</strong> its compact invariant sets. This model was elaborated in [1] and has the<br />
form: ˙x1 = x1(1−x1)−a12x1x2−a13x1x3, ˙x2 = r2x2(1−x2)−a21x1x2, ˙x3 = r3x1x3<br />
x1+k3 −a31x1x3−d3x3,<br />
where by x(t) we denote the vector <strong>of</strong> cell populations: x1(t) is the number <strong>of</strong> tumour cells at the<br />
moment t; x2(t) is the number <strong>of</strong> healthy host cells at t; x3(t) is the number <strong>of</strong> effector immune<br />
cells at t. Here a localization means a description <strong>of</strong> the locus <strong>of</strong> all compact invariant sets by<br />
using equations and inequalities expressed in terms <strong>of</strong> parameters <strong>of</strong> a system, [2]. Our main<br />
results are as follows: 1) we compute upper and lower bounds for the global attractor in R3 + ;<br />
2) we study cases when each trajectory in R3 + may tend to 2i) tumor-free or ”dead” equilibrium<br />
points only; 2ii) small tumor mass equilibrium point only; 2iii) tumor-free equilibrium point only<br />
and some other related topics.<br />
Acknowledgment. This work is supported by the CONACYT project N. 78890, MEXICO.<br />
[1] de Pillis LG, Radunskaya A, [2003] Math and Comput. Modelling, 37, 1221;<br />
[2] Krishchenko AP, Starkov KE, [2006] Phys. Lett. A 353, 383.<br />
Experimental and theoretical investigations on s<strong>of</strong>t tissue remodeling enhanced by<br />
cell activity<br />
Jeong-Hun Yi, Marcus St<strong>of</strong>fel, Dieter Weichert (RWTH Aachen), Sven Nebelung and Björn Rath<br />
(<strong>Universität</strong>sklinikum Aachen) Schedule<br />
The aim <strong>of</strong> the paper is to investigate the remodeling phenomenon <strong>of</strong> a cell-seeded material. For<br />
the experiments, a cell-seeded condensed collagen gel is mechanically stimulated in a bioreactor<br />
for two or four weeks and histological investigations are carried out. Collagen type-II newly<br />
synthesized by cells causes a change <strong>of</strong> the material’s mechanical properties. In this study the<br />
new remodeled stiffness <strong>of</strong> the material is subsequently measured by a compression test. For this<br />
phenomenon, a viscoelastic-diffusion material model is proposed, which incorporates an evolution<br />
equation for the observed, long-term change <strong>of</strong> stiffness.
74 Section 3: Damage and fracture mechanics<br />
Section 3: Damage and fracture mechanics<br />
Organizers: Jörn Mosler (TU Dortmund), Manuela Sander (<strong>Universität</strong> Rostock)<br />
S3.1: Modeling material failure Tue, 13:30–15:30<br />
Chair: Ragnar Larsson, Jörn Mosler S1|03–116<br />
Ductile dynamic fracture modeling using embedded discontinuities in CGI machining<br />
simulations<br />
Ragnar Larsson, Goran Ljustina, Martin Fagerström (Chalmers University <strong>of</strong> Technology Göteborg)<br />
Schedule<br />
A major driving force for the industry to simulate various manufacturing processes is the incorporation<br />
<strong>of</strong> new design materials e.g. in order to promote lightweight design <strong>of</strong>ten leading to<br />
significant changes in manufacturing conditions, which can be assessed in an efficient way by simulation<br />
rather than more expensive testing. In the current contribution we are concerned with the<br />
constitutive modeling <strong>of</strong> Compacted Graphite Iron (CGI) with respect to orthogonal machining<br />
simulations. Although CGI consists in general <strong>of</strong> pearlite, graphite and ferrite, focus is placed<br />
on the constitutive modeling <strong>of</strong> the pearlitic phase since this is the dominating constituent with<br />
respect to the machinability issues. In this study, the continuum hardening response is modeled<br />
using the Johnson-Cook (JC) plasticity model; a model that has been extensively used in the<br />
literature for the modeling effects <strong>of</strong> large strains, high strain rates and high temperatures related<br />
to machining. In earlier works, the JC plasticity model has been used along with ductile fracture<br />
response that has been described with the element deletion based on Johnson-Cook dynamic failure<br />
criterion. In the current development we it is proposed to use a continuum damage approach<br />
for the continuous behavior up to the critical stress-strain states where discontinuous bifurcation<br />
occurs. Whenever a critical state has been diagnosed, a Cohesive Zone (CZ) is established so that<br />
the actual critical stress state is located right at the onset <strong>of</strong> stress degradation in the CZ. Both<br />
pre-peak continuum damage and post-peak CZ damage, representing distributed and localized<br />
damage evolution, respectively, are considered in the formulation. Both the pre- and post-peak<br />
damage evolutions are defined as a post-processing <strong>of</strong> the effective stress response. The localized<br />
cohesive zone damage is kinematically realized as an element embedded discontinuity which is<br />
introduced elementwise, thereby facilitating the model developments in standard FE-packages.<br />
The orthogonal machining simulations show that the new continuum damage model appears to<br />
be sensitive to element locking as well as significant element size dependence without the cohesive<br />
zone enhancement <strong>of</strong> the model. In order to investigate the extent <strong>of</strong> locking behavior in simulations<br />
and also the possible pathological mesh dependency the series <strong>of</strong> 2D shear test simulations<br />
with both triangular and rectangular elements with different sizes have been conducted and results<br />
are compared.<br />
New three-dimensional finite elements with embedded strong discontinuities to model<br />
solids at failure<br />
Christian Linder, Xiaoxuan Zhang (<strong>Universität</strong> Stuttgart) Schedule<br />
This work presents new finite elements that incorporate strong discontinuities with linear interpolations<br />
<strong>of</strong> the displacement jumps for three-dimensional finite elements within the infinitesimal<br />
theory to model solids at failure. The cases <strong>of</strong> interest are characterized by a localized cohesive<br />
law along a propagating discontinuity representing a crack in the solid, with this propagation<br />
occurring in a general finite element mesh without remeshing. As in [1] for plane problems, the<br />
new elements are constructed by enhancing the strain field <strong>of</strong> existing displacement based, as-
Section 3: Damage and fracture mechanics 75<br />
sumed strain based, and enhanced strain based 3D finite elements. The enhancement is driven<br />
by the incorporation <strong>of</strong> 9 separation modes directly into the finite element framework which are<br />
chosen so that stress locking in general brick finite elements is avoided. This results in an efficient<br />
formulation where all the introduced enhanced parameters can be statically condensed out at the<br />
element level.<br />
A series <strong>of</strong> numerical tests including single element tests and convergence studies outline<br />
the performance <strong>of</strong> the new finite elements. To drive the crack propagation for sophisticated<br />
and realistic numerical simulations in three dimensions, a global tracking algorithm is employed.<br />
The obtained results are close to experimentally observed crack paths and reaction force versus<br />
displacement relations.<br />
[1] C. Linder, F. Armero, Finite elements with embedded strong discontinuities for the modeling<br />
<strong>of</strong> failure in solids, Int. J. Numer. Meth. Engng. 72 (2007), 1391 – 1433.<br />
On the size-dependent damage behaviour <strong>of</strong> short fibre reinforced composites<br />
Ingo Scheider, Yongjun Chen, Norbert Huber (Helmholtz-Zentrum Geesthacht), Jörn Mosler (TU<br />
Dortmund, Helmholtz-Zentrum Geesthacht) Schedule<br />
The present paper is concerned with the analysis <strong>of</strong> size effects <strong>of</strong> short fibre reinforced composites.<br />
The microstructure <strong>of</strong> such composites <strong>of</strong>ten represents the first hierarchy level <strong>of</strong> a bioinspired<br />
material, and thus an elastic organic matrix material with strong but brittle ceramic fibres has<br />
been investigated. For modelling the various failure mechanisms occuring in heterogeneous materials,<br />
i.e. fibre cracking, debonding between fibre and matrix material, and matrix cracking, a fully<br />
three-dimensional cohesive zone model is applied. It is shown that this model indeed captures the<br />
size effect associated with material failure <strong>of</strong> fibre reinforced materials. More explicitly and in line<br />
with previous investigations by Gao (Int. J. Fract. 2006; 138:101-137), it is shown that a surface<br />
precracked fibre reaches its theoretical strength, if its diameter is smaller than a certain threshold.<br />
However, the one-dimensional model advocated by Gao usually leads to an overestimation<br />
<strong>of</strong> the flaw tolerance due to their simplifying assumptions. Based on these findings, a representative<br />
volume element (RVE) containing ceramic fibres with fixed aspect ratios embedded within a<br />
polymer matrix is considered. Similar to the single fibre, the RVE also shows a pronounced size<br />
effect, but the underlying physical process is significantly more complex. More explicitly, the size<br />
effect <strong>of</strong> the RVE is a superposition <strong>of</strong> that related to the isolated fibres (i.e. fibre breaking) as<br />
well as <strong>of</strong> that induced by debonding <strong>of</strong> the fibres from the matrix material.<br />
Analysis <strong>of</strong> Break Up Events in Antarctic Ice Shelves Using Configurational Forces<br />
Carolin Plate (TU Kaiserslautern), Dietmar Gross (TU <strong>Darmstadt</strong>), Angelika Humbert (<strong>Universität</strong><br />
Hamburg), Ralf Müller (TU Kaiserslautern) Schedule<br />
Previous studies on the sensitivity <strong>of</strong> cracks in ice shelves with different boundary conditions,<br />
stress states and density pr<strong>of</strong>iles revealed the need for further analyses. Therefore, the aim <strong>of</strong> this<br />
presentation is to discuss new findings on the effect <strong>of</strong> freezing water in surface crevasses and<br />
the influence <strong>of</strong> depth dependent material parameters, e.g. Youngs modulus and Poissons ratio<br />
on the criticality <strong>of</strong> cracks. The numerical simulations are conducted using Finite Elements utilizing<br />
the concept <strong>of</strong> configurational forces. Therefore, a 2-dimensional geometry with mode-I loads<br />
and additional body forces is analyzed. As the transfer <strong>of</strong> boundary conditions from dynamic ice<br />
flow simulations to the linear elastic fracture analyses proved to be a critical aspect in previous<br />
studies, preliminary results on visco-elastic fracture simulations <strong>of</strong> ice shelves will be provided.
76 Section 3: Damage and fracture mechanics<br />
These results yield the opportunity <strong>of</strong> finding a measure on how cracks <strong>of</strong> different size influence<br />
the viscosity <strong>of</strong> the ice shelf in dynamic flow simulations.<br />
Modeling <strong>of</strong> deformation and failure in rubber-toughened polymers – effect <strong>of</strong> distributed<br />
crazing<br />
Martin Helbig, Thomas Seelig (KIT) Schedule<br />
The improved ductility and toughness <strong>of</strong> rubber-modified polymers, e.g. ABS, relies on microscale<br />
deformation and damage mechanisms such as rubber particle cavitation, matrix shear yielding<br />
and crazing. The present work focusses on the effect <strong>of</strong> distributed crazing, i.e. the formation <strong>of</strong><br />
cohesive crack-like defects, between the fine dispersed rubber particles. A macroscopic material<br />
model for the inelastic deformation behavior <strong>of</strong> ABS is developed that describes distributed crazing<br />
as an anisotropic flow process. Scaling <strong>of</strong> the overall yield strength and failure strain with the<br />
rubber volume fraction is explicitly accounted for through micromechanical considerations. The<br />
suitability <strong>of</strong> the model is analyzed by comparison <strong>of</strong> finite element simulations with experimental<br />
findings.<br />
S3.2: Continuum damage mechanics and phase field models Tue, 16:00–18:00<br />
Chair: Daniel Balzani, Jörn Mosler S1|03–116<br />
Relaxed Incremental Variational Formulation for Damage in Fiber-Reinforced Materials<br />
Daniel Balzani (<strong>Universität</strong> Duisburg-Essen), Michael Ortiz (Caltech) Schedule<br />
An incremental variational formulation for damage at finite strains is proposed based on the<br />
classical continuum damage mechanics. Since loss <strong>of</strong> convexity is obtained at some critical deformations<br />
a relaxed incremental stress potential is constructed which convexifies the original<br />
non-convex problem, see also [1] for the small strain framework. This approach is in line with<br />
the general approach for standard dissipative solids presented in [2]. The resulting model can be<br />
interpreted as the homogenization <strong>of</strong> a micro-heterogeneous material bifurcated into a strongly<br />
and weakly damaged phase at the microscale, cf. [3]. A one-dimensional relaxed formulation is<br />
derived and based thereon, a model for fiber-reinforced materials is given, see [4]. Finally, some<br />
numerical examples illustrate the performance <strong>of</strong> the model.<br />
[1] E. Gürses, Aspects <strong>of</strong> Energy Minimization in Solid Mechanics: Evolution <strong>of</strong> Inelastic Microstructures<br />
and Crack Propagation, Bericht Nr.: I-19, Institut für Mechanik (Bauwesen),<br />
Lehrstuhl I, Pr<strong>of</strong>essor C. Miehe, 2007<br />
[2] C. Miehe and M. Lambrecht, A two-scale finite element relaxation analysis <strong>of</strong> shear bands in<br />
non-convex inelastic solids: small strain theory for standard dissipative materials, Computer<br />
Methods in Applied Mechanics and Engineering, 192:473-508, 2003.<br />
[3] G.A. Francfort and A. Garroni, A variational view <strong>of</strong> partial brittle damage evolution, Archive<br />
<strong>of</strong> Rational Mech. and Analysis, 182:125-152, 2006.<br />
[4] D. Balzani and M. Ortiz, Relaxed Incremental Variational Formulation for Damage at Large<br />
Strains with Application to Fiber-Reinforced Materials and Materials with Truss-like Microstructures,<br />
Computer Methods in Applied Mechanics and Engineering, submitted.<br />
Interpretation <strong>of</strong> parameters in phase field models for fracture<br />
Charlotte Kuhn, Ralf Müller (TU Kaiserslautern) Schedule
Section 3: Damage and fracture mechanics 77<br />
Based on Bourdin’s regularization <strong>of</strong> a variational fracture criterion, a phase field fracture model<br />
is formulated. This model, as virtually any phase field fracture model, features a length scale parameter<br />
which controls the width <strong>of</strong> the transition zone between broken and undamaged areas. In<br />
the limit case <strong>of</strong> a vanishing length parameter, the model converges to the underlying sharp crack<br />
model. From this point <strong>of</strong> view, the length scale parameter is a purely auxiliary numerical quantity.<br />
The study <strong>of</strong> the model in an one-dimensional quasi-static setting yields another interpretation<br />
<strong>of</strong> the length parameter. Qualitatively, there are two different solutions to the one-dimensional<br />
quasi-static problem: a homogeneous solution with a constant crack field, and an inhomogeneous<br />
solution, where the crack field localizes at a certain point which leads to the nucleation <strong>of</strong> a crack.<br />
In the homogeneous setting, it is observed that there is a critical stress value, at which the material<br />
starts to s<strong>of</strong>ten. It can be shown, that this stress level coincides with the stability point <strong>of</strong><br />
the homogeneous solution. At this point, the numerical solution bifurcates to the inhomogeneous<br />
solution and a crack forms. The value <strong>of</strong> this critical stress is determined by the stiffness and<br />
cracking resistance <strong>of</strong> the material in conjunction with the introduced length parameter. In this<br />
regard, the length parameter may be seen as a material parameter since is related to the critical<br />
stress at which crack nucleation occurs. The analytical findings are approved in finite element<br />
simulations.<br />
Phase Field Modeling <strong>of</strong> Fracture in Plates and Shells<br />
H. Ulmer, M. H<strong>of</strong>acker, C. Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
The numerical modeling <strong>of</strong> failure mechanisms in plates and shells due to fracture based on sharp<br />
crack discontinuities is extremely demanding and suffers in situations with complex crack topologies.<br />
This drawback can be overcome by a diffusive crack modeling, which is based on the<br />
introduction <strong>of</strong> a crack phase field. Such an approach to brittle fracture is conceptually in line<br />
with gradient-extended continuum damage models which include internal length scales. In this<br />
lecture, we extend ideas recently outlined in [1,2] towards the phase field modeling <strong>of</strong> fracture in<br />
dimension-reduced continua with application to plates and shells. We start our investigation with<br />
a regularized crack line functional that converges for vanishing length-scale parameter to a sharp<br />
crack topology functional. This functional provides the basis for the definition <strong>of</strong> suitable dissipation<br />
functions, which govern the evolution <strong>of</strong> the crack phase field. Next, we define energy storage<br />
functions for Kirchh<strong>of</strong>f plates and shells, which degrade with increasing phase field. Finally, we<br />
propose rate-type variational principles, whose Euler equations are the quasi-static form <strong>of</strong> the<br />
balance <strong>of</strong> momentum and a partial differential equation that describes the evolution <strong>of</strong> the crack<br />
phase field. The introduction <strong>of</strong> history fields, containing the maximum reference energy obtained<br />
in history, provides a very transparent representation <strong>of</strong> these coupled equations. In particular,<br />
it allows the construction <strong>of</strong> an extremely robust operator split technique. An important aspect<br />
<strong>of</strong> the modeling is the separation <strong>of</strong> bending and membrane source terms in the evolution equation<br />
<strong>of</strong> the crack phase field. A very simple and robust discretization <strong>of</strong> the coupled problem is<br />
obtained by C 0 continuous rotation-free finite elements for plates and shells, whose only nodal<br />
degrees <strong>of</strong> freedom are the displacement and the phase field. We demonstrate the performance <strong>of</strong><br />
the proposed models by means <strong>of</strong> some representative numerical examples showing complex crack<br />
patterns and failure modes in plates and shells.<br />
[1] C. Miehe, F. Welschinger, M. H<strong>of</strong>acker, Thermodynamically consistent phase-field models <strong>of</strong><br />
fracture: Variational principles and multi-field FE implementations, Int. J. Numer. Meth.<br />
Eng., 83 (2010), 1273–1311.<br />
[2] C. Miehe, M. H<strong>of</strong>acker, F. Welschinger, A phase field model for rate-independent crack<br />
propagation: Robust algorithmic implementation based on operator splits, Comput. Method.
78 Section 3: Damage and fracture mechanics<br />
Appl. M. 199 (2010), 2765–2778.<br />
Damage processes coupled with phase separation in elastically stressed alloys<br />
Christian Heinemann, Christiane Kraus (WIAS Berlin) Schedule<br />
Diffuse interface models can be used to describe phase separation and coarsening as well as damage<br />
processes in elastic multi-component alloys.<br />
This talk first introduces a model where both processes, phase separation and incomplete<br />
damage, are coupled. The phase separation is here described by a elastic Cahn-Hilliard equation<br />
and the damage process by a doubly nonlinear differential inclusion. In incomplete damage models,<br />
the material maintains its elastic behavior even in a region <strong>of</strong> maximal damage. We are interested<br />
in free energies <strong>of</strong> the system which may contain a chemical energy <strong>of</strong> polynomial or logarithmic<br />
type, an inhomogeneous elastic energy and a quadratic term <strong>of</strong> the gradient <strong>of</strong> the damage variable.<br />
An important example <strong>of</strong> an elastic energy density which is covered in our framework is<br />
W = 1<br />
2 (z + ε)C(c)(e(u) − e⋆ (c)) : (e(u) − e ⋆ (c))<br />
with concentration c, damage z and deformation u. Existence theorems are presented for polynomial<br />
and logarithmic chemical potentials.<br />
Additionally, the complete damage case, i.e. ε = 0, where the diffusion mobility also depends<br />
on the damage and degenerates on the completely damaged parts is studied. Using the previous<br />
framework, the problems arising in the transition ε → 0 + are discussed. The limit model can be<br />
formulated in terms <strong>of</strong> a free boundary which borders the region <strong>of</strong> the not completely damaged<br />
parts with Dirichlet boundary from the parts where no deformation field can be established.<br />
The influence <strong>of</strong> viscoelastic material behaviour on the interface failure in composite<br />
materials<br />
Sebastian Müller, Markus Kästner, Volker Ulbricht (TU Dresden) Schedule<br />
The nonlinear macroscopic material behaviour <strong>of</strong> composites is amongst others driven by damage<br />
effects and the strain-rate dependent material behaviour <strong>of</strong> typical polymeric matrices. As a result<br />
<strong>of</strong> the complex geometry <strong>of</strong> textile reinforcing architectures, the application <strong>of</strong> the standard finite<br />
element method tends to result in an extensive modelling and meshing effort including problems<br />
related to distorted element shapes and a poor numerical condition <strong>of</strong> the system <strong>of</strong> equations to<br />
be solved. Therefore, the authors have implemented XFEM [1] to model the local heterogeneous<br />
material structure in an RVE.<br />
For the description <strong>of</strong> curved material interfaces a higher order XFEM formulation including<br />
quadratic basis functions and integration subdomains which are consistent to the curved path<br />
<strong>of</strong> the discontinuity has been developed. In order to incorporate microscopic damage effects, the<br />
modelling procedure has been enhanced to model the failure <strong>of</strong> the fibre-matrix interface. To<br />
this end, a second enrichment term [2] accounting for the strong discontinuity is added to the<br />
displacement approximation. The mechanical behaviour in the fracture zone is represented by an<br />
cohesive zone model.<br />
In addition to these approaches, which account for the material structure and the interface<br />
failure, a fractional viscoelastic material model has been developed for the polymeric matrix<br />
material [3]. The combination with the XFEM model and homogenisation techniques allows for<br />
the calculation <strong>of</strong> effective inelastic material behaviour <strong>of</strong> the composite material.<br />
[1] M. Kästner, G. Haasemann and V. Ulbricht, Multiscale XFEM-modelling and simulation <strong>of</strong>
Section 3: Damage and fracture mechanics 79<br />
the inelastic material behaviour <strong>of</strong> textile-reinforced polymers, Int. J. Numer. Meth. Engng.<br />
86 (2011), 477 – 498.<br />
[2] G. Zi and T. Belytschko, New crack-tip elements for XFEM and applications to cohesive<br />
cracks, Int. J. Numer. Meth. Engng. 57 (2003), 2221 – 2240.<br />
[3] S. Müller, M. Käestner, J. Brummund, V. Ulbricht, A nonlinear fractional viscoelastic material<br />
model for polymers, Computational Materials Science 50 (2011), 2938-2949.<br />
Creep damage modeling <strong>of</strong> a polycrystalline material<br />
Oksana Ozhoga-Maslovskaja, Holm Altenbach, Konstantin Naumenko, Oleksandr Prygorniev<br />
(<strong>Universität</strong> Magdeburg) Schedule<br />
A polycrystal unit cell is simulated and investigated under creep conditions within the framework<br />
<strong>of</strong> continuum micromechanics. Geometrical 3D model <strong>of</strong> a polycrystalline microstructure is represented<br />
as a unit cell with grains <strong>of</strong> random crystallographical orientation and shape. Thickness <strong>of</strong><br />
the plains, separating neighboring grains in the unit cell, has non-zero value. Obtained geometry<br />
assigns a special zone in the vicinity <strong>of</strong> grain boundaries, possessing unordered crystalline structure.<br />
Within the grain interior crystalline structure is ordered, what prescribes cubic symmetry<br />
<strong>of</strong> a material. According to this the anisotropic material model with the cubic symmetry is implemented<br />
in ABAQUS and used to assign elastic and creep behavior <strong>of</strong> a grain interior. Material<br />
parameters are identified from creep tests for single crystals copper. In order to describe damage<br />
processes in a polycrystalline material, accompanying the tertiary creep stage, micromechanical<br />
damage model is involved. The continuum damage model, based on grain boundary cavitation is<br />
implemented in the grain boundary zone <strong>of</strong> the unit cell. Stress redistribution within the grains<br />
is investigated. Overall response <strong>of</strong> the unit cell is analyzed during the primary, secondary and<br />
tertiary creep.<br />
S3.3: Fracture Mechanics Wed, 13:30–15:30<br />
Chair: Manuela Sander, Geralf Hütter S1|03–116<br />
Recovery based error estimation for 3D multiscale computations within the XFEM<br />
for cracks<br />
Corinna Prange, Stefan Loehnert, Peter Wriggers (<strong>Universität</strong> Hannover) Schedule<br />
The extended finite element method (XFEM) is established as a reasonable method to simulate<br />
cracks. Using the XFEM, cracks can be modelled independent <strong>of</strong> the mesh. Even coarse meshes<br />
usually lead to suitable results for displacements and stresses. Nevertheless, the solution is more<br />
accurate for finer meshes. Therefore, an adaptive mesh refinement based on a discretization error<br />
estimation technique is applied.<br />
In many materials in the vicinity <strong>of</strong> a propagating macrocrack microcracks develop. Considering<br />
these microckracks is important for crack growth since they can lead to crack shielding<br />
or crack amplification effects. Microcracks further away to the crack front are <strong>of</strong> less influence.<br />
Therefore, only those microcracks in the vicinity to a macrocrack front need to be considered.<br />
To model the microcracks in an accurate way the mesh has to be finer than for the macrocrack<br />
description. A twoscale technique based on a projection method enables the consideration <strong>of</strong><br />
microcracks around each crack front with low computational effort.<br />
To improve the results <strong>of</strong> the microscale computation the above mentioned recovery based<br />
discretization error estimation is utilised. The adaptive mesh refinement causes incompatible
80 Section 3: Damage and fracture mechanics<br />
’hanging’ nodes. Applied to the XFEM some specialties occur, e.g. in our approach those hanging<br />
nodes are not allowed to be enriched with additional degrees <strong>of</strong> freedom.<br />
The error estimator is presented for 3D single- and multiscale computations. Effects <strong>of</strong> the<br />
radius <strong>of</strong> the microdomain around a crack front are analysed.<br />
Modeling <strong>of</strong> quasi-static crack growth with a multilevel embedded FEM<br />
Arun Raina, Christian Linder (<strong>Universität</strong> Stuttgart) Schedule<br />
Modern engineering applications sometimes subject materials to external forces beyond their<br />
design limit. It is <strong>of</strong> utmost importance for the integrity <strong>of</strong> the structure and general safety that<br />
material behavior beyond design limit is understood. Cracks or shearbands are the starting point <strong>of</strong><br />
any material failure subjected to high stresses which appear as jumps in the displacement field also<br />
called as ’strong discontinuities’. Some advanced numerical techniques like the ”embedded finite<br />
element method (EFEM)” [1] can model failure <strong>of</strong> solids with a very good approximation. The key<br />
advantages <strong>of</strong> EFEM over other available methods are its mesh independency and computational<br />
efficiency that makes the method suitable for the newly developed multilevel approach as described<br />
below. The multilevel embedded finite element method facilitates the use <strong>of</strong> even coarser meshes<br />
at the failure zone with improved accuracy. The methodology also enables the development <strong>of</strong><br />
multiple strong discontinuities in a single finite element which can be used to model certain<br />
complex failure phenomena.<br />
The multilevel approach <strong>of</strong> using the EFEM is derived from the method <strong>of</strong> domain decomposition<br />
[2]. For a discretized domain, the finite elements at the zone where a strong discontinuity<br />
can form and propagate based on some failure criterion are treated as separate sub-boundary<br />
value problems. Each global finite element representing a sub-boundary value problem is adaptively<br />
discretized during the run time into a number <strong>of</strong> sub-elements which are subjected to a<br />
kinematic constraint at the degrees <strong>of</strong> freedom associated with its boundary. The newly created<br />
sub-boundary problem therefore becomes a constrained minimization problem which is solved in<br />
every Newton iteration <strong>of</strong> an incremental time step. Each sub-element in a sub-boundary value<br />
problem is equally capable <strong>of</strong> developing a strong discontinuity depending upon its state <strong>of</strong> stress.<br />
The kinematic constraint at the boundary is a linear displacement based interface which is modified<br />
accordingly as soon as a strong discontinuity crosses the global finite element boundary. For<br />
the local equilibrium, the coupling between the quantities at two different levels <strong>of</strong> discretization<br />
is obtained by matching the virtual energies due to admissible variations <strong>of</strong> the global finite<br />
element and its constituent sub-elements.<br />
[1] C. Linder, F. Armero, Finite elements with embedded strong discontinuities for the modeling<br />
<strong>of</strong> failure in solids, Int. J. Numer. Methods Engrg. 72 (2007), 1391-1433.<br />
[2] K.C. Park, C.A. Felippa, A variational principle for the formulation <strong>of</strong> the partitioned structural<br />
systems, Int. J. Numer. Methods Engrg. 47 (2000), 395–418.<br />
Crack growth in elastic materials with internal boundaries and interfaces<br />
P. Judt, A. Ricoeur (<strong>Universität</strong> Kassel) Schedule<br />
This work presents numerical methods used for predicting crack paths in technical structures<br />
based on the theory <strong>of</strong> linear elastic fracture mechanics. The FE-method is used in combination<br />
with an efficient remeshing algorithm to simulate crack growth. Different post processors providing<br />
loading parameters such as the J-integral and stress intensity factors (SIF) are presented.<br />
Path-independent contour integrals [1] are used to avoid special requirements concerning crack tip
Section 3: Damage and fracture mechanics 81<br />
meshing and to enable efficient calculations for domains including interfaces and internal boundaries.<br />
Several crack growth criteria are compared with respect to the resulting crack paths. In<br />
particular, the interaction <strong>of</strong> cracks and internal boundaries and interfaces is investigated. The<br />
simulation combines crack propagation within elastic bodies and at bimaterial interfaces. The latter<br />
is based on a cohesive zone model. The presented numerical results <strong>of</strong> crack paths are verified<br />
by experiments.<br />
[1] Rice, J.R.; Journal <strong>of</strong> Applied Mechanics 35, 379-386 (1968)<br />
Simulation <strong>of</strong> Crack Propagation with Competing Brittle and Ductile Damage Mechanisms<br />
Geralf Hütter (TU Freiberg), Thomas Linse (TU Dresden), Uwe Mühlich, Meinhard Kuna (TU<br />
Freiberg) Schedule<br />
For decreasing temperatures, typical engineering metals show a transition from ductile to brittle<br />
failure. The accompanied loss <strong>of</strong> toughness, e.g. measured as Charpy-energy or crack growth resistance,<br />
is a problem in many technical applications. Today, the so-called local approach to fracture<br />
got state-<strong>of</strong>-the-art, whereby the damage is computed equivalently to stresses and deformations.<br />
However, in most cases only the ductile damage is taken into account as damage variable whereas<br />
possible cleavage is still evaluated by post-processing criteria. Mostly, it is argued that cleavage<br />
cracks propagate instably coinciding with structural failure. Certainly, this type <strong>of</strong> approach does<br />
not account for the interaction <strong>of</strong> ductile and cleavage mechanisms which is important in the<br />
upper ductile-brittle transition region as well as for phenomena like crack arrest.<br />
For our contribution we employ a non-local model <strong>of</strong> Gurson-type together with a cohesive<br />
zone to model the ductile-brittle transition region. This consistent formulation <strong>of</strong> a boundary<br />
value problem allows arbitrary mesh resolutions. The crack propagation is simulated within the<br />
limiting case <strong>of</strong> small-scale yielding.<br />
The results show that the model captures qualitative effects <strong>of</strong> corresponding experiments<br />
such as pop-ins, the formation <strong>of</strong> a stretch zone and secondary cracks. The influence <strong>of</strong> the temperature<br />
on the predicted toughness is reproduced in the whole ductile-brittle transition region<br />
without introducing temperature dependent fit parameters. The pop-in mechanism <strong>of</strong> secondary<br />
cracks and unloading zones is highlighted.<br />
Monitoring fatigue cracks and stress intensity factors based on local strains<br />
Ramdane Boukellif, Andreas Ricoeur (<strong>Universität</strong> Kassel) Schedule<br />
We present a method for crack detection and stress intensity factor measurement in plate structures<br />
by using strain gauges and applying the Body Force Method (BFM) as well as the dislocation<br />
method. The BFM is based on elastic solutions for concentrated loads and the principle <strong>of</strong> linear<br />
superposition allowing e.g. the calculation <strong>of</strong> the strain field in a cracked body. The dislocation<br />
method is based on a similar idea, however the crack is here represented by a line <strong>of</strong> point dislocations.<br />
Thus, the approach is based on the weighted superposition <strong>of</strong> elastic Greens functions<br />
representing the strain field due to the presence <strong>of</strong> a crack, where the weights are being identified<br />
by inverse problem solution. Since the strain fields are controlled by both external loads and<br />
the crack growth the unknown parameters are crack position and inclination as well as loading<br />
quantities. First, the algorithms are verified based on numerical simulations. The particle swarm<br />
algorithm came out to be most suitable for parameter identification in a high dimensional space.<br />
Experimentally, we use strain gauges at different positions to measure the remote strain field on<br />
the surface <strong>of</strong> a plate structure. Experiments are carried out under cyclic loading using pre-cracked
82 Section 3: Damage and fracture mechanics<br />
plates made <strong>of</strong> aluminum alloy.<br />
Investigation <strong>of</strong> the local behavior <strong>of</strong> different cohesive zone models<br />
Claudio Balzani (<strong>Universität</strong> Hannover) Schedule<br />
Cohesive interface elements are well suited for three-dimensional crack propagation analyses as<br />
long as the crack path is well known. This is the case e.g. in delamination analyses <strong>of</strong> laminated<br />
composite structures or failure analyses <strong>of</strong> adhesively bonded joints. Actually, they are widely<br />
used in such applications for both brittle and ductile systems.<br />
As long as the strength and fracture toughness <strong>of</strong> the material are accurately captured it is<br />
generally accepted that the shape <strong>of</strong> the cohesive law describing the nonlinear s<strong>of</strong>tening behavior<br />
has little to no influence on the mechanical behavior <strong>of</strong> the investigated structures. The author<br />
agrees if the global structural response is <strong>of</strong> interest.<br />
However, when having a look on the local behavior <strong>of</strong> different cohesive zone models, such as<br />
stress distribution in the fracture process zone, the results exhibit certain differences. These will<br />
be studied in the present contribution. Especially the local stress distribution will be investigated<br />
and the effect on the computational efficiency will be pointed out based on relevant numerical<br />
examples with experimental evidence.<br />
S3.4: Dynamic Fracture Mechanics Wed, 16:00–18:00<br />
Chair: Manuela Sander, Martina H<strong>of</strong>acker S1|03–116<br />
Dynamic crack analysis in 2D elastic solids with the singular edge-based smoothed<br />
finite element method<br />
Tinh Q. Bui, Chuanzeng Zhang (<strong>Universität</strong> Siegen) Schedule<br />
In this work, the recently developed singular edge-based smoothed finite element method (sES-<br />
FEM) [1] is further developed for dynamic crack analysis in two-dimensional elastic solids. The<br />
objective <strong>of</strong> this paper is to provide a better understanding <strong>of</strong> the dynamic fracture behaviors <strong>of</strong><br />
linear elastic solids in the framework <strong>of</strong> the strain smoothing approach. Following this approach,<br />
the strains are smoothed and the system stiffness matrix is thus performed using the strain<br />
smoothing technique over the smoothing domains associated with the element edges. In order<br />
to accurately capture the singular fields at the crack tip, a two-layer singular five-node crack-tip<br />
element is employed. Due to the unique feature <strong>of</strong> the present sES-FEM formulation, such singular<br />
crack-tip element is constructed based on the assumed displacement values on the boundary <strong>of</strong> the<br />
smoothing domains without the need <strong>of</strong> the derivatives. The singular shape functions are generated<br />
by a simple point interpolation with a fractional order basis without the mapping procedure. The<br />
governing dynamic equations are transformed into a standard weak-form, which is then discretized<br />
into a sES-FEM system <strong>of</strong> time-dependent equations to be solved by the unconditionally stable<br />
implicit Newmark time integration method. To analyze the fracture behaviors <strong>of</strong> linear elastic<br />
solids, mixed-mode dynamic stress intensity factors (DSIFs) are evaluated using the domain forms<br />
<strong>of</strong> the interaction integrals in terms <strong>of</strong> the smoothing technique. Various numerical examples are<br />
considered to illustrate the accuracy <strong>of</strong> the proposed approach, and the computed results for the<br />
normalized DSIFs are compared with reference solutions in a wide range <strong>of</strong> benchmark dynamic<br />
crack problems which shows high accuracy <strong>of</strong> the proposed sES-FEM.<br />
[1] G. R. Liu, N. Nourbakhshnia, L. Chen, Y. W. Zhang. A novel general formulation for singular<br />
stress field using the ES-FEM method for the analysis <strong>of</strong> mixed-mode cracks. Int J Comput<br />
Methods 7 (2010), 191–214
Section 3: Damage and fracture mechanics 83<br />
A New Phase Field Model for Dynamic Fracture Accounting for Brittle to Ductile<br />
Failure Mode Transition<br />
M. H<strong>of</strong>acker, C. Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
The computational modeling <strong>of</strong> failure mechanisms in solids due to fracture based on sharp crack<br />
discontinuities suffers in dynamic problems with complex crack topologies including branching.<br />
This can be overcome by a diffusive crack modeling based on the introduction <strong>of</strong> a crack phase<br />
field as suggested in [1,2]. In this work, we extend these recent models <strong>of</strong> brittle crack propagation<br />
towards the analysis <strong>of</strong> ductile fracture in elastic-plastic solids. In particular, we propose a<br />
formulation that is able to predict the brittle-to-ductile failure mode transition under dynamic<br />
loading. The proposed model is able to reproduce the classical impact test performed by Kalth<strong>of</strong>f<br />
and Winkler, which shows brittle-to-ductile failure mode transition for increasing impact velocity.<br />
We start our investigation with an intuitive and descriptive derivation <strong>of</strong> a regularized crack<br />
surface functional that converges for vanishing length-scale parameter to a sharp crack topology<br />
functional. This functional provides the basis for the construction <strong>of</strong> suitable energy storage and<br />
dissipation functions, which govern the degrading stress response in ductile materials and the<br />
evolution <strong>of</strong> both the plastic strain as well as the crack phase field. The governing equations are<br />
derived in a consistent manner from a rate-type variational principle. We then introduce local<br />
history fields which contain suitably defined crack sources which accumulate in the deformation<br />
history. It is shown that these local variables drive the evolution <strong>of</strong> the crack phase field. The<br />
introduction <strong>of</strong> the history fields inspires the construction <strong>of</strong> extremely robust operator split schemes<br />
<strong>of</strong> phase-field-type fracture which successively update in a typical time step the history fields,<br />
the crack phase field and finally the displacement field. We demonstrate the performance <strong>of</strong> the<br />
proposed phase field formulation <strong>of</strong> fracture by means <strong>of</strong> the simulation <strong>of</strong> the Kalth<strong>of</strong>f Winkler<br />
experiment and show the failure mode transition.<br />
[1] C. Miehe, M. H<strong>of</strong>acker, F. Welschinger, A phase field model forrate-independent crack propagation:<br />
Robust algorithmic implementation based onoperator splits, Comput. Method. Appl.<br />
M. 199 (2010), 2765–2778.<br />
[2] M. H<strong>of</strong>acker, C. Miehe, A phase field model <strong>of</strong> dynamic fracture: Robust field updates for<br />
the analysis <strong>of</strong> complex crack patterns, submitted to Int. J. Numer. Meth. Eng.<br />
Debonding propagation analysis <strong>of</strong> sandwich beams subjected to dynamic bending<br />
loading<br />
Vyacheslav N. Burlayenko (National Technical University KhPI, Kharkov), Tomasz Sadowski<br />
(Lublin University <strong>of</strong> Technology) Schedule<br />
Sandwich materials are an assembly <strong>of</strong> generally orthotropic layers, consisting <strong>of</strong> rigid face sheets<br />
sandwiched by the lightweight and s<strong>of</strong>t core. The resin rich interface between the basic layers are<br />
susceptible to damage from occurring large stresses that can be the prelude to debonding initiation<br />
and its advancing under loading conditions. In this study an assessment <strong>of</strong> the debonding advance<br />
within a sandwich beam is examined. The sandwich beam with an embedded debonding zone<br />
is subjected to both a static and a dynamic transverse load. The finite element model <strong>of</strong> the<br />
sandwich beam is simulated by using the finite element code ABAQUS. Both the linear fracture<br />
mechanics approach, based on the virtual crack closure technique and the damage mechanics<br />
approach, implemented in ABAQUS through cohesive elements are applied to consideration <strong>of</strong><br />
the stress regimes at the damaged interface to predict the debonding capability to propagate. For<br />
this application the behavior <strong>of</strong> cohesive elements is defined in terms <strong>of</strong> the traction-separation
84 Section 3: Damage and fracture mechanics<br />
law along with a progressive damage model. Stress-based damage initiation criteria are used to<br />
evaluate the propensity <strong>of</strong> the sandwich beam to undergo damage. Both implicit and explicit<br />
solvers available in ABAQUS are applied for analyzing damage tolerance <strong>of</strong> partially debonded<br />
sandwich beams under conditions <strong>of</strong> static and dynamic loading. Distributions <strong>of</strong> stresses and<br />
components <strong>of</strong> strain energy release rate are calculated at the debonding front so that to make a<br />
conclusion on debonding propagation process.<br />
Microcrack Evolution in Functionally Graded Material under Dynamic Loading<br />
Ralf Mueller, Natalia Konchakova (<strong>Universität</strong> Kaiserslautern) Schedule<br />
The damage process <strong>of</strong> metal-ceramic functionally graded material (FGM) is investigated. The<br />
microcrack evolution in a layered structure is analyzed using numerical simulation (FEM) <strong>of</strong> stresses<br />
and configurational forces. The modelling <strong>of</strong> an FGM <strong>of</strong> alumina ceramic and a metalic phase<br />
with gradually changing volume fraction <strong>of</strong> alumina is performed. A structure <strong>of</strong> two different<br />
layers bonded to a substrate is used. The stiffness and density <strong>of</strong> the three materials are varying.<br />
The evolution <strong>of</strong> configurational forces is simulated.<br />
The influence <strong>of</strong> crack length on the crack driving force is studied for the case <strong>of</strong> a stress wave<br />
loading. The stress loading is applied in the horizontal direction as a dead load.<br />
The comparison with an uncracked FGM is considered. It is shown that in the case <strong>of</strong> an<br />
uncracked FGM the zone <strong>of</strong> maximal stress is placed in the central part <strong>of</strong> the specimen in the<br />
material with maximal volume fraction <strong>of</strong> alumina, which yields maximal Young Modulus and<br />
minimal density.<br />
Boundary Integral Equations in the Frequency Domain for Interface Cracks under<br />
Impact Loading<br />
Oleksandr V. Menshykov, Maryna V. Menshykova (University <strong>of</strong> Aberdeen), Michael Wuensche,<br />
Chuanzeng Zhang (<strong>Universität</strong> Siegen) Schedule<br />
It is common knowledge that all existing structural materials contain various inter- and intracomponent<br />
cracks which appear in materials during fabrication or in-service. The presence <strong>of</strong><br />
structural defects considerably decreases the strength and the reliability <strong>of</strong> materials.<br />
Under deformation the opposite faces <strong>of</strong> the existing cracks interact with each other, altering<br />
significantly the stress fields near the crack tips. The analysis <strong>of</strong> static problems demonstrates<br />
that the contact interaction considerably changes the solution. It takes on special significance for<br />
the case <strong>of</strong> high rate deformations as found in impact and high-frequency dynamics, which covers<br />
an extremely wide range <strong>of</strong> situations, where the contact interaction can change the response substantially.<br />
Unfortunately, due to the non-linearity <strong>of</strong> the problem and substantial computational<br />
difficulties, the overwhelming majority <strong>of</strong> studies neglect the contact interaction <strong>of</strong> crack faces in<br />
spite <strong>of</strong> its evident significance.<br />
In the current study we investigate 2D interface cracks between two dissimilar homogeneous<br />
isotropic half-spaces undergoing impact loading. In order to take the contact interaction <strong>of</strong> crack<br />
faces into account the Signorini constraints are imposed for normal components <strong>of</strong> displacements<br />
and forces. The problem is solved using the boundary integral equations in the frequency domain.<br />
The distributions <strong>of</strong> the displacements and tractions at the bonding interface and surfaces <strong>of</strong> the<br />
cracks are obtained and analysed. The stress intensity factors (opening and shear modes) are<br />
computed for different values <strong>of</strong> the wave frequency and different properties <strong>of</strong> the bimaterial.
Section 3: Damage and fracture mechanics 85<br />
BEM for transient thermoelastic analysis <strong>of</strong> a functionally graded layer on a homogeneous<br />
substrate under thermal shock<br />
A. Ekhlakov (<strong>Universität</strong> Siegen), Oksana M. Khay (<strong>Universität</strong> Siegen, Pidstryhach Institute for<br />
Applied Problems <strong>of</strong> Mechanics and Mathematics Lviv), Chuanzeng Zhang (<strong>Universität</strong> Siegen)<br />
Schedule<br />
In this paper, transient thermoelastic analysis <strong>of</strong> two-dimensional, isotropic and linear elastic bimaterials,<br />
which are constituted by a functionally graded (FG) layer attached to a homogeneous<br />
substrate, subjected to thermal shock is investigated. For this purpose, a boundary element method<br />
(BEM) for coupled and linear thermoelasticity is developed. The material properties <strong>of</strong> the<br />
FG layer are assumed to be continuous functions <strong>of</strong> the spatial coordinates, while Poissons ratio is<br />
taken as constant. The Laplace-transform technique is applied to eliminate the time-dependence<br />
in the governing partial differential equations.<br />
Fundamental solutions <strong>of</strong> linear coupled thermoelasticity for homogeneous, isotropic and linear<br />
elastic materials in the Laplace-transformed domain are used to derive boundary-domain integral<br />
representations for the mechanical and thermal fields. The FG/homogeneous bimaterials are modeled<br />
by using a sub-domain technique. The bimaterial system is divided into a homogeneous and<br />
a non-homogeneous sub-domain along the interface. The boundary-domain integral equations are<br />
applied to each sub-domain and the continuity conditions are employed on the interface boundary.<br />
Due to the material non-homogeneity in the FG layer, this approach leads to domain integrals<br />
involving the unknown quantities in addition to the conventional boundary integrals. The domain<br />
integrals are transformed into boundary integrals by using the radial integration method (RIM).<br />
For the homogeneous and linear elastic substrate, only boundary integrals need to be considered<br />
in the boundary integral equations. A collocation method is implemented for the spatial discretization<br />
<strong>of</strong> the boundary-domain integral equations. Numerical solutions are first obtained in the<br />
Laplace-transformed domain for discrete values <strong>of</strong> the Laplace-transform parameter. To obtain<br />
time-dependent solutions, an inverse Laplace-transform by using Stehfests algorithm is performed.<br />
Numerical examples for an exponential gradation <strong>of</strong> the material parameters are presented<br />
and discussed to demonstrate the accuracy and the efficiency <strong>of</strong> the present BEM.<br />
S3.5: Different advanced aspects in damage modeling Thu, 13:30–15:30<br />
Chair: Maksim Zapara, Vladimir Shneider S1|03–116<br />
Strain induced damage <strong>of</strong> ductile materials under compression<br />
Maksim Zapara (TU Berlin), Nikolai Tutyshkin (<strong>Universität</strong> Tula, Russia), Wolfgang H. Müller,<br />
Ralf Wille (TU Berlin) Schedule<br />
The scheme <strong>of</strong> plastic compression has been successfully implemented in many metal forming<br />
processes and can be characterized by negative values <strong>of</strong> stress triaxiality. Damage mechanics<br />
considers ductile failure as a kinetic deterioration <strong>of</strong> the deformed material. The difficulties <strong>of</strong> the<br />
analysis <strong>of</strong> damage kinetics are related to the determination <strong>of</strong> the material functions which appear<br />
in the constitutive equations. Stress triaxiality under plastic compression varies considerably both<br />
over the specimen volume (in the meridian section) and over the strain path. The averaged values<br />
<strong>of</strong> stress triaxiality are commonly used for the analysis <strong>of</strong> plastic compression.<br />
In this paper the problem <strong>of</strong> ductile damage and failure prediction is solved by taking a change<br />
in stress triaxiality under plastic compression <strong>of</strong> cylindrical specimens made <strong>of</strong> low-carbon lowalloy<br />
steel, aluminum alloy, and pure copper into account. It is shown that such a more accurate<br />
assessment leads to a greater shift <strong>of</strong> stress triaxialities into a range <strong>of</strong> negative values (compared<br />
to their averaged values). At such values <strong>of</strong> stress triaxiality the material can be subjected to
86 Section 3: Damage and fracture mechanics<br />
plastic compression without failure under arbitrarily large deformations (due to the healing <strong>of</strong><br />
micro-defects). The constitutive equations <strong>of</strong> the tensorial framework for ductile damage recently<br />
developed by the authors are applied to modeling.<br />
Investigation <strong>of</strong> gradient-enhanced damage evolution in viscoplastic plates under propagating<br />
disturbance<br />
An Danh Nguyen, Marcus St<strong>of</strong>fel, Dieter Weichert (RWTH Aachen) Schedule<br />
This work investigates gradient-enhanced damage evolution by performing a parameter study for<br />
the authors’s finite element shell model, in which the free energy function is enhanced phenomenologically<br />
in terms <strong>of</strong> a non-local damage variable and its gradient on the mid-surface <strong>of</strong> shell<br />
structures. This enhancement gives rise to an introduction <strong>of</strong> gradient parameters in terms <strong>of</strong> a<br />
substructure-related intrisic length-scale and a relationship between non-local and local damage<br />
variable. Based on the global displacement-force curves obtained from shock-tube tests on aluminium<br />
plate specimens, the gradient parameters are determined to validate the proposed shell<br />
model. The influence <strong>of</strong> spatial gradient <strong>of</strong> loading on the material behaviour within a macroscopic<br />
continuum element will be discussed through several examples.<br />
Enhancement <strong>of</strong> the micro mechanical basis for local approach cleavage models<br />
Volker Hardenacke, Jörg Hohe (Fraunh<strong>of</strong>er IWM Freiburg) Schedule<br />
The present study is concerned with the investigation <strong>of</strong> the micro mechanisms <strong>of</strong> micro defect<br />
nucleation in ferritic steels in order to provide an enhanced basis for probabilistic cleavage models.<br />
Brittle fracture <strong>of</strong> ferritic steels is a probabilistic process, triggered by the failure <strong>of</strong> randomly<br />
distributed second phase particles. These particles fracture due to plastic deformation <strong>of</strong> the surrounding<br />
matrix, resulting in the nucleation <strong>of</strong> micro defects. Once nucleated, the local stress<br />
state controls the possible instability <strong>of</strong> the defects. In this context, the local stress triaxiality is<br />
assumed to govern the blunting <strong>of</strong> freshly nucleated micro cracks. By a micro mechanical modelling<br />
<strong>of</strong> the cleavage initiation process the effects and the interactions <strong>of</strong> the relevant parameters<br />
can be identified. For this purpose Representative Volume Elements (RVE) <strong>of</strong> the micro structure<br />
are utilised, accounting for both, the grain structure as well as the brittle particles at the<br />
grain boundaries. The RVEs are loaded based on the local mechanical field quantities determined<br />
numerically for different fracture mechanics specimen types at the cleavage origins. Thus, the<br />
behaviour <strong>of</strong> the particles against the micromechanical conditions can be specified, resulting in a<br />
better understanding <strong>of</strong> the processes at cleavage fracture initiation.<br />
Marciniak-Kuczynski type modelling <strong>of</strong> the effect <strong>of</strong> complex loading on the forming<br />
limits <strong>of</strong> sheet metal<br />
D.K.Teslenko, V.P.Shneider, Yu.A.Chernyakov (Dnepropetrovsk National University) Schedule<br />
Formability <strong>of</strong> sheet metal is limited to the beginning <strong>of</strong> localized shear or necking. In connection<br />
with the application value, recently interest to the problem <strong>of</strong> determining the maximum allowable<br />
strain in the biaxial tension <strong>of</strong> elastoplastic thin plates is increased. Most articles on this subject<br />
use the classical model <strong>of</strong> Marciniak-Kuczynski (MK) [1]. Later, in a number <strong>of</strong> studies, this<br />
model has been improved, allowing taking into account all possible orientations <strong>of</strong> localization,<br />
including through-thickness shear [2].<br />
Despite the substantial progress made in modeling the limiting conditions <strong>of</strong> formation, virtually<br />
all studies that describe the elastic-plastic behavior <strong>of</strong> materials are limited to using the<br />
simplest theories <strong>of</strong> plasticity. However, the processes <strong>of</strong> forming <strong>of</strong> sheet metal is generally accompanied<br />
by large deformations and complex loading and improving <strong>of</strong> prediction <strong>of</strong> sheet forming<br />
simulation <strong>of</strong>ten requires physically based model defining.
Section 3: Damage and fracture mechanics 87<br />
In this paper for describing the behavior <strong>of</strong> elastic-plastic material we use the theory <strong>of</strong> plasticity,<br />
taking into account microstrain [3].<br />
In the framework <strong>of</strong> this theory, a comparative analysis <strong>of</strong> the MK approach and the bifurcation<br />
analysis, followed by the construction <strong>of</strong> afterbifurcational solutions for the plate, are made.<br />
The dependences <strong>of</strong> the limit <strong>of</strong> formability <strong>of</strong> the material under load (with a given strain)<br />
on two-tier broken are calculated. A comparison <strong>of</strong> ultimate strains with the values obtained with<br />
the proportional deformation are made. It is shown that under non-proportional deformation the<br />
ultimate strain may increase. We studied the dependence <strong>of</strong> the formability limit under cyclic<br />
loading and ratcheting. It was found that in this case the limit <strong>of</strong> formability depends on the<br />
cyclic properties <strong>of</strong> the material and can both increase and decrease.<br />
[1] Marciniak, Z., Kuczynski, K. Limit strains in the processes <strong>of</strong> stretch-forming sheet metal,<br />
International Journal <strong>of</strong> Mechanical Sciences 9 (1967), 609620.<br />
[2] Eyckens P., Van Bael A., Van Houtte P. MarciniakKuczynski type modelling <strong>of</strong> the effect<br />
<strong>of</strong> Through-Thickness Shear on the forming limits <strong>of</strong> sheet metal, International Journal <strong>of</strong><br />
Plasticity 25 (2009), 22492268.<br />
[3] Kadashevich Yu.I., Chernyakov Yu.A. Theory <strong>of</strong> plasticity, taking into account micro stresses<br />
Advances in Mechanics 15 (1992), 3-39.<br />
Mechanical properties <strong>of</strong> hybrid composites made <strong>of</strong> a steel plate and a laminate<br />
connected with screw rivets<br />
Zolkiewski Slawomir (Silesian University <strong>of</strong> Technology) Schedule<br />
In this paper the research results <strong>of</strong> hybrid composite materials made <strong>of</strong> a steel plate and laminates<br />
will be presented. The tested composites were made <strong>of</strong> a metal sheet plate and a laminate<br />
plate connected with screw rivets. The laminates were made <strong>of</strong> three different types <strong>of</strong> fabrics<br />
with: fibreglass, carbon fibres and aramid fibres. As a warp, epoxide resin and polyester resin<br />
were used. The FML (fibre-metal laminate) hybrid composites connect advantages <strong>of</strong> metal sheet<br />
plates and laminates, especially locking <strong>of</strong> expansion <strong>of</strong> cracks on the composite surface (avoiding<br />
delamination) under multiple loading [1]. They also have very good force versus displacement<br />
characteristics, strain characteristics, percussive resistance and a strength versus total mass ratio.<br />
In the work the following characteristics and the juxtaposition <strong>of</strong> results <strong>of</strong> experimental tests will<br />
be presented. The application <strong>of</strong> the hybrid composite materials is very wide and popular. These<br />
composites can be applied in: connecting systems made <strong>of</strong> different fabrics, connecting systems<br />
with a large number <strong>of</strong> layers in their structure and in a system with a variety <strong>of</strong> configurations<br />
between metals and laminates. The experimental tests were carried out in the Dynamic Machines<br />
Laboratory on the dedicated laboratory stands. The laboratory stand consists <strong>of</strong> the carrying frame,<br />
fixing frame, manual hydraulic actuator and measuring elements: displacement sensor and/or<br />
extensometers [2] and force gauge. The laminates were the handmade ones and fabricated in the<br />
same conditions in the laboratory. This fact is important when comparing sample results. The<br />
maximal and minimal strains were derived and average strain was calculated. The strain in the<br />
time function graphs were presented. The tests relies on fixing <strong>of</strong> the specimen in the fixation<br />
frame and loading it by means <strong>of</strong> the manual hydraulic actuator. The specimen was fixed in<br />
the frame by hand screws. The force gauge was situated between the specimen and the manual<br />
hydraulic actuator. The force gauge U2B-50kN was used for force measurements. The specimen<br />
was loaded in the centre point with the force originating from the manual hydraulic actuator.
88 Section 3: Damage and fracture mechanics<br />
The displacement sensor WA L-20 was used on the other side <strong>of</strong> the laboratory stand. The extensometers<br />
were stuck on the specimen surface. The stand allows measuring the displacement<br />
<strong>of</strong> the centre point <strong>of</strong> the sample under the given load and displacements in a place where the<br />
extensometers were applied.<br />
[1] B. Surowska, Functional and hybrid materials in air transport, Eksploatacja i Niezawodnosc<br />
Maintenance and Reliability, 3 (2008), 30 – 40.<br />
[2] S. Zolkiewski, Laboratory Test Of The Composite Material Provided By Extensometer, Sev-<br />
NTU Journal, 110 (2010), 128 – 129.<br />
Predicting ductile fracture under multi-axial loading: comparison <strong>of</strong> modified Mohr-<br />
Coulomb with shear modified Gurson model<br />
Matthieu Dunand, Dirk Mohr (MIT and École Polytechnique) Schedule<br />
Substantial progress has been made over the past decade in characterizing and modeling the effect<br />
<strong>of</strong> the Lode angle parameter on ductile fracture at low stress triaxialities. In this talk, we compare<br />
the performance <strong>of</strong> shear-modified Gurson models with that <strong>of</strong> the Modified Mohr-Coulomb<br />
(MMC) damage indicator model in view <strong>of</strong> predicting the onset <strong>of</strong> fracture over a wide range <strong>of</strong><br />
stress-states. The experimental program on TRIP780 steel sheets includes notched tension tests,<br />
a punch test and combined tension/shear experiments on butterfly specimens. It is found that<br />
onset <strong>of</strong> fracture in all nine experiments is predicted correctly by the MMC fracture model. The<br />
predictions <strong>of</strong> the shear-modified Gurson model are found to be less accurate. The differences and<br />
shortcomings <strong>of</strong> both models are discussed in detail along with important underlying experimental<br />
challenges.<br />
Keywords: Ductile fracture, stress triaxiality, Lode angle,
Section 4: Structural mechanics 89<br />
Section 4: Structural mechanics<br />
Organizers: Christian Hellmich (TU Wien), Martin Schagerl (Johannes Kepler <strong>Universität</strong><br />
Linz)<br />
S4.1: Numerical Methods 1 Tue, 13:30–15:30<br />
Chair: Jochen Hebel S2|02–C205<br />
An Efficient Scheme for Stochastic Finite Element Solutions<br />
Philipp-Paul Jablonski, Udo Nackenhorst (<strong>Universität</strong> Hannover) Schedule<br />
Results from computational mechanics analysis are unsure due to uncertain model parameters<br />
like boundary conditions, constitutive models and process development. Increasing computer performance<br />
and sophisticated modeling approaches enable for stochastic analysis <strong>of</strong> mechanical<br />
processes. However, a broad variety <strong>of</strong> methods for the treatment <strong>of</strong> stochastic partial differential<br />
equations are under discussion in the related literature.<br />
In this presentation the concept <strong>of</strong> Polynomical Chaos expansion is investigated with regard<br />
to the analysis <strong>of</strong> welded steel joints. The constitutive parameters in the zone <strong>of</strong> interest are<br />
assumed to be uncertain with a priory statistical distribution.<br />
With regard to the computational efficiency it has to be notices, that with each stochastic<br />
variable an additional infinite dimension is added to the problem. In order to treat these problems<br />
within a finite element computational framework, a novel staggered iterative scheme is suggested<br />
to solve the resulting linear system. Furthermore, sophisticated schemes for the postprocessing,<br />
e.g. the computation <strong>of</strong> equivalent stresses from uncertain displacement fields and uncertain material<br />
properties will be introduced.<br />
Computational results are compared with results obtained from well defined experimental<br />
investigations. The fatigue under cyclic loading will be discussed.<br />
Application <strong>of</strong> isogeometric analysis to domain decomposition and phase separation<br />
problems<br />
Christian Hesch, Peter Betsch (<strong>Universität</strong> Siegen) Schedule<br />
During the past decate various new spatial discretization techniques have been developed. In<br />
particular, the usage <strong>of</strong> NURBS based shape functions, well known to the CAD community, has<br />
been adapted to finite element technology, used to solve different types <strong>of</strong> PDEs.<br />
Within this talk we concentrate on two different aspects: First, we search for a remedy <strong>of</strong> a<br />
major drawback <strong>of</strong> NURBS based shape functions: The discretization relies on a specific index<br />
space, imposing restrictions to h-refinements and the possible geometry. In the field <strong>of</strong> CAD<br />
applications this is resolved by using unconnected patches or by introducing T-Splines. Contrary<br />
to the mentioned solutions for CAD applications, we resolve this by introducing a variational<br />
consistent and non conform domain decomposition method, based on Mortar projections <strong>of</strong> the<br />
displacement field.<br />
Second, we search for the limitations <strong>of</strong> NURBS based shape functions. In particular, a specific<br />
higher order phase separation model, based on the Cahn-Hilliard model, is discretized with C 1<br />
continuous NURBS in space and a modified mid-point type discretization scheme in time. It turns<br />
out, that the spatial discretization imposes restrictions to the time integration if applied to this<br />
type <strong>of</strong> transport equations.<br />
Bayesian Inference <strong>of</strong> Linear Time-Varying Systems Based on Hilbert-Huang Transform<br />
Han Hu, Carsten Proppe (KIT) Schedule
90 Section 4: Structural mechanics<br />
This paper proposes an identification method for general linear time-varying MDOF systems<br />
(including chainlike and non-chainlike systems) based on the Hilbert-Huang Transform. The main<br />
procedures <strong>of</strong> the identification for system with n degrees <strong>of</strong> freedom are: First, by using Bayesian<br />
Inference and a Transitional Markov Chain Monte Carlo algorithm, initial knowledge about the<br />
free vibration system responses and the white noise in system responses is updated based on<br />
measured system responses, which yields the posterior distributions <strong>of</strong> the noise parameters.<br />
Second, each sample system responses are obtained in accordance with the posterior distribution<br />
and are processed by Hilbert-Huang Transform in order to obtain n intrinsic mode functions<br />
(IMFs) and the residue as well as the corresponding n analytical IMFs and the analytical residue<br />
for each degree <strong>of</strong> freedom. Finally, the above signals for each degree <strong>of</strong> freedom are summed<br />
respectively to form new responses and new analytical responses for each set <strong>of</strong> sample system<br />
responses, which are then used in the proposed identification equations to identify the distributions<br />
<strong>of</strong> system parameters.<br />
The proposed method is applied to chainlike and non-chainlike linear time-varying systems with<br />
three types <strong>of</strong> stiffness variations: smooth, abrupt and periodical variations. The effectiveness and<br />
accuracy <strong>of</strong> the proposed method on SDOF and MDOF systems is discussed in numerical simulations.<br />
System responses are perturbed by white noise, and the identified results demonstrate the<br />
robustness <strong>of</strong> the method.<br />
Keywords: System identification, Linear systems, Special transforms (Legendre, Hilbert, etc.),<br />
Bayesian inference, Transitional Markov Chain Monte Carlo algorithm<br />
Energy-consistent time-integration for a dynamic finite deformation thermoviscoelastic<br />
continuum<br />
Melanie Krüger (<strong>Universität</strong> Siegen), Michael Groß (TU Chemnitz), Peter Betsch (<strong>Universität</strong><br />
Siegen) Schedule<br />
The main goal <strong>of</strong> the present paper is the description <strong>of</strong> a dynamic finite deformation thermoviscoelastic<br />
continuum in the enhanced GENERIC (General equations for non-equilibrium reversible<br />
irreversible coupling) format, which is based on the works <strong>of</strong> Romero [1] (thermoelasticity)<br />
and a work <strong>of</strong> Krüger et al. [2] (enhanced GENERIC for masspoint systems). The time integration<br />
for the energy-momentum consistent or thermodynamically consistent system is done with<br />
partitioned discrete derivatives, which are well known from Gonzalez [3]. The underlying structure,<br />
in which the system <strong>of</strong> partial differential equations is described, is the enhancement <strong>of</strong> the<br />
so called GENERIC format. This GENERIC format was introduced by Öttinger [4] for thermoelastodynamic<br />
systems. The considered variables <strong>of</strong> the system are the Poissonian variables, which<br />
are here the linear momentum, the configuration, the entropy and the internal variable.<br />
The thermo-viscoelastic continuum needs two constitutive equations for the thermoelastic and<br />
viscoelastic part <strong>of</strong> the system. The thermal evolution equation is described with Fourier’s law <strong>of</strong><br />
isotropic heat conduction and the viscous part is given by an fourth order compliance tensor.<br />
The enhanced numerical stability <strong>of</strong> the newly developed structure-preserving integrators in<br />
comparison to standard integrators is demonstrated by means <strong>of</strong> numerical examples.<br />
[1] I. Romero, Algorithms for coupled problems that preserve symmetries and the laws <strong>of</strong> thermodynamics,<br />
Part I: Monolithic integrators and their application to finite strain thermoelasticity,<br />
Computer Methods in Applied Mechanics and Engineering, 2010, 199:1841-1858<br />
[2] M. Krüger, M. Groß and P. Betsch, Energy-consistent time-integration for dynamic finite<br />
deformation thermo-viscoelasticity, PAMM, 2011, submitted for publication
Section 4: Structural mechanics 91<br />
[3] O. Gonzalez, Design and analysis <strong>of</strong> conserving integrators for nonlinear Hamiltonian systems<br />
with symmetry, Ph.D. Thesis, Department <strong>of</strong> Mechnical Engineering, Stanford University,<br />
1996<br />
[4] H.C. Öttinger, Beyond equilibrium thermodynamics, Wiley, New York, 2005<br />
System Identification based on Selective Sensitivity Analysis<br />
Billmaier Maximilian, Bucher Christian (TU Wien) Schedule<br />
Dynamical measurements are applied to assess structural reliability in the context <strong>of</strong> health<br />
monitoring or design evaluation. However, system identification requires the solution <strong>of</strong> inverse<br />
problems, which usually leads to rather ill-conditioned formulations.<br />
The selective sensitivity analysis provides a way out <strong>of</strong> this dilemma. In this analysis, the output<br />
<strong>of</strong> a structure is only sensitive to a few model parameters (to be identified), but insensitive to the<br />
others.<br />
These essential few parameters are then identified by applying selective sensitive excitations. It is<br />
shown that the updating algorithms for selective sensitive excitations are always better conditioned<br />
than those for any other excitation combination. A limitation <strong>of</strong> this method has <strong>of</strong>ten been<br />
called the realization <strong>of</strong> theoretically derived excitations in dynamical experiments.<br />
In a first laboratory application, the analysis is applied. With only a very limited prior knowledge<br />
<strong>of</strong> the structure, a robust converging mathematical model is presented. It is shown that the<br />
selective sensitive excitations can be experimentally realized in a convenient approach.<br />
Adaptive FEM with Stabilized Elements for Parameter Identification <strong>of</strong> Incompressible<br />
Hyperelastic Materials<br />
Kai-Uwe Widany, Rolf Mahnken (<strong>Universität</strong> Paderborn) Schedule<br />
This work is concerned with the identification <strong>of</strong> material parameters for isotropic, incompressible<br />
hyperelastic material models. Besides the principal stretch-based strain-energy function by Ogden<br />
an invariant-based strain-energy function by Rivlin/Saunders is considered for which parameter<br />
sensitivities are derived. The identification is formulated as a least-squares minimization problem<br />
based on the finite element method to account for inhomogeneous states <strong>of</strong> stresses and strains<br />
in the experimental data which is obtained by optical measurements [2]. For the finite element<br />
method low-order tetrahedral elements in a mixed displacement-pressure formulation with stabilization<br />
are considered [3]. Special attention is payed to an adaptive mesh-refinement based on a<br />
goal-oriented a posteriori error indicator to gain reliable material parameters [1]. To approximate<br />
error terms an element-wise recovery technique based on enhanced gradients is introduced.<br />
[1] R. Becker, B. Vexler, A posteriori error estimation for finite element discretization <strong>of</strong> parameter<br />
identification problems. Numerische Mathematik 96(3) (2004), 435 – 459.<br />
[2] R. Mahnken, E. Stein, Parameter identification for finite deformation elasto-plasticity in<br />
principal directions. Comp. Meths. Appl. Mech. Eng. (1997) 147, 17 – 39.<br />
[3] K.-U. Widany, I. Caylak, R. Mahnken, Stabilized Mixed Tetrahedrals with Volume and Area<br />
Bubble Functions at Large Deformations, Proc. Appl. Math. Mech. 10 (2010), 227 – 228.<br />
S4.2: Numerical Methods 2 Tue, 16:00–18:00<br />
Chair: Vadim Potapov S2|02–C205
92 Section 4: Structural mechanics<br />
Incompatible Modes for Volumetric Shell Elements in Explicit Time Integration<br />
Steffen Mattern, Christoph Schmied, Karl Schweizerh<strong>of</strong> (KIT) Schedule<br />
Explicit time integration methods as the widely-used central difference scheme are characterized<br />
by efficient vector equations on the global level due to the application <strong>of</strong> diagonalized mass<br />
matrices. Together with a limitation <strong>of</strong> the time step size by a critical value, this leads to a<br />
domination <strong>of</strong> the numerical effort on element level.<br />
Volumetric shell elements as presented e. g. in [1], are formulated only with displacement<br />
degrees <strong>of</strong> freedom and hence allow the simulation <strong>of</strong> shell-like structures with full representation<br />
<strong>of</strong> its continuum properties. As all lower order displacement based element formulations with<br />
standard numerical integration, they show artificial stiffness effects, the so-called locking. One<br />
well-known strategy for the treatment <strong>of</strong> locking is the enhanced assumed strain (EAS) method [2],<br />
based on an enhancement <strong>of</strong> the compatible strain field by introducing additional degrees <strong>of</strong><br />
freedom, which are condensed-out by local equation solving. This leads to a significant increase <strong>of</strong><br />
the numerical effort on element level. The method <strong>of</strong> incompatible modes (IM) has originally been<br />
the basis for the variational principle presented in [2]. As presented in [3] for 2D-plane elements,<br />
it is possible to generally formulate the method in order to reproduce any EAS-element with<br />
corresponding incompatible modes also for the 3D volumetric shell elements. In order to achieve<br />
an efficient element formulation, the additional displacement degrees <strong>of</strong> freedom are treated as<br />
regular unknowns in the global equations, so the formulation <strong>of</strong> a diagonalized mass matrix for<br />
the additional degrees <strong>of</strong> freedom has to be discussed.<br />
The implementation <strong>of</strong> efficient element routines is supported by the programming tool Ace-<br />
Gen [4], which allows the application <strong>of</strong> symbolic operations and the generation <strong>of</strong> highly optimized<br />
program code. Both EAS- and IM-elements are implemented using AceGen and compared<br />
regarding the treatment <strong>of</strong> locking effects and their numerical performance.<br />
[1] R. Hauptmann & K. Schweizerh<strong>of</strong>: A systematic development <strong>of</strong> ‘solid-shell’ element formulations<br />
for linear and non-linear analyses employing only displacement degrees <strong>of</strong> freedom,<br />
IJNME, 42(1): 49–69, 1998.<br />
[2] J.C. Simo & M.S. Rifai: A class <strong>of</strong> mixed assumed strain methods and the method <strong>of</strong> incompatible<br />
modes, IJNME, 29(8): 1595–1638, 1990.<br />
[3] M. Bisch<strong>of</strong>f & I. Romero: A generalization <strong>of</strong> the method <strong>of</strong> incompatible modes, IJNME,<br />
69(9): 1851–1868, 2007.<br />
[4] J. Korelc: http://www.fgg.uni-lj.si/Symech/, 2011.<br />
Solid-shell finite elements for tesselated geometries<br />
Johannes Wimmer, Stefanie Reese (RWTH Aachen) Schedule<br />
Tesselated folded sheets have a multitude <strong>of</strong> applications in sandwich panel cores or impact absorbing<br />
elements while allowing for additional functionality like cooling and moisture removal.<br />
Particularly in transportation industry applications, the lightweight but stiff combination <strong>of</strong> tesselated<br />
cores with smooth top and bottom sheets is <strong>of</strong> huge interest. Furthermore, these structures<br />
are very economical in terms <strong>of</strong> usage <strong>of</strong> raw materials.<br />
The tesselation can be chosen to fulfil specific structural requirements, but the production <strong>of</strong><br />
these tailor-made sheets has proven to be troublesome. E.g. zig-zag fold-patterns cause a strong<br />
coupling between the facets and the transformation from a planar to a three-dimensional structure
Section 4: Structural mechanics 93<br />
leads to significant biaxial contraction. In order to reduce time- and cost-intensive prototype production,<br />
finite element analysis can provide an alternative to experimental testing, but this only<br />
holds if the representation <strong>of</strong> both the structure and the material behaviour is sufficiently accurate.<br />
Currently, typical simulations make use <strong>of</strong> standard finite elements, which are based on the<br />
classical shell, beam or plate theory, respectively. High requirements towards precision, especially<br />
for the transverse stress distribution, yield a high computational effort. Here, the solid-shell concept<br />
provides an alternative with potential benefits in accuracy and performance.<br />
In addition, solid-shell elements can overcome several numerical difficulties in finite element<br />
simulations, such as locking phenomena. Volumetric, as well as membrane and thickness locking<br />
are removed directly within the solid-shell formulation. Application <strong>of</strong> the assumed natural strain<br />
concept provides a remedy for the transverse shear and curvature thickness locking. Furthermore,<br />
we use reduced integration together with hourglass stabilisation.<br />
Thus, the proposed elements are quite attractive from a numerical point <strong>of</strong> view due to their<br />
computational efficiency and provide a suitable approach to the representation <strong>of</strong> tesselated sheets.<br />
Keywords: tesselated geometry, folded sheet, solid-shell, locking<br />
Coupled multiscale finite element analysis <strong>of</strong> shell structures<br />
Jochen Hebel, Friedrich Gruttmann (TU <strong>Darmstadt</strong>) Schedule<br />
In this study, a coupled multiscale finite element procedure (FE 2 ) for the analysis <strong>of</strong> shell structures<br />
is proposed. On the macrolevel, a shell element with Reissner-Mindlin kinematic assumptions<br />
is employed. On the microlevel, a representative volume element (RVE) ranging through the full<br />
shell thickness is formulated. Numerical homogenisation in terms <strong>of</strong> shell stress resultants and<br />
strains is used for coupling both scales. The resulting moduli are obtained by means <strong>of</strong> static<br />
condensation <strong>of</strong> the internal degrees <strong>of</strong> freedom <strong>of</strong> the RVE. The finite element analyses on the<br />
microlevel are solved efficiently in a parallel manner. A fully three-dimensional stress state is<br />
obtained from the microproblem allowing an accurate analysis <strong>of</strong> even thick shells or composite<br />
sections including inelastic material behaviour. Numerical examples demonstrate the effectiveness<br />
and efficiency <strong>of</strong> the approach.<br />
An Extended Product Ansatz for the Computation <strong>of</strong> Interlaminar Stresses in a<br />
Mixed Finite Element<br />
M. Schürg, J. Wackerfuß, F. Gruttmann (TU <strong>Darmstadt</strong>) Schedule<br />
In this paper we enlarge on an extended shell kinematic which is implemented in a mixed four-node<br />
shell element and described in detail in [1]. It is able to describe the complete three-dimensional<br />
strain state. An extended product ansatz is introduced, so that additionally to the conventional<br />
degrees <strong>of</strong> freedom <strong>of</strong> the shell based on the Reissner-Mindlin theory with inextensible director<br />
vector also warping and thickness changes can be described. For the second part, it is considered<br />
that the derivatives to the two coordinates in the plane are zero. In the context <strong>of</strong> the related<br />
finite element formulation this leads to values that are constant in each element.<br />
In this paper we consider that the derivatives to the two coordinates are not zero and describe<br />
the corresponding finite element equations. In the context <strong>of</strong> the used finite element implemention,<br />
this approach leads to a higher number <strong>of</strong> degrees <strong>of</strong> freedom on element level and it means that<br />
an ansatz in the domain has to be made. The results <strong>of</strong> the two considerations are compared.<br />
[1] M. Schürg, J. Wackerfuß, F. Gruttmann, Using A Mixed Shell Formulation To Compute
94 Section 4: Structural mechanics<br />
Interlaminar Stresses In Layered Composite Shell Structures, 3rd ECCOMAS Thematic<br />
Conference on the Mechanical Response <strong>of</strong> Composites 21st - 23rd September (2011).<br />
Solving hyperelastic problems using mixed LSFEM<br />
Karl Steeger, Alexander Schwarz, Jörg Schröder (<strong>Universität</strong> Duisburg-Essen), Gerhard Starke,<br />
Benjamin Müller (<strong>Universität</strong> Hannover) Schedule<br />
The focus <strong>of</strong> this contribution is the solution <strong>of</strong> hyperelastic problems using the least-squares<br />
finite element method (LSFEM). In particular a mixed least-squares finite element formulation is<br />
provided and applied on geometrically nonlinear problems. The basis for the element formulation is<br />
a div-grad first order system consisting <strong>of</strong> the equilibrium condition and the constitutive equation<br />
both written in a residual form. An L2-norm is adopted on the residuals leading to a functional<br />
depending on displacements and stresses which has to be minimized. Therefore the first variations<br />
with respect to both free variables have to be zero. The solution can then be found by applying<br />
Newton’s Method. For the continuous approximation <strong>of</strong> the displacements in W 1,p with p > 2,<br />
standard polynomials are used. Shape functions belonging to a Raviart-Thomas space are applied<br />
for the stress interpolation. These vector-valued functions ensure a conforming discretization <strong>of</strong><br />
the Sobolev space H(div, Ω). Finally the proposed formulation is tested on several numerical<br />
examples.<br />
FEM system matrix modifications for structural optimization problems<br />
Andreas Wagner, Gottfried Spelsberg-Korspeter, Peter Hagedorn (TU <strong>Darmstadt</strong>) Schedule<br />
Design engineers frequently rely on the finite element method since it <strong>of</strong>fers a broad range <strong>of</strong><br />
possibilities and is available in many powerful commercial tools. Also, finite element models can<br />
be a basis for structural optimization. There are many optimization strategies and tools available,<br />
however, if the finite element method is used in the context <strong>of</strong> structural optimization, it is <strong>of</strong>ten<br />
necessary to change the mesh <strong>of</strong> the structure in every or at least some optimization steps. In order<br />
to avoid this remeshing process, a new modeling approach for structures with modifications is<br />
proposed. The approach can be <strong>of</strong> great advantage if the optimization aims for global properties<br />
<strong>of</strong> the structure, e.g. the distribution <strong>of</strong> eigenfrequencies, and not local properties like stress<br />
concentrations. The basic idea <strong>of</strong> the approach is to combine separate finite element meshes <strong>of</strong><br />
the basis structure and <strong>of</strong> the modifications by kinematical relations, leading to mass and stiffness<br />
matrices <strong>of</strong> the complete structure. The approach will be demonstrated by a concise example.<br />
S4.3: Shells and Plates Wed, 13:30–15:30<br />
Chair: Wolfgang Müller S2|02–C205<br />
Some geometrically nonlinear problems <strong>of</strong> thin periodic plates<br />
Jarosław Jędrysiak, Łukasz Domagalski, Michał Gajdzicki (Technical University <strong>of</strong> Łódź) Schedule<br />
Thin plates with periodic structure in planes parallel to the midplane are considered in this note.<br />
In these plates we can distinguish many small, repeated elements called periodic cells, treated<br />
as thin plates. The size <strong>of</strong> periodic, being a diameter <strong>of</strong> the cell, is called the microstructure<br />
parameter l. It is assumed that on the microlevel properties <strong>of</strong> these plates are described by<br />
periodic, highly oscillating, non-continuous functions. Such plates are called periodic plates.<br />
Deflections <strong>of</strong> these plates are <strong>of</strong> the order <strong>of</strong> their thickness. Hence, they are usually analysed<br />
in the framework <strong>of</strong> geometrically nonlinear theories, such as the well-known von Karman theory,<br />
cf. [6]. But, for thin periodic plates the obtained governing equations have highly-oscillating, pe-
Section 4: Structural mechanics 95<br />
riodic, non-continuous functional coefficients. Thus, it is rather difficult to apply these equations<br />
to investigate special problems. In order to replace these equations by equations with constant<br />
coefficients, various averaging techniques are used, e.g. asymptotic homogenization, cf. [4]. Unfortunately,<br />
obtained governing equations usually neglect the effect <strong>of</strong> the microstructure size.<br />
To avoid this drawback the tolerance averaging technique can be applied, proposed and developed<br />
to analyse periodic composites and structures in a series <strong>of</strong> papers, e.g. for thin periodic<br />
plates in [3], for periodic plates with a moderately thickness in [1], for periodic wavy-type plates<br />
in [5], for periodic shells in [7]. An extended list <strong>of</strong> publications related to applications <strong>of</strong> this<br />
approach can be found in the books [9, 8].<br />
In this paper the governing equations with constant coefficients <strong>of</strong> the tolerance model for elastostatics<br />
<strong>of</strong> periodic geometrically non-linear plates are applied to analyse some special problems,<br />
cf. [2]. Moreover, results obtained in the framework <strong>of</strong> the proposed tolerance model and using<br />
the orthogonality method are compared to results calculated using the finite element method.<br />
[1] BARON E.: On modelling <strong>of</strong> periodic plates having the inhomogeneity period <strong>of</strong> an order <strong>of</strong><br />
the plate thickness, J. Theor. Appl. Mech., 44, 2006, 3-18.<br />
[2] DOMAGALSKI Ł., JĘDRYSIAK J.: Modelling <strong>of</strong> thin periodic plates subjected to large<br />
deflections, Civ. Env. Eng. Rep., 5, 2010, 121-136.<br />
[3] JĘDRYSIAK J.: Dispersive models <strong>of</strong> thin periodic plates, Łódź, Wyd. Politechniki Łódzkiej<br />
2001, (in Polish).<br />
[4] KOHN R.V., VOGELIUS M.: A new model <strong>of</strong> thin plates with rapidly varying thickness,<br />
Int. J. Solids Struct., 20, 1984, 333-350.<br />
[5] MICHALAK B.: The meso-shape functions for the meso-structural models <strong>of</strong> wavy-plates,<br />
ZAMM, 81, 2001, 639-641.<br />
[6] TIMOSHENKO S., WOINOWSKY-KRIEGER S.: Theory <strong>of</strong> plates and shells, New York,<br />
McGraw-Hill 1959.<br />
[7] TOMCZYK B.: A non-asymptotic model for the stability analysis <strong>of</strong> thin biperiodic cylindrical<br />
shells., Thin Walled Struct., 45, 2007, 941-944.<br />
[8] WOŹNIAK CZ., ET AL. [eds]: Mathematical modelling and analysis in continuum mechanics<br />
<strong>of</strong> microstructured media, Gliwice, Wyd. Politechniki Śląskiej 2010.<br />
[9] WOŹNIAK CZ., MICHALAK B., JĘDRYSIAK J. [eds]: Thermomechanics <strong>of</strong> microheterogeneous<br />
solids and structures, Łódź, Wyd. Politechniki Łódzkiej 2008.<br />
Analysis <strong>of</strong> notches and cracks in circular Kirchh<strong>of</strong>f plates using the scaled boundary<br />
finite element method<br />
Rolf Dieringer, Wilfried Becker (TU <strong>Darmstadt</strong>) Schedule<br />
In this contribution, a new formulation <strong>of</strong> the scaled boundary finite element method (SBFEM)<br />
is presented for the analysis <strong>of</strong> circular plates in the framework <strong>of</strong> Kirchh<strong>of</strong>f’s plate theory. The<br />
basic characteristic <strong>of</strong> the method is that a domain is described by the mapping <strong>of</strong> its boundary<br />
with respect to a scaling centre. The governing partial differential equations are transformed into<br />
scaled boundary coordinates and are reduced to a set <strong>of</strong> ordinary differential equations applying
96 Section 4: Structural mechanics<br />
a discrete form <strong>of</strong> the Kantorovich reduction method. If the scaling centre is selected at the crack<br />
tip, the SBFEM enables the effective and precise calculation <strong>of</strong> stress intensity factors <strong>of</strong> cracked<br />
and notched structures, solving the corresponding eigenvalue problem. Although the method has<br />
been applied successfully to many problems <strong>of</strong> continuum mechanics, its application to plate<br />
bending problems is rather unexploited. The study provides the employment <strong>of</strong> the method for<br />
the static analysis <strong>of</strong> circular plates using Kirchh<strong>of</strong>f kinematics. The element stiffness matrices<br />
for bounded and unbounded media are derived. Numerical examples show the performance and<br />
efficiency <strong>of</strong> the method, applied to plate bending problems.<br />
Stress concentrations at free edges <strong>of</strong> shear webs<br />
Christoph Kralovec, Kai-Uwe Schröder, Martin Schagerl (<strong>Universität</strong> Linz) Schedule<br />
Shear webs with free edges occur frequently in lightweight constructions. A typical example in aircraft<br />
design is the attachment <strong>of</strong> the circumferential frames to the fuselage skin. This attachment<br />
is predominately loaded by the shear between the frame and skin. The web <strong>of</strong> this attachment<br />
is interrupted by so-called “mouse-holes” at crossing <strong>of</strong> the stringers, so that the longitudinal<br />
stringers can run through without interruption. Due to these holes the web has free edges at the<br />
stringer positions. The other two opposite edges <strong>of</strong> the web are loaded by shear, which is brought<br />
in by the frame and the skin, respectively. In this short communication we discuss the in-plane<br />
strength <strong>of</strong> the shear web under these loading and boundary conditions. For analysis we use both,<br />
analytical and numerical considerations.<br />
For our study we consider a rectangular plate, which is loaded by shear on two simply supported<br />
opposite sides. The other opposite sides can move freely and remain unloaded. Analyzing the<br />
plates in-plane stress state it is obvious that at the corners the maximum equivalent stress occurs.<br />
If no buckling occurs this stress determines the strength <strong>of</strong> the plate. However, the evaluation <strong>of</strong><br />
the stress-state at the corners raises some difficulties, as at these points the loaded and unloaded<br />
edges meet, which indicates the development <strong>of</strong> stress concentrations.<br />
A comparative study <strong>of</strong> deformations <strong>of</strong> elastic-viscoplastic plates using different<br />
structural hypotheses<br />
Marcus St<strong>of</strong>fel, Duy Thang Vu, Rüdiger Schmidt, Dieter Weichert, (RWTH Aachen) Schedule<br />
In the present study the geometrically and physically non-linear response <strong>of</strong> ductile structures<br />
under shock wave loading conditions is investigated. The considered elastic-viscoplastic deformations<br />
are occurring during time ranges <strong>of</strong> several microseconds. A finite element algorithm <strong>of</strong><br />
the transient structural response is based on shell theories taking first- and third-order transverse<br />
shear deformations into account. In order to consider material non-linear effects, viscoplastic<br />
constitutive equations are combined with the structural theory. The aim is to determine which<br />
structural model predicts deformations under blast loading conditions most accurately. For this<br />
reason, an experimental investigation with developed shock tubes is introduced as well. By subjecting<br />
pressure waves in shock tubes to plate specimens, deflections and loading histories can be<br />
measured during the impulse period and can be compared to simulation results.<br />
Analysis <strong>of</strong> magnetoelectric laminated plates using a coupled zig-zag model<br />
C.L. Zhang (<strong>Universität</strong> Siegen/Zhejiang University Hangzhou), W.Q. Chen (Zhejiang University<br />
Hangzhou), Chuanzeng Zhang (<strong>Universität</strong> Siegen) Schedule<br />
Two-dimensional equations (2D) for the analysis <strong>of</strong> magnetoelectric laminated (MEL) plates are<br />
derived based on a coupled zig-zag model. A layer-wise linear zig-zag approximation is adopted<br />
for the in-plane displacements and the transverse displacement is approximated by taking<br />
account <strong>of</strong> the normal strain in the thickness direction <strong>of</strong> the MEL plates as a result <strong>of</strong> the piezo-
Section 4: Structural mechanics 97<br />
electric/piezomagnetic coupling effects. The electrical and magnetic potentials in each layer are<br />
assumed to be a piecewise quadratic function across the thickness. Numerical examples will be<br />
presented and discussed to compare the present theory with the available 2D theories <strong>of</strong> MEL<br />
plates and investigate the static behavior <strong>of</strong> simply supported MEL plates under different loads.<br />
S4.4: Composites and Structured Materials Wed, 16:00–18:00<br />
Chair: Jaroslaw Jedrysiak S2|02–C205<br />
Numerical modelling <strong>of</strong> layered composite struts<br />
C. Völlmecke, W.H. Müller (TU Berlin) Schedule<br />
Composite components are on the forefront in most engineering applications these days. They<br />
are increasingly employed in a broad range <strong>of</strong> applications from mechanical via structural engineering<br />
components to marine and aerospace applications. In particular they are utilized when<br />
lightweight principles are a dominant design criteria since they possess a high stiffness-to-weight<br />
ratio. Thereby they effectively reduce a structures overall weight whilst allowing for loadings to be<br />
transferred efficiently. However, owing to the manufacturing process <strong>of</strong> laminating several layers<br />
<strong>of</strong> fibre-matrix plies interlaminar defects may occur. Once this so-called delamination is present,<br />
the residual capacity <strong>of</strong> a component may be severely affected under compression.<br />
In order to investigate the effects <strong>of</strong> an interlaminar defect on the buckling and postbuckling<br />
behaviour <strong>of</strong> a strut, a numerical representation <strong>of</strong> a delaminated strut is developed based on a<br />
previously developed analytical model. The underlying variational formulations are derived based<br />
on continuum mechanics. The model is then discretized using an open source finite element<br />
code and investigated carefully whilst varying system parameters. Subsequently the results are<br />
validated against a previously developed analytical model. The numerical model allows a very<br />
efficient investigation <strong>of</strong> the behaviour <strong>of</strong> the delaminated component. Moreover, the requirement<br />
<strong>of</strong> imposing imperfections is superfluous which is usually necessary when the (post-) buckling<br />
behaviour <strong>of</strong> structures is attempted to be simulated via finite elements.<br />
Modal Response Design for Efficient Configuration Control <strong>of</strong> Bistable Structures<br />
Andres F. Arrieta, Peter Hagedorn (TU <strong>Darmstadt</strong>) Schedule<br />
Composite laminates are becoming increasingly important in a wide variety <strong>of</strong> applications, particularly<br />
in aerospace engineering. Within this context, anisotropic composites allowing for a<br />
high degree <strong>of</strong> directional stiffness tailoring are increasingly been developed as a solution for the<br />
conflicting aerospace requirements <strong>of</strong> light-weight and high-strength structural materials. This<br />
capability in the design <strong>of</strong> aerospace structures is particularly important to achieve conformal<br />
change <strong>of</strong> shape, or morphing. This idea has attracted much attention from researchers within<br />
the aerospace community given the <strong>of</strong>fered potential performance gains and, in particular, the<br />
possibility <strong>of</strong> augmented optimal operation over a wide range <strong>of</strong> different mission objectives and<br />
environmental conditions. One example <strong>of</strong> structural materials <strong>of</strong>fering the stated capabilities are<br />
multi-stable composites. These composite laminates are structures capable <strong>of</strong> adopting multiple<br />
statically stable configurations [1]. The multi-stability property has drawn considerable attention<br />
from the adaptive structure community for its potential applications in morphing structures, as<br />
no energy is required to hold each <strong>of</strong> the stable configurations [2]. The mechanism for changes<br />
between stable states known as snap-through is strongly nonlinear in nature, resulting on rich<br />
dynamic behaviour. Recently, the idea to exploit the dynamics <strong>of</strong> bistable composites, a class <strong>of</strong><br />
multi-stable composites, to allow for less energy intensive actuation, and hence lighter actuators,<br />
has been proposed showing encouraging results [3].
98 Section 4: Structural mechanics<br />
In this paper the structural tailoring <strong>of</strong> the dynamic response <strong>of</strong> multi-stable composites<br />
to obtain desired modal properties to allow for easier actuation is proposed. The response is<br />
design such that resonant oscillations are easily induced in order to trigger controlled snapthrough,<br />
i.e. changes between stable states, <strong>of</strong> the multi-stable structures resulting in minimum<br />
actuation effort. In this work the effects on the dynamic response <strong>of</strong> varying dimensions, stacking<br />
sequence and discrete inclusions adding inertia or stiffness are studied for bistable composites. In<br />
particular, the effect <strong>of</strong> introducing asymmetry in the structure to ensure the responses <strong>of</strong> each<br />
stable configuration are slightly different avoiding complex dynamics involving constant snapthrough,<br />
such as large amplitude limit cycles or chaotic oscillations, is studied. The effect <strong>of</strong><br />
the attached flexible piezoelectric actuators on the dynamics <strong>of</strong> the morphing structures is also<br />
considered and used to achieve minimum morphing actuation.<br />
[1] M. W. Hyer. Some observations on the cured shapes <strong>of</strong> thin unsymmetric laminates. Journal<br />
<strong>of</strong> Composite Materials, 15:175194, 1981.<br />
[2] C. G. Diaconu, P. M. Weaver, and F. Mattioni. Concepts for morphing airfoil sections using<br />
bi-stable laminated composite structures. Thin-Walled Structures, 46:689701, 2008.<br />
[3] A. F. Arrieta, D. J. Wagg, and S. A. Neild. Dynamic snap-through for morphing <strong>of</strong> bi-stable<br />
composite plates. Journal <strong>of</strong> Intelligent Material Systems and Structures, 22:103112, 2011.<br />
Microstructural Model <strong>of</strong> a Closed-Cell Foam on the Basis <strong>of</strong> Image Analysis<br />
Nina-Carolin Fahlbusch, Wilfried Becker (TU <strong>Darmstadt</strong>) Schedule<br />
Polymer foams combine an excellent weight-specific stiffness and strength with advantageous properties<br />
such as a low density, thermal conductivity and cost-effective production. Therefore, they<br />
are suited for many lightweight applications. The focus <strong>of</strong> this work is the identification <strong>of</strong> a unit<br />
cell that is able to represent the microstructure <strong>of</strong> a closed-cell foam. For the investigation, a<br />
finite element model consisting <strong>of</strong> a repeating unit cell with periodical boundary conditions is<br />
implemented. As simplified cell geometry a tetrakaidecahedral foam microstructure is considered<br />
and a strain-energy based homogenisation concept is utilized. On the basis <strong>of</strong> image analysis<br />
imperfections are applied to the cell. These imperfections can be curved cell walls and edges,<br />
geometric irregularities <strong>of</strong> corner nodes and material concentrations at the cell edges. Some input<br />
data, for example Young’s modulus <strong>of</strong> the matrix material, are difficult to test experimentally.<br />
Consequently, these parameters are identified by an optimization. The obtained model is used<br />
as representative volume element (RVE) for further investigations <strong>of</strong> the postbuckling behaviour<br />
<strong>of</strong> the foams. Different analyses are performed and the results are compared to literature and<br />
experimental data.<br />
Homogenization <strong>of</strong> thin structured sheet metals by using FEM<br />
T. de Silva, A. Kühhorn, M. Golze (TU Cottbus) Schedule<br />
Thin structured sheet metals promise high potential concerning lightweight design in industrial<br />
applications regarding the classical mechanical engineering and vehicle construction as well as the<br />
aeronautics.<br />
Compared to flat, unstructured sheet metals the component stiffness and buckling behavior can<br />
significantly be improved by structuring especially in out <strong>of</strong> plane direction.<br />
To be able to calculate the elastic behavior <strong>of</strong> large structures from structured sheet metals a<br />
mechanical surrogate model is developed which describes effectively average material parameters<br />
based on processes <strong>of</strong> homogenization.
Section 4: Structural mechanics 99<br />
For the surrogate properties symmetry and antisymmetry boundaries and periodic boundaries respectively<br />
are contemplated on elementary cells whose structural mechanical behavior is decisive.<br />
By using an energetic approach the stiffness’s <strong>of</strong> large plate and shell structures can be determined<br />
by a cooperatively small amount <strong>of</strong> finite elements. By means <strong>of</strong> these material properties elastic<br />
behavior can easily be calculated. With it an efficient numerical design is guaranteed.<br />
This explained analysis can be applied to other periodically built up plate structures.<br />
[1] J. Hohe. Elastizitätsverhalten von Sandwich-Zellkernen und zweidimensionalen Modellschäumen.<br />
Shaker Verlag, Aachen, 2003.<br />
Material libraries for texturized thin metal sheets in elastic range<br />
Jonathan Montalvo-Urquizo (<strong>Universität</strong> Bremen) Schedule<br />
Thin metal sheets are highly determined by the rolling process during production, causing the<br />
material grains to have preferred orientations. The existence <strong>of</strong> such preferences is known as<br />
texture and cannot be modeled as a deterministic process.<br />
We present a simulation approach for the simulation <strong>of</strong> the elastic material responses based<br />
in stochastic generation <strong>of</strong> material samples and a subdomain-based FEM simulation. Both the<br />
single grain geometries and the lattice orientations are stochastically simulated.<br />
Combining a series <strong>of</strong> material samples with FEM simulations it is possible to generate a<br />
Material Library (ML) <strong>of</strong> responses. Being constructed only once for a given material, the ML<br />
can be used in a fast two-scale simulation avoiding any detailed computation in the microscale.<br />
Using Steel DC01 we show the simulated texture and its comparison with experimental data<br />
and present some results in the microscale and main ideas towards the two-scale method.<br />
S4.5: Material behavior I Thu, 13:30–15:30<br />
Chair: Christian Hellmich S2|02–C120<br />
Plastic deformation <strong>of</strong> rough surfaces<br />
Kai Willner, Franz Hauer (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
We present a fully elasto-plastic halfspace contact formulation based on the work <strong>of</strong> Jacq et al.<br />
[1]. Linear elastic-plastic material behavior is modeled based on v.Mises plasticity with isotropic<br />
hardening. The algorithm gives the residual stress as well as the full plastic deformation field due<br />
to a frictionless normal contact.<br />
The general algorithm is outlined and demonstrated using Hertzian type contact problems,<br />
showing for example the influence <strong>of</strong> the discretization and hardening effects. The results are<br />
compared to finite element solutions and a simplified elasto-plastic halfspace contact algorithm<br />
[2], showing the limits <strong>of</strong> the simplified algorithm.<br />
Use <strong>of</strong> FFT based convolutions <strong>of</strong> the influence functions allows the introduction <strong>of</strong> periodic<br />
boundary conditions suitable for the simulation <strong>of</strong> representative surface elements <strong>of</strong> rough surfaces.<br />
As an example, a typical contact pairing <strong>of</strong> a rough workpiece and a smooth die in a metal<br />
forming situation is simulated, allowing the identification <strong>of</strong> a constitutive contact law which can<br />
be used in a finite element simulation <strong>of</strong> the forming process.<br />
[1] C. Jacq, D. Nelias, G. Lormand, and D. Girodin. Development <strong>of</strong> a Three-Dimensional Semi-<br />
Analytical Elastic-Plastic Contact Code. Journal <strong>of</strong> Tribology (124) pp. 653–667, 2002.<br />
[2] K. Willner. Elasto-Plastic Normal Contact <strong>of</strong> Three-Dimensional Fractal Surfaces Using<br />
Halfspace Theory. Journal <strong>of</strong> Tribology (126) pp. 28–33, 2004.
100 Section 4: Structural mechanics<br />
Sensitivity analysis <strong>of</strong> elastic beams on Winkler foundation with stiffness weakening<br />
by Greens functions<br />
Kai Schwartpaul, Chuanzeng Zhang (<strong>Universität</strong> Siegen), Oliver Carl (C + P Engineering) Schedule<br />
This paper presents a sensitivity analysis <strong>of</strong> elastic beams on Winkler foundation with stiffness<br />
weakening. A local method is developed that enables us to predict the changes in the solution <strong>of</strong><br />
the structure resulting from the stiffness weakening by considering only the weakened or damaged<br />
parts. The advantage <strong>of</strong> this method is that it results in a local analysis instead <strong>of</strong> recalculating<br />
the whole structure. Consequently, it is computationally less time-consuming than the commonly<br />
used conventional method. The key idea <strong>of</strong> this method is based on the comparison between the<br />
elastic strain energies <strong>of</strong> the original and the weakened structures.<br />
As a suitable tool for the sensitivity analysis, the Green’s functions are applied [2]. If the<br />
different elastic strain energies <strong>of</strong> the original and the weakened systems are considered, then the<br />
solution for the changes <strong>of</strong> the internal forces, displacements or reaction forces can be obtained<br />
by substituting the virtual displacements by the corresponding Green’s functions.<br />
Furthermore, an approximate approach for the sensitivity analysis is presented which is described<br />
in detail in [1,3]. This approach enables us to predict the changes in the results due to the<br />
stiffness weakening within the beam or the elastic Winkler foundation by considering only the<br />
internal forces or the deflections <strong>of</strong> the initial system.<br />
In addition, an iterative method is developed to enhance the accuracy <strong>of</strong> the present approach.<br />
Numerical examples will be presented and discussed to show the accuracy and efficiency <strong>of</strong> the<br />
proposed method.<br />
[1] O. Carl: Static and dynamic sensitivity analysis <strong>of</strong> damaged structures by Green’s functions<br />
(in German). Dissertation, University <strong>of</strong> Siegen, 2011.<br />
[2] F. Hartmann; C. Katz: Structural Analysis with Finite Elements. Springer-Verlag, 2nd Edition,<br />
Berlin, 2007.<br />
[3] K. Schwartpaul: Sensitivity analysis with Green’s functions <strong>of</strong> weakened beams on elastic<br />
foundation (in German). Master Thesis, University <strong>of</strong> Siegen, 2011.<br />
Elastic-plastic States <strong>of</strong> Two-layer Curved Bar Under Pure Bending<br />
İsmail Y. Sülü, Eray Arslan (Inonu University, Turkey) Schedule<br />
An elastic-partially plastic two-layer curved bar with a narrow rectangular cross section subjected<br />
to couples at both ends is considered. In state <strong>of</strong> plane stress, small deformations and cylindrical<br />
symmetry are assumed. Trescas yield criterion and its associated flow rule initiate an analytical<br />
solution <strong>of</strong> the problem. A governing differential equation describing elastic and plastic behaviors<br />
<strong>of</strong> the two layers is derived. Field equations for elastic regions in two layers are obtained by<br />
integration <strong>of</strong> the governing equation and the solutions onset <strong>of</strong> yielding are investigated. The<br />
results show that yielding may emerge at the inner surface, at the outer surface <strong>of</strong> the whole<br />
bar or at the interface between two layers depending on selected materials and the geometry <strong>of</strong><br />
the layers. It is noted that in case <strong>of</strong> a homogeneous bar, however, plastic deformation always<br />
commences on the inner surface at the elastic limit. Furthermore, a critical case, in which yielding<br />
commences at the outer and the interface surfaces <strong>of</strong> the two-layer bar simultaneously, is observed.<br />
In the critical case, solutions <strong>of</strong> the governing equation for plastic regions enclose different Trescas
Section 4: Structural mechanics 101<br />
yield condition are obtained. Numerical results for real engineering materials in partially plastic<br />
state, which consists <strong>of</strong> elastic and plastic regions, are presented in graphical form.<br />
Analysis <strong>of</strong> the coupling effects <strong>of</strong> the longitudinal and transversal displacements on<br />
the deformation and internal forces <strong>of</strong> functionally graded beams<br />
Pedro D. Villamil, Chuanzeng Zhang (<strong>Universität</strong> Siegen) Schedule<br />
In this contribution, functionally graded beams (FGBs) with an arbitrary gradation <strong>of</strong> the material<br />
properties along the thickness <strong>of</strong> the beams are analyzed. Such FGBs are <strong>of</strong> special interest in<br />
civil and mechanical engineering to improve both the thermal and the mechanical behaviour <strong>of</strong><br />
the beams.<br />
In [1] free vibrations <strong>of</strong> functionally graded Timoshenko and Euler-Bernoulli beams have been<br />
considered. The described analytical solutions are based on the work <strong>of</strong> Li [2], where closed-form<br />
solutions <strong>of</strong> stress distributions, eigenfrequencies and eigenfunctions have been derived by means<br />
<strong>of</strong> a single differential equation <strong>of</strong> motion for the deflection.<br />
However, these previous considerations did not take into account the coupling between the<br />
longitudinal and the transversal displacements and its effect on the deformation and internal<br />
forces <strong>of</strong> the FGBs. This approximation is exact only for a symmetrical material gradation but it<br />
may not be valid for general cases with an arbitrary material gradation.<br />
In this contribution, the coupling effects <strong>of</strong> the longitudinal and transverse displacements on<br />
the deformation and internal forces <strong>of</strong> FGBs are investigated for different boundary conditions.<br />
An analytical solution <strong>of</strong> the corresponding boundary problem is derived. A comparison is also<br />
made with the numerical results obtained by the Finite Element Method. The obtained solution<br />
and its applications to FGBs with or without an elastic foundation are discussed.<br />
[1] P. D. Villamil, Vibrations <strong>of</strong> Functionally Graded Bars and Beams (in German), Diploma<br />
Thesis, Chair <strong>of</strong> Structural Mechanics, University <strong>of</strong> Siegen (2010).<br />
[2] X.-F. Li, A unified approach for analyzing static and dynamic behaviors <strong>of</strong> functionally graded<br />
Timoshenko and Euler-Bernoulli beams, Journal <strong>of</strong> Sound and Vibration 318 (2008), 1210<br />
– 1229.<br />
Asymptotic formulae for the flexibility <strong>of</strong> an infinite row <strong>of</strong> pin-loaded holes<br />
Jan Kratochvil, Wilfried Becker (TU <strong>Darmstadt</strong>) Schedule<br />
The problem <strong>of</strong> the flexibility <strong>of</strong> an infinite row <strong>of</strong> pin-loaded holes in an elastic plane or halfplane<br />
is considered within the framework <strong>of</strong> the complex potential method [1] and the theory <strong>of</strong><br />
compound asymptotic expansions [2]. First, the relative radius <strong>of</strong> the holes is introduced as a small<br />
parameter. The holes are loaded by an arbitrary distribution <strong>of</strong> radial and tangential stresses with<br />
a resultant equal to the overall transmitted force. Then, an asymptotic expansion <strong>of</strong> the complex<br />
potentials in terms <strong>of</strong> this small parameter is constructed. This expansion is uniformly valid in the<br />
whole domain, i.e. in the vicinity <strong>of</strong> the holes as well as in the far-field. Finally, the flexibility <strong>of</strong><br />
the row <strong>of</strong> pin-loaded holes is evaluated using this solution. In this manner, closed-form analytical<br />
approximations <strong>of</strong> the flexibility <strong>of</strong> several configurations <strong>of</strong> rows <strong>of</strong> pin-loaded holes are obtained.<br />
It appears that the results to a sufficient order <strong>of</strong> approximation do not depend on the complete<br />
information about the distribution <strong>of</strong> the contact pressure but only on several so called load<br />
coefficients that can be easily fitted from the experiment. The presented results are compared<br />
to the semi-empirical Huth’s formula [3] for the fastener flexibility which is widely used in the<br />
engineering practice.
102 Section 4: Structural mechanics<br />
[1] Muskhelishvili, N.I., Some Basic Problems <strong>of</strong> the Mathematical Theory <strong>of</strong> Elasticity, P.<br />
Nordho<strong>of</strong> Ltd, 1963<br />
[2] Maz’ya, V.; Nazarov, S.; Plamenevskij, B., Asymptotic Theory <strong>of</strong> Elliptic Boundary Value<br />
Problems in Singularly Perturbed Domains, Birkhäuser, 2000<br />
[3] Huth, H., Zum Einfluss der Nietnachgiebigkeit mehrreihiger Nietverbindungen auf die Lastübertragungs-<br />
und Lebensdauervorhersage, Frauenh<strong>of</strong>er-Institut für Betriebsfestigkeit <strong>Darmstadt</strong>,<br />
1984<br />
S4.6: Dynamics <strong>of</strong> Structures Thu, 13:30–15:30<br />
Chair: Jonathan Montalvo-Urquizo S2|02–C205<br />
Analysis <strong>of</strong> the lamition stack influence on the stiffness <strong>of</strong> stator active component<br />
Vera Luchscheider, Kai Willner (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
For electric motors light weight construction becomes increasingly important. This is why the<br />
nearly unknown stiffness and dynamical characteristic <strong>of</strong> the lamination stack has a bigger influence<br />
on the strength and oscillation calculation. For this reason in a first step the stiffness<br />
behavior is identified with quasi-static tests. Subsequently dynamical tests are to carry out.<br />
In the quasi-static tests the electric sheets are just stacked and an axial load is applied. At first a<br />
pressure <strong>of</strong> 1.5 or 3 N/mm 2 is exerted, representing the packaging process. Then a cyclic loading<br />
is superposed to simulate the forces acting during the motors life. The analysis <strong>of</strong> the lamination<br />
stack behavior at uniform loading has a progressive characteristic and a settling. The behavior at<br />
cyclic loading is hysteretic. The settling and some <strong>of</strong> the progression can be explained with the<br />
sheets waviness. Reason for this are the internal stresses, which are an effect <strong>of</strong> the sheets rolling<br />
and which release at the blanking process. The lamination stack behavior is also influenced by the<br />
coreplate varnish and the contacts <strong>of</strong> the sheets. Their mechanical characteristics are unknown<br />
and have to be modeled in this project. It is done with springs, dampers and frictional elements,<br />
which are coupeled parallel and in series. For this the models <strong>of</strong> Maxwell, Biot or Zener are<br />
<strong>of</strong>ten used [1]. Usually the frictional elements are Coulomb elements. The influence <strong>of</strong> the dampers<br />
is identified in dynamical tests, because they are dependent on the velocity. The stiffness <strong>of</strong><br />
the springs is mostly nonlinear and <strong>of</strong>ten exponetial dependent on the surfaces intersection. This<br />
aspect is motivated by the increasing contact <strong>of</strong> the surfaces by loading and the roughness heights,<br />
which are normally distributed and therefore follow an exponential function [2]. The hysteresis<br />
area is direct proportional to the dissipated work. With the dissipated work the sort <strong>of</strong> damping<br />
can be determined [1].<br />
After characterizing the lamination stack behavior in axial direction, there will be a tangential loading<br />
superposed and a model for the tangential direction developed. Therefor the just mentioned<br />
elements and procedure are used too.<br />
[1] G. Siegl, Das Biegeschwingungsverhalten von Rotoren, die mit Blechpaketen besetzt sind,<br />
Dissertation, <strong>Technische</strong> <strong>Universität</strong> Berlin (1981)<br />
[2] D. Görke, Experimentelle und numerische Untersuchung der Normal- und Tangenialkontaktverhaltens<br />
rauer metallischer Oberflächen, Dissertation, Friedrich-Alexander-<strong>Universität</strong> Erlangen-Nürnberg<br />
(2010)
Section 4: Structural mechanics 103<br />
Shaking table tests <strong>of</strong> a model-scale building with 2DOF pendulum mass damper<br />
Krzyszt<strong>of</strong> Majcher (Wroclaw University <strong>of</strong> Technology) Schedule<br />
In this paper, the numerical and experimental studies <strong>of</strong> a tall buildings model with 2DOF pendulum<br />
mass damper (PMD) are considered. It is assumed that the model excitation is in the<br />
form <strong>of</strong> horizontal and/or torsional motion <strong>of</strong> the ground caused by earthquake. The construction<br />
consists <strong>of</strong> the main system (tall buildings model) and a double pendulum mass damper,<br />
which is attuned to the first (bending) and the second (torsional) eigenfrequencies <strong>of</strong> the main<br />
structure. The analysis focuses on reduction <strong>of</strong> structure vibration caused by horizontal or torsional<br />
component <strong>of</strong> ground motions. Therefore, results presented in this work show efficiency <strong>of</strong><br />
2DOF PMD for vibration reduction. The numerical analysis <strong>of</strong> the problem is performed with<br />
using COSMOS/M system (a FEM numerical model is defined), while experimental analysis is<br />
carried out on a physical model-scale building with 2DOF PMD. Model consists <strong>of</strong> twenty five<br />
recurrent storeys (total height 2,5m) and on the highest storey there is a PMD located. Shaking<br />
table device is used to simulate an earthquake excitation in horizontal and torsional component<br />
independently.<br />
Application <strong>of</strong> the Proper Orthogonal Decomposition for structures under earthquake<br />
excitations<br />
Franz Bamer (TU Wien), Christian Bucher Schedule<br />
Model reduction has become very important in order to save calculation time. Especially in Structural<br />
Mechanics computations become very time consuming when the critical timestep <strong>of</strong> explicit<br />
integrators gets very small. The main focus <strong>of</strong> this work is to use the Proper Orthogonal Decomposition<br />
(POD) method for an earthquake loaded structure and to compare its results to<br />
those according to the classical method <strong>of</strong> modal truncation. After testing the applicability <strong>of</strong> the<br />
Proper Orthogonal Decomposition on linear systems, nonlinear friction base isolation systems are<br />
integrated. The POD is a very powerful and elegant method if the snapshots within a certain<br />
chosen time interval describe the main behavior <strong>of</strong> the system. Both in the linear and in the<br />
nonlinear case the approximation <strong>of</strong> the POD reduced system is very accurate by using only a<br />
few POD modes. The advantage over the method <strong>of</strong> Modal Truncation is the optimality <strong>of</strong> the<br />
POD modes, which are not only dependent on the system but also on the excitation.<br />
Analysis <strong>of</strong> macro- and micro-vibrations <strong>of</strong> transversally graded thin plates<br />
Magda Kaźmierczak, Jarosław Jędrysiak (Technical University <strong>of</strong> Łódź) Schedule<br />
Thin plates having tolerance-periodic microstructure in planes parallel to the plate midplane are<br />
considered in this note. But their macrostructure is functionally graded. These plates consist <strong>of</strong><br />
many small elements. Distant elements can be very different, but adjacent elements can be nearly<br />
identical. All elements are treated as thin plates and called cells. The size <strong>of</strong> the microstructure<br />
is described by a diameter <strong>of</strong> the cell l, called microstructure parameter. Plates <strong>of</strong> this kind will<br />
be treated as made <strong>of</strong> functionally graded materials, cf. [7], and called transversally graded thin<br />
plates.<br />
Vibrations <strong>of</strong> these functionally graded plates are described by differential equations which<br />
coefficients are highly oscillating, tolerance-periodic and non-continuous functions. Thus, these<br />
governing equations are not a proper tool to analyse specials engineering problems.<br />
In order to obtain equations with continuous, slowly-varying coefficients there are proposed<br />
various averaging techniques. Functionally graded structures are <strong>of</strong>ten described by averaging<br />
approaches, which are applied for macroscopically homogeneous structures, e.g. periodic, cf. [7].
104 Section 4: Structural mechanics<br />
Unfortunately, governing equations <strong>of</strong> these models neglect usually the effect <strong>of</strong> the microstructure.<br />
However, to avoid this drawback and to describe the effect <strong>of</strong> the microstructure the tolerance<br />
averaging technique can be applied. This modelling method was proposed and developed for<br />
various periodic structures, cf. [9], [8]. Then it has been also adopted to analyse various thermomechanical<br />
problems <strong>of</strong> functionally graded media with a microstructure, e.g. for heat conduction<br />
in composites, cf. [2, 6], for thermoelasticity problems in laminates, cf. [1], for functionally graded<br />
plates, cf. [3, 4, 5]. These different problems are shown in a series <strong>of</strong> papers. Extended lists <strong>of</strong><br />
publications can be found in monographs [9, 8].<br />
The main aim <strong>of</strong> this paper is to show and apply an asymptotic-tolerance model <strong>of</strong> the plates<br />
under consideration. The model equations are obtained using both the asymptotic and the<br />
tolerance modelling procedures, cf. [8]. In the framework <strong>of</strong> this model macro- and micro-vibrations<br />
<strong>of</strong> transversally graded plates can be analysed.<br />
[1] JĘDRYSIAK J.: On the tolerance modelling <strong>of</strong> thermoelasticity problems for transversally<br />
graded laminates, Arch. Civ. Mech. Engn., 11, 2011, 61-74.<br />
[2] JĘDRYSIAK J., RADZIKOWSKA A.: Tolerance averaging <strong>of</strong> heat conduction in transversally<br />
graded laminates, Meccanica, 2011, Doi:10.1007/s11012-010-9420-y.<br />
[3] KAŹMIERCZAK M., JĘDRYSIAK J.: Free vibrations <strong>of</strong> transversally graded plate band,<br />
Electr. J. Polish Agric. Univ., 13, 4, 2010.<br />
[4] KAŹMIERCZAK M., JĘDRYSIAK J.: Tolerance modelling <strong>of</strong> vibrations <strong>of</strong> thin functionally<br />
graded plates, Thin Walled Struct., 49, 2011, 1295-1303.<br />
[5] KAŹMIERCZAK M., JĘDRYSIAK J., WIROWSKI A.: Free vibrations <strong>of</strong> thin plates with<br />
transversally graded structure, Civ. Env. Eng. Rep., 5, 2010, 137-152.<br />
[6] OSTROWSKI P., MICHALAK B.: Non-stationary heat transfer in a hollow cylinder with<br />
functionally graded material properties, J. Theor. Appl. Mech., 49, 2011, 385-397.<br />
[7] SURESH S., MORTENSEN A.: Fundamentals <strong>of</strong> functionally graded materials, Cambridge,<br />
The University Press 1998.<br />
[8] WOŹNIAK CZ., ET AL. [eds]: Mathematical modelling and analysis in continuum mechanics<br />
<strong>of</strong> microstructured media, Gliwice, Wyd. Politechniki Śląskiej 2010.<br />
[9] WOŹNIAK CZ., MICHALAK B., JĘDRYSIAK J. [eds]: Thermomechnics <strong>of</strong> microheterogeneous<br />
solids and structures, Łódź, Wyd. Politechniki Łódzkiej 2008.<br />
Effects <strong>of</strong> Damping Mechanisms in Forced Longitudinal Vibration <strong>of</strong> a Bar Connected<br />
to a Viscoelastic Halfspace<br />
Thanh Chung Pham, Jörg Wauer, Wolfgang Seemann (KIT) Schedule<br />
This is one <strong>of</strong> our continuous researches about effects <strong>of</strong> damping mechanisms in free and forced<br />
vibrations <strong>of</strong> some structural members, such as bars and beams [1]. The interactive transmission<br />
<strong>of</strong> a signal from a cylindrical bar to an attached halfspace is presented in this study. The damping<br />
and stiffness properties <strong>of</strong> the resonating environment are simultaneously taken into account. Finally,<br />
it brings forward the substitution <strong>of</strong> an equivalent viscoelastic spring or impedance for the<br />
foundation, as well as the identification <strong>of</strong> the clamping parameters. It is required to consider
Section 4: Structural mechanics 105<br />
wave propagation effects by applying the theory <strong>of</strong> continuum mechanics, and numerical method<br />
with integral transforms and approximation. The results <strong>of</strong> our previous study <strong>of</strong> the vibration <strong>of</strong><br />
a substitution system [1] as well some related studies, such as Saito and coworkers’ researches [2,<br />
3], are utilized and related to ones in this paper.<br />
Keywords: structural member, bar, beam, damping, stiffness, mechanisms, boundary condition,<br />
identification, clamping parameter, halfspace, dynamic interaction, interactive transmission,<br />
viscoelastic, longitudinal, axial, vibration, oscillation, substitution system, foundation, wave propagation,<br />
integral transform.<br />
[1] T. C. Pham, J. Wauer, W. Seemann, Effects <strong>of</strong> Damping Mechanisms in Free and Forced<br />
Vibrations <strong>of</strong> Some Structural Members, Proc. Appl. Math. Mech., WILEY-VCH Verlag,<br />
2011, 11, 259-260.<br />
[2] H. Saito and S. Chonan, Forced longitudinal vibration <strong>of</strong> an elastic circular rod on an elastic<br />
half-space, The Journal <strong>of</strong> the Acoustical Society <strong>of</strong> America 59(4), 861-865 (1976).<br />
[3] H. Saito and H. Wada, Forced vibrations <strong>of</strong> a mass connected to an elastic half-space by an<br />
elastic rod or a spring, Journal <strong>of</strong> Sound and Vibration 50(4), 519-532 (1977).<br />
Simplified assessment <strong>of</strong> high-speed train induced bridge vibrations considering shear<br />
effects<br />
Patrick Salcher, Christoph Adam (<strong>Universität</strong> Innsbruck) Schedule<br />
An improved response spectrum methodology for fast and yet accurate assessment <strong>of</strong> the dynamic<br />
peak response <strong>of</strong> simple railway bridges is presented. The derived response spectra are based on<br />
the Timoshenko beam theory in an effort to include the effect <strong>of</strong> shear deformation, which is <strong>of</strong><br />
importance, if the considered bridge is a truss structure. In contrast to the Bernoulli-Euler theory,<br />
the ratio <strong>of</strong> two sequent natural frequencies depends on the bridge parameters when Timoshenko<br />
theory is used. Thus, for the considered study the modal peak responses <strong>of</strong> the bridge such as<br />
acceleration, displacement, and bending moment are derived separately. Then, the peak response<br />
is found by statistical combination <strong>of</strong> the individual modal responses applying different rules. In<br />
the underlying numerical analyses a sequence <strong>of</strong> moving single forces <strong>of</strong> constant speed simulate<br />
the effect <strong>of</strong> passing trains. These loads are adjusted to real European high-speed trains and to the<br />
train load models <strong>of</strong> Eurocode I. The presented response spectra are based on non-dimensional<br />
characteristic bridge and train parameters. The proposed methodology is assessed and meaningful<br />
examples are discussed.<br />
S4.7: Material behavior II Thu, 16:00–18:00<br />
Chair: Kai Willner S2|02–C120<br />
Elastic limit analysis <strong>of</strong> a thick-walled cylindrical panel subject to radial heating<br />
Eray Arslan (Inonu University, Turkey), Werner Mack (TU Wien) Schedule<br />
In analogy to the theory <strong>of</strong> wide curved beams, first the basic equations for a thick-walled cylindrical<br />
panel with rectangular cross-section under plane strain condition are given. The sides <strong>of</strong><br />
the panel parallel to the cylinder axis are presupposed to be guided in such a way that a displacement<br />
in circumferential direction may occur and the curvature <strong>of</strong> the middle surface remains<br />
constant. Then, both for homogeneous heating and for the occurrence <strong>of</strong> a temperature gradient
106 Section 4: Structural mechanics<br />
independent <strong>of</strong> the circumferential coordinate, as it will occur e.g. by heating <strong>of</strong> the outer surface,<br />
couples act on those sides. These couples give rise to a stress state corresponding to pure bending<br />
conditions, and yielding may occur. Hence, in the present contribution, the limits for elastic behavior<br />
in dependence on the heating conditions and on the thickness <strong>of</strong> the panel are investigated.<br />
Moreover, thermal s<strong>of</strong>tening and therefore a reduced yield stress are taken into account, and both<br />
von Mises and Trescas yield criterion are considered. For the latter, an example for the partially<br />
plastic state after the onset <strong>of</strong> plastic flow is given, too.<br />
A Finite Element formulation for static droplets in contact with rough surfaces<br />
Muhammad Osman, Roger A. Sauer (RWTH Aachen) Schedule<br />
The shapes <strong>of</strong> two dimentional static droplets in contact with rough surfaces are computed using<br />
the Young-Laplace equation. The problem is modeled within a continuum mechanical framework,<br />
and solved using the Finite Element method. Three constraints are introduced in a polar coordinates<br />
based model. A constraint for the droplet volume is enforced using the Lagrange multiplier<br />
method. Surface contact constraint is enforced by the penalty and the Augumented Lagrange<br />
multiplier method. At the three phase contact line, the contact angle is prescribed as a penalty<br />
constraint, allowing for capturing local contact at the individual asperities <strong>of</strong> the rough surface.<br />
A two level structured rough surface is constructed by superposition <strong>of</strong> exponential functions.<br />
The entire formulation is also expressed in cartesian basis for consistency and robustness. The<br />
numerical model is verified against analytical solutions <strong>of</strong> special cases, and convergence has been<br />
studied.<br />
Micro - mechanical analysis <strong>of</strong> creep behavior in a multipass weld<br />
Ivan Lvov (<strong>Universität</strong> Magdeburg) Schedule<br />
A method <strong>of</strong> evaluating creep response <strong>of</strong> the multipass weld based on the micro-macro mechanics<br />
approach is introduced. Multipass weld microstructure that consists from columnar, coarse and<br />
fine grained zones is considered. Materials <strong>of</strong> these constituents assumed to be isotropic. Weld<br />
metal properties <strong>of</strong> inelastic behavior have unknown type <strong>of</strong> symmetry and are described by the<br />
following anisotropic creep constitutive model [1]:<br />
〈 ˙ε〉 = 〈σ n 2〉[B]〈σ〉<br />
To model the microstructure <strong>of</strong> the multipass weld metal the representative volume element<br />
(RVE) is created for CAE Abaqus. Material properties <strong>of</strong> weld metal grain type zones are taken<br />
from [2]. Numerical tests on uniform loading <strong>of</strong> the RVE are performed. Creep material properties<br />
for equivalent weld material are found for welds with different number <strong>of</strong> passes. The symmetry<br />
type <strong>of</strong> the creep material properties <strong>of</strong> multi-pass weld are evaluated for the equivalent weld<br />
material. As an example <strong>of</strong> macro model analysis <strong>of</strong> the welding, the creep calculation <strong>of</strong> the<br />
cylindrical shell with the welding under the uniform inner pressure is performed.<br />
[1] Zolochevsky AA. About the influence <strong>of</strong> loading on the theory <strong>of</strong> creep in isotropic and anisotropic<br />
materials / / J. Appl. mechanics and technical physics. - 1982, 4. - S. 140-144.<br />
[2] Hyde T.H., Sun W. Creep failure behavior <strong>of</strong> a 9CrMoNbV weld metal with anisotropy under<br />
a biaxial loading state“J. Strain Analysis Vol. 41 No. 5, 2006
Section 4: Structural mechanics 107<br />
Influence <strong>of</strong> shotcrete composition on load-level estimation in NATM-tunnel shells:<br />
Micromechanics-based sensitivity analyses<br />
Christian Hellmich, Shafi Ullah, Bernhard Pichler, Stefan Scheiner (TU Wien) Schedule<br />
Displacement measurement-based estimations <strong>of</strong> loads and utilization degrees in shotcrete tunnel<br />
shells as part <strong>of</strong> the New Austrian Tunneling Method (NATM), have become standard tools<br />
in tunnel practice; their quality, however, may crucially depend on the knowledge <strong>of</strong> the actual<br />
shotcrete composition after spraying. To shed light on this issue, we here determine, based<br />
on experimentally validated micromechanical representations <strong>of</strong> shotcrete, the hydration degreedependent<br />
elastic, creep, and strength properties <strong>of</strong> different shotcretes, characterized by water<br />
cement ratios (w/c) between 0.4 and 0.6, aggregate cement ratios (a/c) between 3.5 and 5, and<br />
Youngs modulus <strong>of</strong> aggregates (Eagg) between 40 and 80 GPa. These properties are fed into a<br />
structural shell model <strong>of</strong> the Sieberg tunnel, and this model is subjected to displacement fields<br />
approximated from daily displacement measurements at five selected points along the shells inner<br />
surface. Resulting stresses and forces in the tunnel shell allow for analyzing the influence <strong>of</strong><br />
shotcrete composition on load-level estimation in NATM tunnel shells: The magnitudes <strong>of</strong> circumferential<br />
and longitudinal normal forces increase significantly with decreasing w/c, while a/c and<br />
Eagg have the inverse and relatively minor effect. The utilization degree is virtually insensitive<br />
to changes in w/c (especially at early ages), and only slightly decreases with decreasing a/c and<br />
Eagg. The location <strong>of</strong> maximum loading is unaffected by the shotcrete composition underlying the<br />
analysis. Conclusively, location and magnitude <strong>of</strong> maximum utilization degrees are very robust<br />
estimates (not affected by limited knowledge on the shotcrete composition), whereas realistic estimation<br />
<strong>of</strong> stresses and forces does require more accurate consideration <strong>of</strong> shotcrete composition.<br />
S4.8: Stability and Eigenvalue Problems Thu, 16:00–18:00<br />
Chair: Martin Schagerl S2|02–C205<br />
Elastic stability <strong>of</strong> predeformed beams<br />
Dominik Kern, Wolfgang Seemann (KIT) Schedule<br />
As is well known, the load capacity <strong>of</strong> mechanical components is not only limited by the maximum<br />
stresses but also by buckling failures. Beside the Euler cases, the lateral-torsional buckling is a<br />
common failure mode, particularly for beams with a high ratio <strong>of</strong> the area moments <strong>of</strong> inertia. In<br />
many applications, such as trusses, the predeformation may be neglected for the buckling analysis.<br />
However, flexure hinges characteristically undergo large deformations in operation, thus the<br />
predeformations must be taken into account. Mathematically, the predeformations are imperfections<br />
changing the bifurcation paths. As consequence, the bifurcation point itself may not be a<br />
precise indicator for the failure, since large failure displacements may occur at lower loads. Thus<br />
alternative failure criteria are needed. As example the lateral-torsional buckling <strong>of</strong> a flexure hinge<br />
(leaf spring type) is examined by energy methods. The crucial point is that the elastic energy<br />
stored in the beam is formulated intrinsically, while the potential <strong>of</strong> external conservative loads<br />
is formulated in a space-fixed coordinate system. Expressions derived from differential geometry<br />
are compared with well-established approximations.<br />
About the effect <strong>of</strong> elastic-plastic properties <strong>of</strong> the material on the stability <strong>of</strong> columns<br />
under deterministic and stochastic parametric excitations<br />
Vadim D. Potapov (Moscow State University <strong>of</strong> Means Communication) Schedule<br />
In the message it is shown that at defined combinations <strong>of</strong> input data a linear elastic column<br />
laying on a nonlinear elastic foundation under the action <strong>of</strong> the periodic deterministic parametric
force can perform a chaotic motion. If the material <strong>of</strong> the column is nonlinear, then the character<br />
<strong>of</strong> its motion at the same input data is not changed principally. And if the material is elasticplastic<br />
then the motion <strong>of</strong> the column remains unstable, but it strives to stationary process. It<br />
is shown that an unstable motion <strong>of</strong> the elastic column at the deterministic treatment <strong>of</strong> the<br />
problem can be done stable by the addition <strong>of</strong> a force in the form <strong>of</strong> a random stationary process.<br />
(The stability for the deterministic problem is understood as the stability in Liapunov sense and<br />
in the stochastic case as the almost sure stability, stability in the mean and stability in the mean<br />
square.) In a case <strong>of</strong> a nonlinear elastic or elastic-plastic column at the same input data the similar<br />
effect is not observed. If the column made from a nonlinear or elastic-plastic material is unstable<br />
at deterministic treatment then it is unstable too at stochastic treatment <strong>of</strong> the problem.<br />
Geometrically exact solutions <strong>of</strong> buckling columns with asymmetric boundary conditions<br />
Gerhard Prechtl, Martin Schagerl, Kai-Uwe Schröder (<strong>Universität</strong> Linz) Schedule<br />
For the symmetrically supported Euler buckling column with both ends hinged the classical stability<br />
theory yields simple trigonometric functions as buckling modes, i.e. w(x) = A sin αx. The<br />
eigenvalues α are just multiples <strong>of</strong> π. In comparison, the analysis <strong>of</strong> the asymmetrically supported<br />
Euler buckling column with one end fixed and the other end hinged is more complicated: The buckling<br />
modes are a combination <strong>of</strong> trigonometric functions in form <strong>of</strong> w(x) = A (sin αx − αx cos α).<br />
The eigenvalues α follow from a transcendental equation.<br />
Applying a geometrically exact theory to the aforementioned Euler buckling problems, a similar<br />
relation in the complexity <strong>of</strong> the analyses will naturally arise. Using, e.g., the elastica model<br />
the buckling modes <strong>of</strong> the symmetrically supported column are represented by elliptic integrals.<br />
However, the determination <strong>of</strong> the buckling modes <strong>of</strong> the asymmetrically supported column turns<br />
out to be much more complex and elaborate. This short communication presents a thorough<br />
comparison <strong>of</strong> the symmetrically and asymmetrically supported buckling columns regarding their<br />
analyses by means <strong>of</strong> classical stability theory and by a geometrically exact theory.<br />
Comparative Study <strong>of</strong> Experimental and Simulated Buckled Shapes <strong>of</strong> Alternately<br />
Loaded Plates<br />
Russell Todres, Marcus St<strong>of</strong>fel, Dieter Weichert (RWTH Aachen) Schedule<br />
Experimental studies in a shock wave tube have shown that an initially plane, circular plate subjected<br />
to uniform pressure and then alternately loaded to the same peak level deforms inelastically<br />
and snaps-through at an ever increasing load until either a stable limit state is reached or the plate<br />
fails. For the limit state, the final deformed pr<strong>of</strong>ile is asymmetric. To determine whether such a<br />
shape is optimal in terms <strong>of</strong> its resistance to instability, a symmetric spherical cap with height<br />
corresponding to the limit state’s maximum out-<strong>of</strong>-plane displacement and base radius equal to<br />
the radius <strong>of</strong> the flat plate is loaded once with the same uniform pressure as before. Simulations<br />
and experiments are used to compare the snap-through pressure as well as the development <strong>of</strong><br />
plastic strains for this case with those for the limit state above.<br />
Temperature and displacement fields in brake and clutch systems with thermoelastic<br />
instabilities<br />
Matthias Graf, Georg-Peter Ostermeyer (TU Braunschweig) Schedule<br />
In brake and clutch systems kinetic energy is converted into thermal energy. Experiments show<br />
that the corresponding temperature field can develop unstable periodic structures, which can be<br />
parallel or normal to the sliding direction. The temperature field couples to the displacement
Section 4: Structural mechanics 109<br />
field by thermal expansion. Local pressure maxima in the frictional plane and the corresponding<br />
maxima in heat generated cause thermoelastic instabilities (TEI). They appear as so-called hot<br />
bands or hot spots on the sliding bodies.<br />
A model describing both effects covers layers <strong>of</strong> thermoelastic materials for all necessary<br />
mechanical components <strong>of</strong> the system. The set <strong>of</strong> field equations <strong>of</strong> each layer can analytically<br />
be solved by separation <strong>of</strong> constants. These solutions must fulfill the boundary conditions e.g. in<br />
the sliding plane or between different layers in a layered material. A stability discussion yields<br />
whether TEI appear or not.<br />
To cover different TEI phenomena, an angle parameter allows the rotation <strong>of</strong> the two-dimensional<br />
solution with respect to sliding plane. The observed temperature and displacement fields highly<br />
depend on the structure <strong>of</strong> the sliding system. For example, existing models typically find hot<br />
spots appearing in an antisymmetric pattern on both sliding faces on a brake disk. The model<br />
under discussion shows that a symmetric solution is possible as well, when cooling channels in<br />
the disk are taken into account.<br />
On eigenvalue sensitivities <strong>of</strong> restricted eigenvalue problems<br />
Nils Wagner (Intes GmbH) Schedule<br />
Nowadays large finite element models consist <strong>of</strong> incompatible meshes for different parts <strong>of</strong> the<br />
structure. Coupling is achieved by interpolation surfaces. The associated eigenvalue problem in<br />
structural dynamics is given by<br />
Kx = λMx, C T x = 0. (1)<br />
We are interested in eigenvalue sensitivities<br />
∂λ<br />
∂C<br />
with respect to these couplings. Some numerical examples are given.<br />
(2)
110 Section 5: Nonlinear oscillations<br />
Section 5: Nonlinear oscillations<br />
Organizers: Dietrich Flockerzi (MPI Magdeburg), Edwin Kreuzer (TU Hamburg-Harburg)<br />
S5.1: Nonlinear Oscillations I Tue, 13:30–15:30<br />
Chair: Edwin Kreuzer, Dietrich Flockerzi S1|02–344<br />
Self-excitation in decanter centrifuges - a simple mechanism<br />
Eberhard Brommundt (TU Braunschweig) Schedule<br />
Decanter centrifuges, used to separate liquid-solids slurry, can undergo self-excited rotational vibrations<br />
(called ’chatter’ when severe). A model is developed to explain the excitation as result <strong>of</strong><br />
the dynamic interactions between the rotating bowl, the sedimented solids cake sliding inside it,<br />
pushed by the slightly faster rotating conveyor screw. Including the drive, the multi-body system<br />
has six degrees <strong>of</strong> freedom; Coulomb friction forces act between cake/bowl and cake/screw. The<br />
effect <strong>of</strong> the turbulent slurry flow is accounted for by damping.<br />
The stability <strong>of</strong> the stationary operation is studied by numerical solution <strong>of</strong> the variational<br />
equation to the nonlinear equation <strong>of</strong> motion.<br />
Self-excited vibrations and quenching by periodic forcing <strong>of</strong> nonlinear systems<br />
Daniel Hochlenert, Utz von Wagner (TU Berlin) Schedule<br />
In the linear case, the stability <strong>of</strong> the trivial solution <strong>of</strong> a dynamical system is independent <strong>of</strong><br />
a possibly acting external forcing. Therefore, it is impossible to influence self-excited vibrations,<br />
indicated by an unstable trivial solution, by an appropriate forcing <strong>of</strong> the linear system. However,<br />
in the nonlinear case and in the neighbourhood <strong>of</strong> a bifurcation point it is very well possible to<br />
stabilize an unstable trivial solution by an external periodic forcing. This is <strong>of</strong>ten referred to as<br />
quenching <strong>of</strong> self-excited vibrations.<br />
The present talk deals with nonlinear self-excited systems under periodic forcing. Following<br />
the concepts <strong>of</strong> normal form theory, the feasibility <strong>of</strong> quenching the self-excitation is investigated<br />
with respect to the nonlinearities coupling the forcing with the states <strong>of</strong> system. It is analyzed<br />
which nonlinearities are essential to allow for quenching self-excitation. The results are compared<br />
with a direct numerical analysis <strong>of</strong> the nonlinear system.<br />
An experimental method for the phase controlled frequency response measurement<br />
<strong>of</strong> nonlinear vibration systems<br />
Jörg Wallaschek, Sebastian Mojrzisch, Jan Bremer (<strong>Universität</strong> Hannover) Schedule<br />
The experimental determination <strong>of</strong> the frequency response <strong>of</strong> nonlinear systems is difficult when<br />
there exists more than one solution branch. Depending on the system at hand, various types <strong>of</strong><br />
”jump phenomena” can be observed and in the example <strong>of</strong> the well-known Duffing system, it is<br />
not possible to experimentally determine the unstable solution branch if the system is excited by<br />
a harmonic force.<br />
In the present paper we investigate the Duffing system and we present a method which allows<br />
to re-formulate the equation <strong>of</strong> motion <strong>of</strong> the system with force excitation in the form <strong>of</strong> an<br />
equivalent self-excited system. Considering the phase between force and response as the input<br />
variable, it is then possible to calculate the frequency <strong>of</strong> the system vibration for any given phase<br />
shift. And in the same way the corresponding response amplitude can be determined.<br />
An experimental set-up has been designed and built which was used to test the performance<br />
<strong>of</strong> the method. Measurements <strong>of</strong> the backbone curve have been performed and will be discussed<br />
on the background <strong>of</strong> the theoretical predictions.
Section 5: Nonlinear oscillations 111<br />
Analysis <strong>of</strong> Chaotic Dynamics <strong>of</strong> Parametric Vibrations <strong>of</strong> Flexible Cylindrical Panels<br />
and Plates by Using the Wavelet - Analysis<br />
A.V. Krysko (Saratov State Technical University), U. Nackenhorst (<strong>Universität</strong> Hannover), I.V.<br />
Papkova, V.A. Krysko (Saratov State Technical University) Schedule<br />
In this contribution the mathematical model for the complex nonlinear vibrations <strong>of</strong> flexible cylindrical<br />
panels and plates will be presented. Such kind <strong>of</strong> flexible panels and plates are the elements<br />
<strong>of</strong> aircraft and ships constructions. The obtained strongly non-linear partial differential equations<br />
are discretized in space by finite difference methods <strong>of</strong> different order, i.e. O(h 2 ), O(h 4 ), O(h 6 ).<br />
The resulting system <strong>of</strong> ordinary differential equations in time is solved by a Runge-Kutta scheme<br />
<strong>of</strong> fourth order.<br />
The obtained solution is analyzed by methods <strong>of</strong> nonlinear dynamics. In order to study the<br />
parametric vibrations <strong>of</strong> cylindrical plates and panels wavelet analysis has been applied. For these<br />
studies on the chaotic dynamics <strong>of</strong> the parametric vibrations different types <strong>of</strong> wavelets have been<br />
investigated, i.e. different types <strong>of</strong> Gaussian, the MHat (’Mexican hat’) wavelet and the Morlet<br />
wavelet.<br />
These studies guided us to investigate the optimal wavelet formulation for this kind <strong>of</strong> chaotic<br />
parametric vibrations. In addition, with based on the wavelet analysis new phenomena <strong>of</strong> parametric<br />
random vibrations <strong>of</strong> flexible cylindrical panels and plates have been identified. In particular,<br />
a memory like phenomenon has been observed, when the system changes from one type vibrations<br />
to another.<br />
Determination <strong>of</strong> a stochastic friction coefficient depending on a randomly rough<br />
surface<br />
Nicole Gaus, Carsten Proppe (KIT) Schedule<br />
Friction induced vibrations are a widely studied field. In these investigations the friction coefficient<br />
is one <strong>of</strong> the most important parameters. Measurements show that the friction coefficient is<br />
velocity dependent and underlies stochastic fluctuations.<br />
The friction coefficient can be calculated using different analytical approaches which describe<br />
friction causes such as adhesion and elastic deformation. The stochastic fluctuations <strong>of</strong> a friction<br />
coefficient depend strongly on the roughness <strong>of</strong> the contacting surface. If the surface data is described<br />
as a random field, the real contact area and the contact normal force can be calculated with<br />
the Hertz contact formulation for contacting elastic bodies. The friction force can be calculated<br />
with the Bowden-Tabor approach which suggests that the friction force is the force to shear apart<br />
contacting asperities. The Bowden Tabor approach is a good model for adhesion which is <strong>of</strong>ten<br />
the dominant part <strong>of</strong> friction in dry contact.<br />
With these methods the stochastic properties <strong>of</strong> the friction coefficient can be calculated<br />
depending on the stochastic surface data.<br />
A Semi-Analytical Method <strong>of</strong> Solving the Fokker-Planck-Equation for High-Dimensional<br />
Nonlinear Mechanical Systems<br />
Wolfram Martens (TU Berlin) Schedule<br />
Stochastic processes are a common way <strong>of</strong> describing systems that are subjected to random<br />
influences. Technical systems may be excited by road roughness or wind gusts, for example,<br />
as well as fluctuating system parameters, which can all be described by stochastic differential<br />
equations.<br />
In previous works by the author and others (see [1], for example) it has been demonstrated<br />
how a Galerkin-method can be used to obtain global numerical solutions <strong>of</strong> the Fokker-Planck-<br />
Equation (FPE) for nonlinear random dynamical systems. Computational efforts are reduced by
112 Section 5: Nonlinear oscillations<br />
orthogonal polynomial expansion <strong>of</strong> approximate solutions so that probability density functions<br />
(pdfs) for comparably high-dimensional problems have been computed successfully. Stationary<br />
mechanical systems with dimensions up to d = 10 have been investigated, including polynomial<br />
as well as non-smooth nonlinearities.<br />
In general, increasing problem dimensions lead to immense numerical efforts in solving the<br />
FPE, an issue commonly referred to as the ’curse <strong>of</strong> dimensionality’. In order for the presented<br />
method to be feasible for general high-dimensional problems a covariance-based coordinate<br />
transformation is applied. Special focus has been put on Gaussian approximate solutions as they<br />
provide a number <strong>of</strong> analytical relations that can be exploited for efficient computation. However,<br />
in the case <strong>of</strong> pdfs that are far from Gaussian it is also appropriate to use more sophisticated<br />
approximate solutions.<br />
This talk presents results for different nonlinear problems with polynomial nonlinearities as<br />
well as a technical application with non-smooth damping elements. All results are compared with<br />
numerical solutions from Monte Carlo simulations.<br />
[1] W. Martens, U. von Wagner, V. Mehrmann, Calculation <strong>of</strong> high-dimensional probability density<br />
functions <strong>of</strong> stochastically excited nonlinear mechanical systems, Nonlinear Dynamics<br />
(13 July 2011), pp. 1-11. doi:10.1007/ s11071-011-0131-2<br />
S5.2: Nonlinear Oscillations II Wed, 13:30–15:30<br />
Chair: Dietrich Flockerzi, Edwin Kreuzer S1|03–104<br />
Optimizing force time history for interaction between athlete and sports surface<br />
Claudia Körner, Wolfgang Seemann (KIT) Schedule<br />
The aim in high-performance sports activities is reaching the optimum between high efficiency<br />
and low risk <strong>of</strong> injuries during workout. The goal <strong>of</strong> this contribution is to increase the understanding<br />
<strong>of</strong> these two facts for an interaction between athletes and sports surfaces.<br />
For several movements like landing, take-<strong>of</strong>f or running the typical vertical ground reaction force<br />
(VGRF) time history on a rigid ground is well known. In this paper, investigations for the<br />
interaction <strong>of</strong> an athlete with a compliant ground (elastic, linear/nonlinear viscous-elastic) are<br />
made. Therefore, the influence <strong>of</strong> the surface parameters on the force time history are analyzed<br />
and finally optimized for typical movements. The optimization algorithm uses a cost function<br />
which assumes that the work performed by a human body has to be minimal. In a second step,<br />
the optimization criterions are specific key characteristics <strong>of</strong> the force time history such as peak<br />
forces, time <strong>of</strong> peak forces, the first minimum and the time for the first minimum.<br />
Hysteresis Effects in abrasive and frictional Contacts<br />
Kristin M. de Payrebrune, Matthias Kröger (TU Freiberg) Schedule<br />
Grinding is a very complex and high dynamical material removal process with stochastically distributed<br />
grain engagements and strong varying local contact conditions. Over a long time only<br />
macroscopic effects are analyzed and predicted by empirical relation. To understand the dynamical<br />
behaviour also local effects must be considered.<br />
Therefore the local contact conditions and especially the local friction coefficient are analyzed.<br />
One detected effect is the dependency <strong>of</strong> the friction coefficient on the process forces and on<br />
the gradient <strong>of</strong> the forces, so a hysteresis loop occurs for increasing and decreasing values. This<br />
phenomenon is already studied for sliding objects in [1,2,3] but not for abrasion. With higher
Section 5: Nonlinear oscillations 113<br />
force values the dependency on the force gradient decrease, whereas for low normal forces the<br />
loop expand. With the force dependant friction coefficient local and dynamic effects are physically<br />
interpretable. In contrast to this is the global friction coefficient over the entire force range<br />
constant with which only quasi-static effects are describable.<br />
[1] Kröger, M.; Lindner, M. Popp, K.; Modellierung instationärer Reibkräfte, PAMM, 2, 140-141,<br />
2003<br />
[2] Stelter, P. Nichtlineare Schwingungen reibungserregter Strukturen, Fortschritts Bericht VDI-<br />
Reihe, 11, 1990<br />
[3] Ruina, A.L.; Constitutive Relations for Frictional, in Mechanics <strong>of</strong> Geomaterials, ed. Bazart,<br />
Z., Wiley, New York, 167-187, 1985<br />
Influence <strong>of</strong> viscous damping on friction induced travelling waves<br />
Alois Steindl (TU Wien) Schedule<br />
We consider a simple model <strong>of</strong> a brake, a rigid shaft rotating in an elastic cylinder. Due to the<br />
frictional contact between these bodies stick-slip travelling waves occur; also separation zones are<br />
possible, if the pressure between the bodies is small. Numerical investigations show, that these<br />
travelling waves are mostly unstable, which causes quasiperiodic and chaotic dynamics.<br />
In this talk we investigate the influence <strong>of</strong> viscous damping on the existence, shape and<br />
stability <strong>of</strong> the travelling wave solutions more closely. Preliminary calculations indicate, that<br />
the smoothening effect may stabilize the travelling waves against the Hopf bifurcation, but it also<br />
can destroy the travelling waves and force steady state solutions.<br />
The presence <strong>of</strong> the damping terms also changes the structure <strong>of</strong> the differential equations for<br />
the travelling waves by introducing a small leading coefficient. This singular perturbation also<br />
has smoothening effects at the transitions between the different solution regimes.<br />
Degenerate cases <strong>of</strong> stability loss <strong>of</strong> an elastic fluid-conveying tube<br />
Richard Jurisits, Alois Steindl (TU Wien) Schedule<br />
Motivated by the article [1], we consider a two-dimensional, slender elastic tube <strong>of</strong> length l being<br />
clamped to the upper end and with a point mass m being fixed to its lower end. The centerline<br />
<strong>of</strong> the tube is assumed to be inextensible, and the tube carries a fluid having a constant relative<br />
velocity U relative to the tube tangent to the centerline. Two springs with constants c are fixed<br />
to the tube at the position s = lξ (with 0 < ξ < 1) and exert forces only in horizontal direction.<br />
A coefficient α describes the internal material damping <strong>of</strong> the tube, and the effect <strong>of</strong> gravity is<br />
included.<br />
We adopt the model equations for the tube system from previous works, see [2], [3]. The linearized<br />
dimension-free governing equations, written in the standard form <strong>of</strong> a dynamical system read<br />
w = (w1, w2) = (u, ˙u), λ = (ρ, Γ, α, ξ) , (1)<br />
˙w = A(λ)w + g(w, λ) ,<br />
�<br />
0<br />
A(λ) =<br />
−C<br />
�<br />
1<br />
,<br />
−B<br />
(2)<br />
Cw1 = w ′′′′<br />
1 + ρ 2 w ′′<br />
1 − γ[(1 + Γ − s)w ′ 1] ′ , Bw2 = αw ′′′′<br />
2 + 2 � βρw ′ 2 , (3)<br />
and have to be supplemented by appropriate boundary and intermediate conditions. u and<br />
˙u represent the horizontal dislocation and velocity, respectively, <strong>of</strong> a tube element. The nondimensionalized<br />
parameters for U, m, α and ξ, forming the parameter vector λ, are considered
114 Section 5: Nonlinear oscillations<br />
as distinguished parameters.<br />
Performing a linear stability analysis <strong>of</strong> the straight downhanging equilibrium position <strong>of</strong> the<br />
tube (u = 0, ˙u = 0) leads to a three-point boundary-value inverse eigenvalue problem <strong>of</strong> two<br />
fourth-order ordinary differential equations, which can be solved numerically. The resulting stability<br />
diagrams show that steady-state-Hopf and Hopf-Hopf (two flutter) bifurcation interactions<br />
exist for certain parameter regimes. In this talk we focus on the possibility and the necessary<br />
conditions leading to degenerate cases in which both interactions merge, resulting in a coupled<br />
steady-state-Hopf-Hopf bifurcation.<br />
[1] M. Ghayesh, M. Paidoussis, and Y. Modarres-Sadeghi, Three-dimensional dynamics <strong>of</strong> a<br />
fluid-conveying cantilevered pipe fitted with an additional spring-Support and an end-mass,<br />
JSV 330, p. 2869–2899 (2011).<br />
[2] B. Albrecht, Dynamische Verzweigungen eines rotationssymmetrischen, flüssigkeitsdurchströmten<br />
Schlauches mit einer punktförmigen Masse, diploma thesis, TU Wien (1997).<br />
[3] M. Païdoussis, Fluid-structure interactions, Vols. 1 and 2, Academic Press (1998).<br />
Trigger <strong>of</strong> coupled singularities: Nonlinear dynamics <strong>of</strong> mechanical systems with coupled<br />
rotations about no intersecting axes or/and no ideal constraints<br />
Katica (Stevanović) Hedrih (Serbian Academy <strong>of</strong> Sciences, Belgrade/University <strong>of</strong> Nis) Schedule<br />
Starting <strong>of</strong> the numerous examples <strong>of</strong> mechanical system nonlinear dynamics with coupled rotations,<br />
series <strong>of</strong> governing nonlinear differential equations are derived. We focused our attentions<br />
to the system nonlinear dynamics with ideal as well as no ideal constraints with phase portrait<br />
containing coupled singularities and homoclinic orbit in the form <strong>of</strong> number eight. By using special<br />
example <strong>of</strong> heavy mass particle motion along ideal or no ideal rotating curvilinear rough line<br />
about vertical or skew axis series <strong>of</strong> the coupled singularities are identified. A theorem <strong>of</strong> trigger<br />
<strong>of</strong> coupled singularities and homoclinic orbit in the form <strong>of</strong> like number eight are presented.<br />
Transformations <strong>of</strong> the phase portrait structure with appearance and disappearance <strong>of</strong> trigger <strong>of</strong><br />
coupled singularities with change <strong>of</strong> bifurcation parameters are presented. A example od phase<br />
portrait <strong>of</strong> nonlinear dynamics <strong>of</strong> a heavy body coupled rotations about no intersecting axes is<br />
analyzed. Abstractions <strong>of</strong> real engineering system nonlinear dynamics with coupled rotations into<br />
models <strong>of</strong> a rigid body coupled rotations around nonintersecting axes in the gravitational field<br />
show us numerous varieties <strong>of</strong> the homoclinic phase trajectories as well as different sets <strong>of</strong> the<br />
tiger <strong>of</strong> coupled singularities. Also a series <strong>of</strong> the trigger <strong>of</strong> coupled singularities in the phase<br />
portraits and with trigger <strong>of</strong> coupled half-one side singularities are identified in the heavy mass<br />
particle oscillations/motion along rotating rough curvilinear line and no ideal constraints with<br />
Amontons-Coulomb type friction. Governing differential double equation <strong>of</strong> a heavy are analyzed<br />
and corresponding double equation <strong>of</strong> the phase trajectories are given. Linearizations <strong>of</strong> nonlinear<br />
or double differential equations around singular points from trigger <strong>of</strong> coupled singularities are<br />
used for analyzing stability or no stability <strong>of</strong> equilibrium positions or relative equilibrium positions<br />
<strong>of</strong> the system.<br />
Influence <strong>of</strong> gyroscopic effects on the nonlinear vibrations <strong>of</strong> high-speed rotors in<br />
hydrodynamic bearings<br />
Aydin Boyaci (KIT) Schedule<br />
To improve the efficiency <strong>of</strong> turbomachines, the corresponding rotors are operated with very high<br />
speeds. Thereby, high-speed rotors are <strong>of</strong>ten supported in hydrodynamic bearings which show se-
Section 5: Nonlinear oscillations 115<br />
veral oil whirl/oil whip phenomena. Though the nonlinear vibrations <strong>of</strong> such rotors are very well<br />
investigated, the influence <strong>of</strong> gyroscopic effects on the stability and bifurcation behavior <strong>of</strong> rotors<br />
in hydrodynamic bearings is not fully understood. Therefore, a single-disk rotor in two identical<br />
journal bearings is considered as a mechanical model. By applying a linear stability analysis, the<br />
threshold speeds <strong>of</strong> the equilibrium position are determined. After the nonlinear rotor bearing<br />
system loses its stability <strong>of</strong> the equilibrium position, the stability and bifurcations are analyzed<br />
by using numerical continuation methods. In conclusion, the effect <strong>of</strong> the inertia moments and<br />
the position <strong>of</strong> the disk is discussed on the nonlinear dynamics <strong>of</strong> the single-disk rotor in hydrodynamic<br />
bearings.<br />
S5.3: Nonlinear Oscillations III Wed, 16:00–18:00<br />
Chair: Edwin Kreuzer, Dietrich Flockerzi S1|03–104<br />
Liapunov Functions and Carleman Linearization<br />
Heffel, E., Hagedorn, P. (TU <strong>Darmstadt</strong>) Schedule<br />
In order to accurately predict the behavior <strong>of</strong> a nonlinear system, it is important to determine<br />
the domains <strong>of</strong> attraction <strong>of</strong> its stationary solutions. This is in general a difficult problem which<br />
can not be solved analytically. A common approach to estimate the domains <strong>of</strong> attraction <strong>of</strong> stationary<br />
solutions <strong>of</strong> autonomous or non-autonomous systems is via Liapunov functions. Defining<br />
an adequate Liapunov function is in general not easy, due to the lack <strong>of</strong> a systematic approach<br />
for its construction, at least in the non-autonomous case. If the nonlinearities in the system dynamics<br />
are sufficiently smooth, Carleman linearization can be used, not only to study the system<br />
dynamics but also to define appropriate Liapunov functions. The basic idea is to expand the<br />
non-autonomous nonlinear system into a higher dimensional autonomous and linear one, with a<br />
higher order error term, by treating nonlinearities as additional state variables. Neglecting the<br />
error term in a first instance, permits the systematic construction <strong>of</strong> Liapunov functions for the<br />
new, linear system. These Liapunov functions can then be used to estimate the domains <strong>of</strong> attraction,<br />
with the error term now being considered. This approach is demonstrated with simple<br />
examples. At least in these examples the method works surprisingly well. Of course the method<br />
can be used not only to study domains <strong>of</strong> attraction but also to examine stability regions in the<br />
parameter domain.<br />
Intermittent Control <strong>of</strong> Co-existing Attractors<br />
Yang Liu, Marian Wiercigroch, James Ing (University <strong>of</strong> Aberdeen) Schedule<br />
In the recent times, control <strong>of</strong> nonlinear dynamical systems has been among the most active fields<br />
<strong>of</strong> research due to its diverse applications in engineering. Most <strong>of</strong> the existing work has been<br />
focused on controlling chaos including stabilizing unstable periodic orbit, exploiting chaos‘ characteristics<br />
for its control, and synchronizing two identical or different chaotic systems. However,<br />
little attention has been paid to control <strong>of</strong> systems that exhibit multistability or co-existence <strong>of</strong><br />
several stable attractors for a given set <strong>of</strong> parameters, despite the fact that they are observed<br />
abundantly in different fields <strong>of</strong> science, e.g. [1].<br />
This paper proposes a new control method for a class <strong>of</strong> non-autonomous dynamical systems<br />
that naturally exhibit co-existing stable attractors. As it is known, in some papers on controlling<br />
co-existing attractors, e.g. [2], the control objective was achieved by the crisis <strong>of</strong> basins <strong>of</strong> attraction.<br />
However, destroying co-existing attractors is extremely difficult for some complex dynamical<br />
systems, e.g. [3], since any small perturbations <strong>of</strong> the system parameters can induce the emergence<br />
<strong>of</strong> new complicated basins <strong>of</strong> attraction. It is therefore we propose a method <strong>of</strong> intermittent
116 Section 5: Nonlinear oscillations<br />
control here without changing the original basins <strong>of</strong> attraction <strong>of</strong> the system. The central idea<br />
is based on understanding <strong>of</strong> the system‘s basins <strong>of</strong> attraction where the control action is being<br />
switched on only in the vicinity <strong>of</strong> the crossings <strong>of</strong> the actual and the desired trajectories. This<br />
paper also focuses on appropriate selection <strong>of</strong> the control force, which is triggered when a certain<br />
criterion is satisfied.<br />
The method we proposed is applied to a well-known Duffing oscillator and an impact oscillator.<br />
Both numerical and experimental results reveal that the proposed method is effective, and<br />
therefore it can be applied to a broad range <strong>of</strong> continuous and discontinuous systems. For practical<br />
purposes, the constrained intermittent control is considered, and is applied to the two example<br />
systems in simulation and experiment. Further discussion is made for the forcing amplitude <strong>of</strong><br />
intermittent control and the duration <strong>of</strong> control action.<br />
[1] J. Ing, E. Pavlovskaia, M. Wiercigroch, S. Banerjee, Experimental Study <strong>of</strong> Impact Oscillator<br />
with One-sided Elastic Constraint, Phil. Trans. R. Soc. A 366 (2008), 679 – 704.<br />
[2] O. Olusola, U. Vincent, A. Njah, Synchronization, Multistability and Basin Crisis in Coupled<br />
Pendula, J. Sound and Vibration 329 (2010), 443 – 456.<br />
[3] E. Pavlovskaia, J. Ing, M. Wiercigroch, S. Banerjee, Complex Dynamics <strong>of</strong> Bilinear Oscillator<br />
Close to Grazing, Int. J. Bifurcation and Chaos 20 (2010), 3801 – 3817.<br />
Algorithms for the solution <strong>of</strong> parameter dependent quadratic eigenvalue problems<br />
Urs Miller (<strong>Universität</strong> Stuttgart), Lothar Gaul Schedule<br />
The solution <strong>of</strong> mechanical problems <strong>of</strong>ten leads to quadratic eigenvalue problems (λ 2 M(p) +<br />
λP(p) + Q(p))x = 0 with complex eigenvectors, especially if damping or gyroscopic effects are to<br />
be considered. The system matrices are considered as dependent on a parameter p in this work.<br />
Usually, the quadratic eigenvalue problem is solved by transformation to a standard eigenvalue<br />
problem, where the dimension <strong>of</strong> the matrices doubles. Because this leads to an increase <strong>of</strong> memory<br />
consumption, alternative algorithms for the direct solution <strong>of</strong> quadratic eigenvalue problems are<br />
presented and compared.<br />
For the parameter dependent problem, it is convenient to use a predictor corrector method.<br />
This is compared to the solution with quadratic versions <strong>of</strong> the Rayleigh quotient iteration and<br />
the Jacobi Davidson algorithm.<br />
The algorithms are tested by some examples from dynamical systems with and without gyroscopic<br />
effects.<br />
Methology <strong>of</strong> reduced order modeling (ROMing) applying Proper Orthogonal Decomposition<br />
(POD) <strong>of</strong> boiling water reactor (BWR) fuel assemblies (FAs) applied to<br />
introductory examples<br />
D. P. Prill, M. Stockmaier, A. G. Class (KIT), F. Wehle (AREVA Erlangen) Schedule<br />
For high power low flow operating conditions associated with unfavorable power distribution<br />
BWR operation requires attention with respect to density wave oscillations. The main drivers <strong>of</strong><br />
these phenomena are the multiple thermal hydraulic interactions between power, flow rate, and<br />
density, reinforced by the neutronics feedback.<br />
Admissible reactor operation conditions maintain a certain distance to the stability limit given<br />
by linear theory. Evaluation <strong>of</strong> non-linear states requires time-consuming numerical integration<br />
or experimental data but this depends on the specific transients considered. Non-linear stability<br />
analysis aims at accelerating simulations and provides assessment <strong>of</strong> the whole parameter space.
Section 5: Nonlinear oscillations 117<br />
In our transient analysis, the physical behavior <strong>of</strong> the system is approximated by a reduced<br />
order model (ROM) that respects stability relevant characteristics. Proper orthogonal decomposition<br />
(POD), i.e a spectral method based on experimental or computational fluid dynamics<br />
(CFD) data, is capable <strong>of</strong> detecting oscillating states <strong>of</strong> the physical system. Moreover, POD provides<br />
a well-defined truncation criterion for the minimum number <strong>of</strong> modes. A Galerkin method<br />
employing POD modes as ansatz functions yields a non-linear ROM.<br />
In the talk the chosen strategy is firstly applied to toy examples, i.e. the Korteweg de-Vries<br />
(KdV) equation, and secondly to simplified reactor physics [1].<br />
[1] T. Ortega-Gomez, Stability Analysis <strong>of</strong> the High Performance Light Water Reactor, Forschungszentrum<br />
Karlsruhe, FZKA 7432, 2009, Germany<br />
http://bibliothek.fzk.de/zb/berichte/FZKA7432.pdf<br />
Symmetry and self-excited vibrations<br />
Gottfried Spelsberg-Korspeter (TU <strong>Darmstadt</strong>) Schedule<br />
Self-excited vibrations can be wanted or unwanted depending on where they occur. For the excitation<br />
mechanism <strong>of</strong> flutter it can be shown that the excitation mechanism is directly related<br />
to symmetries <strong>of</strong> the structure. This knowledge can either be used to avoid self-excitation but<br />
can also be used to initiate self-excitation. The avoidance <strong>of</strong> self-excited vibrations is for example<br />
beneficial to brakes and paper calenders whereas the initiation can be useful for example in<br />
energy harvesting. Here self-excitation is a very desireable mechanism since it does hardly depend<br />
on the frequency <strong>of</strong> the underlying structure. The current paper aims at showing the underlying<br />
mechanisms and to exploit potential applications.<br />
Rotor Stator Interaction with Many Degrees <strong>of</strong> Freedom<br />
Oliver Alber (TU <strong>Darmstadt</strong>) Schedule<br />
If an unbalanced rotor touches non-rotating parts (e. g. the housing) its dynamics becomes nonlinear.<br />
As a result synchronous as well as asynchronous motions are possible. Asynchronous motion<br />
patterns, especially in the case <strong>of</strong> a backward whirl motion, may exhibit large deflections <strong>of</strong> rotor<br />
and stator in combination with large contact forces that might lead to severe damage <strong>of</strong> the<br />
whole system. Earlier studies on the resulting dynamics <strong>of</strong> these systems focus predominantly<br />
on a one-mass flexible rotor (Jeffcott rotor) which is in contact with a stator with one degree <strong>of</strong><br />
freedom only. For this case both analytical descriptions <strong>of</strong> the resulting synchronous motion and<br />
their stability as well as approximate solutions or parameter studies for asynchronous motion are<br />
available. However, in systems <strong>of</strong> practical interest typically not only a single resonance frequency<br />
<strong>of</strong> the rotor stator system is relevant but many resonance frequencies <strong>of</strong> both rotor and stator<br />
may contribute significantly. Thus, the question arises to which extent these previous results can<br />
be extended to systems with many degrees <strong>of</strong> freedom. It is a main purpose <strong>of</strong> this contribution<br />
to address this issue.<br />
In particular, in this contribution the dynamics <strong>of</strong> a system consisting <strong>of</strong> a Multi-Disk Rotor<br />
is investigated which is in contact with a system <strong>of</strong> flexibly mounted rigid stator rings. Both rotor<br />
and stator are affected by external viscous damping. The contact areas between rotor and stator<br />
are cylindrical surfaces with a clearance and account for dry friction between them. The dynamics<br />
<strong>of</strong> the whole system is explored numerically in parameter regimes <strong>of</strong> practical interest.
118 Section 5: Nonlinear oscillations<br />
S5.4: Nonlinear Oscillations IV Thu, 13:30–15:30<br />
Chair: Dietrich Flockerzi, Edwin Kreuzer S1|03–107<br />
Nonlinear vibration analysis <strong>of</strong> general supersonic composite laminated plates<br />
Ardeshir Guran (Institute <strong>of</strong> Strutronics, Canada) Schedule<br />
The nonlinear aeroelastic behavior <strong>of</strong> a three-dimensional general laminated composite plate at<br />
high supersonic Mach numbers is investigated. The von-Karman’s large deflection plate theory is<br />
assumed for structural modelling and the linear piston theory is used for aerodynamic modeling.<br />
The effects <strong>of</strong> in-plane force, static pressure differential, fiber orientation and aerodynamic damping<br />
on flutter behavior <strong>of</strong> the plates are considered. The numerical results obtained from the<br />
integration <strong>of</strong> the governing nonlinear differential equations <strong>of</strong> the system were compared with<br />
those obtained by ANSYS.<br />
Finite oscillations <strong>of</strong> a channel with a flexible wall conveying viscous flow<br />
Karolina Bach, Hartmut Hetzler, Wolfgang Seemann (KIT) Schedule<br />
The interaction between a flexible structure and flowing fluid can cause flow-induced vibrations<br />
and the steady state may loose stability by divergence or flutter, thus leading to undesirable<br />
dynamic behaviour.<br />
As a model for fluid-structure-interaction a planar and infinitely long channel is studied. The<br />
flow is bounded by a rigid and a flexible wall. The latter is modelled as a one-parametric, nonpermeable<br />
continuum on an elastic foundation, which exhibits bending and extensional stiffness.<br />
It can be shown that for thin channels the coupling effects are strong and therefore the focus <strong>of</strong><br />
this contribution is to investigate the behaviour <strong>of</strong> a channel, where the structural displacements<br />
are large compared to the gap width. Due to this large amplitudes a linear description <strong>of</strong> the<br />
interface between fluid and structure will not be sufficient anymore and the relation between the<br />
Eulerian description <strong>of</strong> the fluid and the Lagrangian description <strong>of</strong> the structure must be taken<br />
into account: eventually, this yields nonlinear boundary conditions.<br />
Furthermore in narrow gaps the viscosity <strong>of</strong> the fluid cannot be ignored. Hence the effect <strong>of</strong> viscosity<br />
will also be considered within this contribution. In order to allow for analytical results and<br />
keep the focus on the effects due to large displacements, a simplified fluid model is adopted: it is<br />
assumed that the fluid is viscous, incompressible and that inertia terms may be neglected, thus<br />
linear equations apply.<br />
A perturbation analysis is utilized to determine the stability <strong>of</strong> the steady state as well as the<br />
post-critical behaviour <strong>of</strong> the coupled problem.<br />
How weathering influences the vibration behavior <strong>of</strong> oil paintings<br />
Kerstin Kracht, Utz von Wagner (TU Berlin) Schedule<br />
Oil paintings undergo vibrations due to multiple reasons. During transports high excitation levels<br />
are reached. But also during exposition there is excitation by trespassing public or external traffic<br />
load. Consequences may be damages in these art treasures. The presentation describes final results<br />
<strong>of</strong> extensive experiments undertaken with a number <strong>of</strong> test dummies prepared by a docent <strong>of</strong> old<br />
painting techniques. These test dummies were weathered over two years at a research institution<br />
for paint and varnish at Magdeburg. There were alternating periods <strong>of</strong> weathering and measurements.<br />
In the measurement periods the dummies were investigated for their dynamical behavior<br />
using different excitations (harmonic, broad-band) and dynamic responses were measured using<br />
special laser equipment newly adapted for measurements on the surface <strong>of</strong> painted canvas. Due<br />
to chemical processes stiffness and density <strong>of</strong> the layers vary with corresponding influence on cha-
Section 5: Nonlinear oscillations 119<br />
racteristic frequencies. Also varying occurrence <strong>of</strong> nonlinearities could be observed. The presented<br />
work should finally lead to condition monitoring <strong>of</strong> oil paintings and techniques for the prevention<br />
<strong>of</strong> artworks from vibrations.<br />
On forced longitudinal vibrations <strong>of</strong> an axially moving yarn<br />
Andreas Franze, Bernd W. Zastrau (TU Dresden) Schedule<br />
During the manufacturing process <strong>of</strong> textiles, yarns are transported between rollers. Because <strong>of</strong><br />
the relative motion <strong>of</strong> yarn and roller the boundary conditions can not be assigned to fixed material<br />
particles. Therefore this system is an example for media in motion with non-material boundary<br />
conditions.<br />
The equation <strong>of</strong> motion for an arbitrary time-varying transport velocity <strong>of</strong> the yarn is derived<br />
from the balance equations. After linearisation <strong>of</strong> the system equations the analytical solution is<br />
analysed and discussed.<br />
Sudden Instabilities and Barring in Paper Machinery<br />
Steffen Wiendl, Gottfried Spelsberg-Korspeter (TU <strong>Darmstadt</strong>) Schedule<br />
The manufacturing <strong>of</strong> high quality paper is still a challenge to the engineers working in the construction<br />
<strong>of</strong> paper machinery. Due to increasing production speeds and increasing width <strong>of</strong> the<br />
nips vibration problems are harder to suppress. This work is concerned with vibration problems<br />
arising in the process <strong>of</strong> paper calendering where in one <strong>of</strong> the last production steps the surface<br />
<strong>of</strong> the paper is rened in huge calenders. In modern paper calenders two types <strong>of</strong> self-excited vibrations<br />
are observed. Sometimes the rollers get into sudden instabilities which may damage the<br />
whole production line if it is not shut <strong>of</strong> immediately. The second phenomenon is barring which is<br />
a corrugation <strong>of</strong> the roller surfaces which develops on a smaller time scale. In this paper models<br />
are developed to model the vibrational behavior <strong>of</strong> paper calenders with detailed focus on the<br />
nip and the wear <strong>of</strong> the rollers. The models can build the basis for constructive measures against<br />
squeal.<br />
Zur Interaktion von Sägedraht und Ingot<br />
M. Lorenz, A. Ams (TU Freiberg) Schedule<br />
Es wird ein mechanisches Modell zur Beschreibung des bewegten Sägedrahtes unter Einwirkung<br />
des Siliziumblocks (Ingot) vorgestellt. Mit dem Prinzip von Hamilton wird, unter der Voraussetzung<br />
nichtlinearer Verformungskinematik sowie unter Berücksichtigung der Dehn- und Biegesteifigkeit<br />
des Drahtes, das Variationsproblem und die Bewegungsgleichungen hergeleitet. Die<br />
Wirkung des Ingot auf den bewegten Draht wird als Folgelast modelliert. Zudem werden die<br />
mechanischen Eigenschaften von Ingot und Bettung in Abhängigkeit von Schnitttiefe und Schnittanzahl<br />
bzw. Drahtposition mittels FEM bestimmt und in das Modell integriert. Ausgehend vom<br />
Variationsproblem wird mit einem gemischten Ritz-Ansatz die stationäre Lage des Drahtes für<br />
verschiedene Einflussparameter berechnet und Stabilitätsuntersuchungen durchgeführt.
120 Section 6: Material modelling in solid mechanics<br />
Section 6: Material modelling in solid mechanics<br />
Organizers: Daniel Balzani (<strong>Universität</strong> Duisburg-Essen), Wolfgang Dreyer (WIAS Berlin)<br />
S6.1: Microstructures in Elasto-Plasticity I Tue, 13:30–15:30<br />
Chair: Thorsten Bartel S1|01–A03<br />
A model for martensitic microstructure, its geometry and interface effects<br />
Mehdi Goodarzi, Klaus Hackl (<strong>Universität</strong> Bochum) Schedule<br />
Martensitic materials demonstrate a characteristic microstructure in the form <strong>of</strong> parallel layers <strong>of</strong><br />
compatible phases. This is the consequence <strong>of</strong> a symmetry-breaking phase transformation which<br />
can be well understood within a continuum mechanical framework by investigating energetically<br />
favorable configurations <strong>of</strong> phase mixtures. We present a micromechanical model built upon this<br />
approach that reflects numerous attributes <strong>of</strong> the microstructure.<br />
In this model, a specific class <strong>of</strong> laminate geometries is constructed based on coherence condition<br />
allowing for curved twin interfaces as well as three-dimensional aggregates. Proper forms <strong>of</strong><br />
surface energies are then proposed based on scaling arguments and crystallographic considerations.<br />
We afterwards look into energy minimizing geometries within the class <strong>of</strong> morphologies that<br />
are considered. The results are notably compliant to the observed scale properties, size effects<br />
and accommodation patterns in the microstructure <strong>of</strong> martensite.<br />
A Formulation <strong>of</strong> Finite Gradient Crystal Plasticity with Systematic Separation <strong>of</strong><br />
Long- and Short-Range States<br />
S. Mauthe, F. Hildebrand, C. Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
With the ongoing trend <strong>of</strong> miniaturization and nanotechnology, the predictive modeling <strong>of</strong> size<br />
effects play an increasingly important role in metal plasticity. These size effects mainly stem<br />
from geometrically necessary dislocations whose description requires gradient-extended theories<br />
<strong>of</strong> crystal plasticity. However, a key challenge <strong>of</strong> the formulation and numerical implementation <strong>of</strong><br />
gradient crystal plasticity is the complexity within full multislip scenarios, in particular in context<br />
<strong>of</strong> rate-independent settings.<br />
In order to partially overcome this difficulty, we suggest a new viscous regularized formulation<br />
<strong>of</strong> rate-independent crystal plasticity, that exploits in a systematic manner the long- and<br />
short-range nature <strong>of</strong> the involved variables. To this end, we outline a multifield scenario, where<br />
the macro-deformation and the plastic slips on crystallographic systems are the primary fields.<br />
Related to these primary fields, we define as the long-range state the deformation gradient, the<br />
plastic slips and their gradients. We then introduce as the short-range plastic state the plastic<br />
deformation map, the dislocation density tensor and scalar hardening parameters associated with<br />
the slip systems. It is then shown that the evolution <strong>of</strong> the short range state is fully determined<br />
by the evolution <strong>of</strong> the long-range state. This separation into long- and short-range states<br />
is systematically exploited in the algorithmic treatment by a new update structure, where the<br />
short-range variables play the role <strong>of</strong> a local history base.<br />
The model problem under consideration accounts in a canonical format for basic effects related<br />
to statistically stored and geometrically necessary dislocation flow, yielding micro-force balances<br />
including non-convex cross-hardening, kinematic hardening and size effects. Further key ingredients<br />
<strong>of</strong> the proposed algorithmic formulation are geometrically exact updates <strong>of</strong> the short-range<br />
state and a destinct regularization <strong>of</strong> the rate-independent dissipation function that preserves the<br />
range <strong>of</strong> the elastic domain.<br />
The formulation is shown to be fully variational in nature, goverend by rate-type continuous
Section 6: Material modelling in solid mechanics 121<br />
and incremental algorithmic variational principles. We demonstrate the modeling capabilities and<br />
algorithmic performance by means <strong>of</strong> representative numerical examples for multislip scenarios<br />
in fcc single crystals.<br />
Numerical Implementation <strong>of</strong> a Three-Dimensional Continuum Dislocation Microplasticity<br />
Theory<br />
Stephan Wulfingh<strong>of</strong>f, Thomas Böhlke (KIT) Schedule<br />
The modelling <strong>of</strong> the mechanical behaviour <strong>of</strong> micro-devices can not be established by classical<br />
continuum mechanical plasticity models without internal length scale. Depending on the system<br />
size, ab-initio simulations or Discrete Dislocation Dynamics serve as mature tools to predict the<br />
mechanical response <strong>of</strong> very small systems. Anyhow, the gap between these discrete and classical<br />
continuum mechanical methods is not yet filled. Besides phenomenological gradient plasticity<br />
models, dislocation density based approaches have emerged which account explicitly for dislocation<br />
transport and line length increase. The presentation is based on the kinematical continuum<br />
mechanical dislocation framework <strong>of</strong> Hochrainer et al. [1] which can be considered as a generalization<br />
<strong>of</strong> Nye’s theory [3]. The theory transfers the kinematics <strong>of</strong> three-dimensional systems <strong>of</strong><br />
discrete dislocations to a continuum mechanical representation in terms <strong>of</strong> continuously distributed<br />
dislocations. An averaged version <strong>of</strong> the theory by Hochrainer et al. [2] (see also Sandfeld et<br />
al. [4]) leads to a significant reduction <strong>of</strong> the computational simulation effords and will mainly<br />
be addressed. The kinematical dislocation theory is coupled to a crystal plasticity framework.<br />
The presentation will focus on the numerical implementation <strong>of</strong> the theory, especially on promising<br />
schemes for the numerical coupling <strong>of</strong> the set <strong>of</strong> PDEs. Finite Element simulation results<br />
demonstrate the performance <strong>of</strong> the implementation in three-dimensional applications.<br />
[1] T. Hochrainer, M. Zaiser and P. Gumbsch, A three-dimensional continuum theory <strong>of</strong> dislocations:<br />
kinematics and mean field formulation. Philosophical Magazine 87 (2007), 1261–1282.<br />
[2] T. Hochrainer, M. Zaiser and P. Gumbsch, Dislocation transport and line length increase in<br />
averaged descriptions <strong>of</strong> dislocations. arXiv:1010.2884v1<br />
[3] J. F. Nye, Some geometrical relations in dislocated crystals. Acta Metallurgica 1 (1953),<br />
153–162.<br />
[4] S. Sandfeld, T. Hochrainer, M. Zaiser and P. Gumbsch, Continuum modeling <strong>of</strong> dislocation<br />
plasticity: Theory, numerical implementation, and validation by discrete dislocation<br />
simulations. J. Mater. Res. 26 (2011), 623–632.<br />
Rigorous derivation <strong>of</strong> a dissipation for laminate microstructures<br />
Sebastian Heinz (WIAS Berlin) Schedule<br />
We study models for finite plasticity in the framework <strong>of</strong> rate-independent evolutionary systems.<br />
The corresponding incremental minimization problems, in general, admit no solutions due to<br />
the creation <strong>of</strong> microstructure, see [1]. We focus on the case where the microstructure is made <strong>of</strong><br />
simple laminates only. We show in a mathematical rigorous way how the incremental minimization<br />
problem can be relaxed and identify the relaxed dissipation as the one introduced in [2].<br />
[1] C. Carstensen, K. Hackl, A. Mielke. Non-convex potentials and microstructures in finite-strain<br />
plasticity, Proc. Royal Soc. London, Ser. A 458 (2002), 299 – 317.
122 Section 6: Material modelling in solid mechanics<br />
[2] K. Hackl, D. M. Kochmann. Relaxed potentials and evolution equations for inelastic microstructures.<br />
In B. Daya Reddy, editor, IUTAM Symposium on Theoretical, Computational<br />
and Modelling Aspects <strong>of</strong> Inelastic Media, pages 27 – 39. Springer-Verlag, 2008.<br />
Thermodynamically and variationally consistent modeling <strong>of</strong> distortional hardening:<br />
application to magnesium<br />
Baodong Shi (Helmholtz-Zentrum Geesthacht), Jörn Mosler (Helmholtz-Zentrum Geesthacht, TU<br />
Dortmund) Schedule<br />
To capture the complex elastoplastic response <strong>of</strong> many materials, classical isotropic and kinematic<br />
hardening alone are <strong>of</strong>ten not sufficient. Typical phenomena which cannot be predicted by the<br />
aforementioned hardening models include, among others, cross hardening or more generally, the<br />
distortion <strong>of</strong> the yield function. However, such phenomena do play an important role in several<br />
applications in particular, for non-radial loading paths. Thus, they usually cannot be ignored. In<br />
the present contribution, a novel macroscopic model capturing all such effects is proposed. In contrast<br />
to most <strong>of</strong> the existing models in the literature, it is strictly derived from thermodynamical<br />
arguments. Furthermore, it is the first macroscopic model including distortional hardening which<br />
is also variationally consistent. More explicitly, all state variables follow naturally from energy<br />
minimization within advocated framework.<br />
A viscosity-limit approach to the evolution <strong>of</strong> microstructures in finite plasticity<br />
Christina Günther, Klaus Hackl (<strong>Universität</strong> Bochum) Schedule<br />
Material microstructures in finite single-slip crystal plasticity occur and evolve due to deformation.<br />
Their formation is not arbitrary, they tend to form structured spatial patterns. This hints at a<br />
universal underlying mechanism, in the same manner as the minimization <strong>of</strong> the global energy governs<br />
the behavior <strong>of</strong> purely elastic materials. For non-quasiconvex potentials, the minimizers are<br />
small scale fluctuations, related to probability distributions <strong>of</strong> the deformation gradients, which<br />
can be found by the relaxation <strong>of</strong> the potential.<br />
As in the approach <strong>of</strong> D.Kochmann and K.Hackl, we use a variational framework, focusing on the<br />
Lagrange functional. For the treatment <strong>of</strong> the laminates, the potentials have to be adapted. The<br />
new approach rests on the introduction <strong>of</strong> a small smooth transition zone between the laminates<br />
in order to avoid a global minimization. This makes the evolution equations more handable for<br />
numerical calculations. We present explicit time-evolution equations for the volume fractions and<br />
the internal variables. We outline a numerical scheme and show some examples.<br />
S6.2: Polymers and Elastomers I Tue, 13:30–15:30<br />
Chair: Mikhail Itskov, Vladimir Kolupaev S1|01–A1<br />
Constitutive modelling <strong>of</strong> chemical ageing<br />
Alexander Lion, Michael Johlitz (<strong>Universität</strong> der Bundeswehr München) Schedule<br />
In order to model chemical ageing <strong>of</strong> rubber a three-dimensional theory is proposed. The fundamentals<br />
<strong>of</strong> this approach are different decompositions <strong>of</strong> the deformation gradient in combination<br />
with an additive split <strong>of</strong> the Helmholtz free energy into three parts. Its first part belongs to the<br />
volumetric material behaviour. The second part is a temperature-dependent hyperelasticity model<br />
which depends on an additional internal variable to consider the long-term degradation <strong>of</strong> the<br />
primary rubber network. The third contribution is a functional <strong>of</strong> the deformation history and a<br />
further internal variable; it describes the creation <strong>of</strong> a new network which remains free <strong>of</strong> stress
Section 6: Material modelling in solid mechanics 123<br />
when the deformation is constant in time. The constitutive relations for the stress tensor and the<br />
internal variables are deduced using the Clausius-Duhem inequality. In order to sketch the main<br />
properties <strong>of</strong> the model, expressions in closed form are derived with respect to continuous and<br />
intermittent relaxation tests as well as for the compression set test. Under the assumption <strong>of</strong> near<br />
incompressible material behaviour, the theory can also represent ageing-induced changes in volume<br />
and their effect on the stress relaxation. The simulations are in accordance with experimental<br />
data from literature.<br />
[1] A. Lion, M. Johlitz, On the representation <strong>of</strong> chemical ageing <strong>of</strong> rubber in continuum mechanics,<br />
International Journal <strong>of</strong> Solids and Structures, under review.<br />
Multi-phase modeling <strong>of</strong> shape memory polymers<br />
Nico Hempel, Markus Böl (TU Braunschweig) Schedule<br />
Shape memory polymers are a highly versatile class <strong>of</strong> so-called smart materials. They are able to<br />
store a certain state <strong>of</strong> deformation and remember another one by means <strong>of</strong> an external stimulus<br />
such as light or temperature. Usually, the physical mechanism responsible for this behavior is a<br />
temperature-dependent phase transition between an “active”, entropy-elastic phase and a “frozen”,<br />
energy-elastic phase. As polymers are usually capable <strong>of</strong> experiencing large deformations, models<br />
are required which are able to represent both the phase transitions and states <strong>of</strong> large deformation.<br />
In the present work, we propose a model based on the idea <strong>of</strong> the multiplicative decomposition<br />
<strong>of</strong> the deformation gradient. Evolution equations for the several deformation components are<br />
presented that provide for the storage <strong>of</strong> the entropy-elastic strain and its recovery during the<br />
transition between the frozen phase and the active phase. First characteristic shape memory cycles<br />
will be presented as a last point.<br />
On response functions in linear thermoelastic models <strong>of</strong> shape memory polymers<br />
Aycan Özlem Aydin, Rasa Kazakevičiute-Makovska , Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
There are two basic classes <strong>of</strong> constitutive models for thermoresponsive Shape Memory Polymers<br />
(SMPs), rheological and thermoelastic models. In this work, we present a detailed analysis <strong>of</strong><br />
linear thermoelastic models. The first model within this class has been proposed by Liu et al. [1]<br />
and in the following years numerous modifications <strong>of</strong> that model have been presented (cf. e.g. [2]).<br />
All these models have a common mathematical structure with three basic response functions.<br />
Different models developed within this concept follow from the general theory by specifications<br />
<strong>of</strong> the relevant response functions. The general mathematical form <strong>of</strong> the response functions<br />
is discussed and an experimental methodology determining <strong>of</strong> response functions directly from<br />
experimental data is presented. Representative examples illustrate the quality and the efficiency<br />
<strong>of</strong> the proposed methodology. It is shown that a reliable evaluation <strong>of</strong> thermoelastic models for<br />
SMPs requires a comparison with data for all four steps <strong>of</strong> the termomechanical cycle, both under<br />
strain- and stress controlled conditions.<br />
[1] Y. Liu, K. Gall, M. L. Dunn, A. R. Greenberg, J. Diani, Thermomechanics <strong>of</strong> shape memory<br />
polymers: Uniaxial experiments and constitutive modeling, Int. J. Plasticity, vol. 22, pp.<br />
279-313, 2006.<br />
[2] R. Kazakevičiute-Makovska, H. Steeb, A. Özlem Aydın, On the evolution law for the frozen<br />
fraction in the linear theories <strong>of</strong> shape memory polymers, Arch. App. Mech., in press, 2011.
124 Section 6: Material modelling in solid mechanics<br />
Modeling the finite strain deformation and initial anisotropy <strong>of</strong> amorphous thermoplastic<br />
polymers<br />
Philipp Hempel, Thomas Seelig (KIT) Schedule<br />
The present work deals with modeling the temperature dependent finite strain deformation behavior<br />
<strong>of</strong> amorphous thermoplastic polymers incorporating the effect <strong>of</strong> an initial anisotropy. The<br />
anisotropy prevails in form <strong>of</strong> a frozen-in pre-orientation <strong>of</strong> molecular chains and results from preceding<br />
manufacturing processes (e.g. injection molding) at elevated temperatures and subsequent<br />
rapid cooling. The initial molecular orientation affects the mechanical response in terms <strong>of</strong> flow<br />
strength and hardening.<br />
The standard finite strain kinematics with a multiplicative split <strong>of</strong> the deformation gradient into<br />
an elastic and plastic part is modified by introducing a network deformation gradient which comprises<br />
the actual plastic deformation and the initial (processing induced) pre-deformation [1],[2].<br />
As a computational example, an injection molded plate is investigated which displays nonuniform<br />
shrinkage and buckling during heating due to the action <strong>of</strong> the frozen-in network stress. The<br />
spatial distribution <strong>of</strong> molecular pre-orientation, and hence initial anisotropy, in the FE model is<br />
estimated from optical birefringence.<br />
[1] E.M. Arruda, M.C. Boyce, Evolution <strong>of</strong> plastic anisotropy in amorphous polymers during<br />
finite straining, International Journal <strong>of</strong> Plasticity (1993), 6 –697.<br />
[2] M.C. Boyce, D.M. Parks, A.S. Argon, Plastic flow in oriented glassy polymers, International<br />
Journal <strong>of</strong> Plasticity (1998), 6 – 593.<br />
Modeling <strong>of</strong> induced anisotropy at large deformations for polymers<br />
Ismail Caylak, Rolf Mahnken (<strong>Universität</strong> Paderborn) Schedule<br />
In this presentation we develop a model to describe the induced plasticity <strong>of</strong> polymers at large<br />
deformations. Polymers such as stretch films exhibit a pronounced strength in the loading direction.<br />
The undeformed state <strong>of</strong> the films is isotropic, whereas after the uni-axial loading the<br />
material becomes anisotropic. In order to consider this induced ansiotropy during the stretch<br />
process, a spectral decomposition <strong>of</strong> the inelastic Cauchy-Green tensor is done. Therefore, the<br />
yield function can be formulated as a function <strong>of</strong> the anisotropic tensor, where again the anisotropic<br />
tensor is a function <strong>of</strong> the maximum eigenvalue. A backward Euler scheme is used for<br />
updating the evolution equations, and the algorithmic tangent operator is derived. The numerical<br />
implementation <strong>of</strong> the resulting set <strong>of</strong> constitutive equations is used in a finite element program<br />
and for parameter identification.<br />
S6.3: Microstructures in Elasto-Plasticity II Tue, 16:00–18:00<br />
Chair: Dennis Kochmann, Sebastian Heinz S1|01–A03<br />
Microstructure development in a Cosserat continuum as a consequence <strong>of</strong> energy<br />
relaxation<br />
Muhammad Sabeel Khan, Klaus Hackl (<strong>Universität</strong> Bochum) Schedule<br />
A rate-independent inelastic material model for a Cosserat continuum is presented. The free energy<br />
<strong>of</strong> the material is enriched with an interaction potential taking into account the intergranular
Section 6: Material modelling in solid mechanics 125<br />
kinematics at the continuum scale. As a result the total energy becomes non-convex, thus giving<br />
rise to the development <strong>of</strong> microstructure. To guarantee the existence <strong>of</strong> minimizers an exact<br />
quasi-convex envelope <strong>of</strong> the corresponding energy functional is derived. As a result microstructure<br />
occurs in both the displacement and micro-rotation field. The corresponding relaxed energy<br />
is then used for finding the minimizers <strong>of</strong> the two field minimization problem corresponding to a<br />
Cosserat continuum. Finite element formulation and numerical simulations are presented. Analytical<br />
and numerical results are discussed.<br />
About the Microstructural Effects <strong>of</strong> Polycrystalline Materials and their Macroscopic<br />
Representation at Finite Deformation<br />
Eva Lehmann, Stefan Loehnert, Peter Wriggers (<strong>Universität</strong> Hannover) Schedule<br />
In the sheet bulk metal forming field, the strict geometrical requirements <strong>of</strong> the workpieces result<br />
in a need <strong>of</strong> a precise prediction <strong>of</strong> the material behaviour. The simulation <strong>of</strong> such forming processes<br />
requires a valid material model, performing well for a huge variety <strong>of</strong> different geometrical<br />
characteristics and finite deformation.<br />
Because <strong>of</strong> the crystalline nature <strong>of</strong> metals, anisotropies have to be taken into account. Macroscopically<br />
observable plastic deformation is traced back to dislocations within considered slip<br />
systems in the crystals causing plastic anisotropy on the microscopic and the macroscopic level.<br />
A finite crystal plasticity model is used to model polycrystalline materials in representative<br />
volume elements (RVEs) <strong>of</strong> the microstructure. A multiplicative decomposition <strong>of</strong> the deformation<br />
gradient into elastic and plastic parts is performed, as well as a volumetric-deviatoric split <strong>of</strong> the<br />
elastic contribution. In order to circumvent singularities stemming from the linear dependency<br />
<strong>of</strong> the slip system vectors, a viscoplastic power-law is introduced providing the evolution <strong>of</strong> the<br />
plastic slips and slip resistances.<br />
The model is validated with experimental microstructural data under deformation. The validation<br />
on the macroscopic scale is performed through the reproduction <strong>of</strong> the experimentally<br />
calculated initial yield surface. Additionally, homogenised stress-strain curves from the microstructure<br />
build the outcome for a suitable effective material model. Through optimisation techniques,<br />
effective material parameters can be determined and compared to results from real forming processes.<br />
A rheological model for arbitrary symmetric distortion <strong>of</strong> the yield surface<br />
A.V. Shutov, J. Ihlemann (TU Chemnitz) Schedule<br />
A new rheological model is presented, which provides insight into phenomenological modelling <strong>of</strong><br />
combined nonlinear kinematic and distortional hardening. The model is constructed by coupling<br />
idealized two-dimensional rheological elements like Hooke-body, Newton-body, and modified St.<br />
Venant element [1,2]. The symmetric distortion <strong>of</strong> the yield surface and its orientation depending<br />
on the recent loading path are captured by the rheological model in a vivid way. We emphasize the<br />
flexibility <strong>of</strong> the proposed approach since it can be used to capture any smooth convex saturated<br />
form <strong>of</strong> the yield surface observed experimentally, if the yield surface is symmetric with respect to<br />
the recent loading direction. In particular, an arbitrary sharpening <strong>of</strong> the saturated yield locus in<br />
the loading direction combined with a flattening on the opposite side can be taken into account<br />
[2]. Moreover, the yield locus evolves smoothly and its convexity is ensured at each hardening<br />
stage.<br />
The rheological model serves as a guideline for construction <strong>of</strong> new constitutive relations. The<br />
kinematic assumptions, the ansatz for the free energy and for the yield function are motivated by<br />
the rheological model. Additionally to kinematic and distortional hardening, a nonlinear isotropic<br />
hardening is introduced as well. Normality flow rule is considered, and a rigorous pro<strong>of</strong> <strong>of</strong> ther-
126 Section 6: Material modelling in solid mechanics<br />
modynamic consistency is provided. Finally, the predictive capabilities <strong>of</strong> the resulting material<br />
model are verified using the experimental data for a very high work hardening annealed aluminum<br />
alloy 1100 Al.<br />
[1] A.V. Shutov, S. Panhans, R. Kreißig, A phenomenological model <strong>of</strong> finite strain viscoplasticity<br />
with distortional hardening, ZAMM, 8, 653 - 680.<br />
[2] A.V. Shutov, J. Ihlemann, A viscoplasticity model with an enhanced control <strong>of</strong> the yield<br />
surface distortion, Submitted to International Journal <strong>of</strong> Plasticity.<br />
Towards the simulation <strong>of</strong> Internal Traverse Grinding – from mesoscale modelling to<br />
process simulations<br />
Raphael Holtermann (TU Dortmund), Andreas Menzel (TU Dortmund / Lund University) Schedule<br />
The present work aims at the modelling and simulation <strong>of</strong> Internal Traverse Grinding <strong>of</strong> hardened<br />
100Cr6/AISI 52100 using electro plated cBN grinding wheels. We focus on the thermomechanical<br />
behaviour resulting from the interaction <strong>of</strong> tool and workpiece in the process zone on a mesoscale.<br />
Based on topology analyses <strong>of</strong> the grinding wheel surface, two-dimensional single- and multigrain<br />
representative numerical experiments are performed to investigate the resulting loaddisplacement-behaviour<br />
as well as the specific heat generation due to friction and plastic dissipation.<br />
A thermoelastic-viscoplastic constitutive model is used to capture thermal s<strong>of</strong>tening <strong>of</strong> the<br />
material taken into account. Based on previous work [1,2], an adaptive remeshing scheme which<br />
uses a combination <strong>of</strong> error estimation and indicator methods, is applied to overcome mesh dependence.<br />
In consequence, the formulation allows to resolve the complex deformation patterns<br />
and to predict a realistic thermomechanical state <strong>of</strong> the resulting workpiece surface [3].<br />
As a future goal, we aim at coupling the above cutting zone model to a process scale simulation<br />
to model the thermomechanical behaviour <strong>of</strong> the entire three-dimensional workpiece.<br />
[1] C. Hortig and B. Svendsen, Simulation <strong>of</strong> chip formation during high-speed cutting, J. Mat.<br />
Processing Technology 186, 66–76 (2007)<br />
[2] C. Hortig and B. Svendsen, Adaptive modeling and simulation <strong>of</strong> shear banding and high<br />
speed cutting, Proc. 10th ESAFORM Conference on Material Forming CP907, 721–726<br />
(2007)<br />
[3] D. Biermann, A. Menzel, T. Bartel, F. Höhne, R. Holtermann, R. Ostwald, B. Sieben, M.<br />
Tiffe, A. Zabel, Experimental and computational investigation <strong>of</strong> machining processes for<br />
functionally graded materials, Procedia Engineering, accepted for publication, 2011<br />
Multiscale crystal plasticity based on continuum theory <strong>of</strong> dislocation mechanics: an<br />
extension to ductile fracture.<br />
Mubeen Shahid, Klaus Hackl (<strong>Universität</strong> Bochum) Schedule<br />
The presentation focuses on the modelling <strong>of</strong> phenomena associated with plastic deformations<br />
in crystalline materials. The plastic deformation in crystalline materials strongly depends on<br />
aggregate behaviour <strong>of</strong> dislocations. However there is no universal constitutive frame-work which
Section 6: Material modelling in solid mechanics 127<br />
directly relates all the attributes <strong>of</strong> dislocations at microscale to the macroscale deformations,<br />
both qualitatively and quantitatively.<br />
First the macroscale constitutive model based on the continuum theory <strong>of</strong> dislocations [1,2]<br />
is discussed. The plastic deformation and crack growth during ductile fracture mutually effect<br />
each other, where dislocations’ movement shape the crack growth, and the latter effects the<br />
dislocations density [3]. We discuss the numerical implementation <strong>of</strong> the proposed crystal viscoelastoplasticity<br />
model coupled with modern dislocation measures [1,2] and present an example<br />
where the mechanisms <strong>of</strong> crystal plasticity are linked to the ductile fracture. The results focus<br />
the effect <strong>of</strong> severe plastic deformation on dislocations evolution and crack growth behaviour,<br />
following the approach <strong>of</strong> Cherepanov [3].<br />
[1] T. Hochrainer, M. Zaiser, P. Gumbsch, A three-dimensional continuum theory <strong>of</strong> dislocation<br />
systems: kinematics and mean-field formulation, Philosophical Magazine, 87:8-9 (2007),<br />
1261-1282.<br />
[2] S. Sandfeld, T. Hochrainer, P. Gumbsch, M. Zaiser, Numerical implementation <strong>of</strong> a 3D<br />
continuum theory <strong>of</strong> dislocation: dynamics and application to micro-bending, Philosophical<br />
Magazine, 90:27-28 (2010), 3697-3728.<br />
[3] G.P. Cherepanov et al., Dislocation generation and crack growth under monotonic loading,<br />
J. Appl. Phys., 78(10) (1995), 6249-6264.<br />
Multiscale modelling and simulation <strong>of</strong> micro machining <strong>of</strong> titan<br />
Richard Lohkamp, Ralf Müller (TU Kaiserslautern) Schedule<br />
The topology <strong>of</strong> micro machined surfaces depends strongly on the underlying heterogeneous microstructure<br />
<strong>of</strong> the material. The crystal structure influences the deformation and separation<br />
characteristics. In the case <strong>of</strong> α-titanium the deformation is dictated by the hcp crystal structure<br />
with its specific slip systems. In the crystal plastic deformation it is essential to take self and latent<br />
hardening into account. Furthermore to capture the rate dependent behavior a visco-plastic<br />
evolution law is used. This setting serves as a framework for more complex constitutive laws, such<br />
as the one given in [1].<br />
As a first attempt to model the cutting process, the fracture mechanisms in a crystalline αtitanium<br />
are analysed within the concept <strong>of</strong> configurational forces. To this end the theory <strong>of</strong><br />
configurational forces is presented for a standard dissipative medium and is specialized to the<br />
crystal plasticity setting. The numerical implementation <strong>of</strong> the material law and the configurational<br />
forces is done in a consistent way within the finite element method. The application <strong>of</strong><br />
configurational forces in the crystal plasticity setting is discussed and demonstrated by illustrative<br />
examples.<br />
S6.4: Polymers and Elastomers II Tue, 16:00–18:00<br />
Chair: Alexander Lion, Joachim Schmitt S1|01–A1<br />
How to approximate the inverse Langevin function?<br />
Mikhail Itskov, Roozbeh Dargazany, Karl Hörnes (RWTH Aachen) Schedule<br />
The inverse Langevin function directly results from the non-Gaussian theory <strong>of</strong> rubber elasticity<br />
as the chain force and represents an indispensable ingredient <strong>of</strong> full-network rubber elasticity models.<br />
However, the inverse Langevin function cannot be represented in a closed-form and requires
128 Section 6: Material modelling in solid mechanics<br />
an approximation as for example a Padé approximation. The Padé approximations can be given<br />
in a relatively simple form and are able to describe the asymptotic behavior <strong>of</strong> the inverse Langevin<br />
function in the vicinity <strong>of</strong> the maximum chain extensibility. Far away from the asymptotic<br />
area the approximation error can be, however, relatively large. In the present contribution we<br />
compare various Padé approximants with the Taylor power series representation <strong>of</strong> the inverse<br />
Langevin function. To this end, a simple recursive procedure calculating power series coefficients<br />
<strong>of</strong> the inverse function is proposed. The procedure can be applied to any function which can be<br />
expanded into Taylor series. Within the convergence radius the resulting series <strong>of</strong> the inversed<br />
Langevin function demonstrates better agreement with the analytical solution than the Padé approximations.<br />
Phenomenological modeling <strong>of</strong> a polymeric composite<br />
Sebastian Borsch, Albrecht Bertram (<strong>Universität</strong> Magdeburg) Schedule<br />
A composite material consisting <strong>of</strong> a polymeric matrix material and metallic filler particles is<br />
modeled in a phenomenological way. The isotropic viscoplastic constitutive model is formulated<br />
within the theory <strong>of</strong> finite deformations. The flow rule is a superposition <strong>of</strong> two terms. This<br />
approach enables us to simulate the strong backflow behavior during unloading, which can be<br />
observed in various polymeric materials. A quasi-static finite-element simulation has been performed<br />
to compare the model with cyclic tension tests as well as a relaxation test.<br />
Modelling <strong>of</strong> nanoindentation <strong>of</strong> polymers with effects <strong>of</strong> surface roughness and parameters<br />
identification<br />
Zhaoyu Chen, Stefan Diebels (<strong>Universität</strong> des Saarlandes) Schedule<br />
Since the nanoindentation testing technique can measure the properties <strong>of</strong> extremely small volumes<br />
with sub-m and sub-N resolution from the continuously sensed force-displacement curves,<br />
it also became one <strong>of</strong> the primary testing techniques for polymeric materials and biological tissues.<br />
The analysis <strong>of</strong> individual indentation tests using the conventionally applied Oliver & Pharr<br />
method has limitations to capture the hyperelastic and rate-dependent properties <strong>of</strong> polymers.<br />
Therefore, an inverse method with respect to the experimental testing, based on finite element<br />
simulation and numerical optimisation has been used and evolved. However, nanoindentation is<br />
composed <strong>of</strong> various error contributions, e. g. friction, adhesion, surface roughness and indentation<br />
process associated factors. These contributions forming the systematic errors between the<br />
numerical model and the experiments will <strong>of</strong>ten lead to large errors in the parameters identification.<br />
Therefore, basic investigations and quantification <strong>of</strong> these influences are indispensable to<br />
characterise the materials accurately from nanoindentation based on the inverse method.<br />
In the present contribution, the characterisation <strong>of</strong> polymers through nanoindentation with effects<br />
<strong>of</strong> the surface roughness based on inverse method will be investigated numerically. The boundary<br />
value problems <strong>of</strong> nanoindentation <strong>of</strong> polymers are modelled with the FE code ABAQUS R○ .<br />
In contrast to the traditional inverse method, virtual experimental data calculated by numerical<br />
simulations with chosen parameters replace the real experimental measurements. Such a procedure<br />
is called parameter re-identification. In this sense, the finite element code ABAQUS R○ is used as<br />
our virtual laboratory. The model parameters are identified using an evolution strategy based on<br />
the concept <strong>of</strong> numerical optimisation. The surface roughness effects are investigated numerically<br />
based on the approach utilizing the phenomenological concepts. The surface roughness is chosen<br />
to have a simple representation considering only one-level <strong>of</strong> roughness pr<strong>of</strong>ile described by a<br />
sine function. The influence <strong>of</strong> the surface roughness is quantified associated to the sine curve
Section 6: Material modelling in solid mechanics 129<br />
parameters as well as to the indentation parameters. Moreover, the real surface topography is<br />
characterised using multi-level <strong>of</strong> protuberance-on-protuberance pr<strong>of</strong>iles. The effects <strong>of</strong> the surface<br />
roughness are investigated with respect to the identified model parameters using a surface<br />
topography with one-level or multi-level pr<strong>of</strong>iles approximated by a sine function. The results are<br />
expected to <strong>of</strong>fer a deep insight into characterising the real surface roughness numerically.<br />
Material force computation for the thermo-mechanical response <strong>of</strong> dynamically loaded<br />
elastomers<br />
Ronny Behnke, Michael Kaliske (TU Dresden) Schedule<br />
Elastomers are widely used in our today’s life. The material is characterized by large deformability<br />
upon failure, elastic and time dependent as well as non-time dependent effects which can<br />
be also a function <strong>of</strong> temperature. In addition, cyclically loaded components show heat built-up<br />
which is due to dissipation. As a result, the temperature evolution <strong>of</strong> an elastomeric component<br />
can strongly influence the material properties and durability characteristics. Representing best<br />
the real thermo-mechanical behaviour <strong>of</strong> an elastomeric component in its design process is one<br />
motivation for the use <strong>of</strong> sophisticated, coupled material approaches within numerical simulations.<br />
In order to assess the durability characteristics, for example regarding crack propagation, the<br />
material forces (configurational forces) are one possible approach to be applied. In the present<br />
contribution, the implementation <strong>of</strong> material forces for a thermo-mechanically coupled material<br />
model including a continuum mechanical damage (CMD) approach is demonstrated in the context<br />
<strong>of</strong> the Finite Element Method (FEM). Special emphasis is given to material forces resulting<br />
from internal variables (viscosity and damage variables), temperature field evolution and dynamic<br />
loading. Using an example <strong>of</strong> an elastomeric component, for which the material model parameters<br />
have been previously identified by a uniaxial extension test, material forces are evaluated quantitatively.<br />
The influence <strong>of</strong> each contribution (internal variables, temperature field and dynamics)<br />
is illustrated and compared to the overall material force response.<br />
Single and multiscale aspects <strong>of</strong> the modeling <strong>of</strong> curing polymers<br />
Alexander Bartels ∗ , Sandra Klinge ∗ , Klaus Hackl ∗ , Paul Steinmann ∗∗ (<strong>Universität</strong> Bochum, <strong>Universität</strong><br />
Erlangen-Nürnberg) Schedule<br />
Within this presentation, the focus is placed on the simulation <strong>of</strong> the isochoric behavior <strong>of</strong> polymers<br />
during the curing process. To this end, a model based on the assumption for the free<br />
energy in the form <strong>of</strong> a convolution integral is applied. Since this allows the implementation <strong>of</strong><br />
the time dependent material parameters, the free energy is interpreted as the total-accumulated<br />
energy. Different from this, the strain energy is related to the current state <strong>of</strong> deformation and<br />
used to define the temporary stiffness. In order to avoid volume locking effects typical for isochoric<br />
materials, the free energy is furthermore split into a volumetric and a deviatoric part. A<br />
multifield description depending on the displacements, volume change and hydrostatic pressure<br />
is introduced as well. The model is implemented within a single- and multiscale FE program<br />
and used to simulate the behavior <strong>of</strong> homogeneous and microheterogeneous polymers. The main<br />
property <strong>of</strong> the multiscale concept used here is that the modeling <strong>of</strong> a heterogeneous body is<br />
performed by simultaneously solving two boundary value problems: one related to the behavior<br />
<strong>of</strong> the macroscopic body and the other one dealing with the analysis <strong>of</strong> the representative volume<br />
element.<br />
Influence <strong>of</strong> nano-particle interactions on the mechanical behavior <strong>of</strong> colloidal structures<br />
in polymeric solutions<br />
Roozbeh Dargazany, Ngoc Khiêm Vu , Mikhail Itskov (RWTH Aachen) Schedule
130 Section 6: Material modelling in solid mechanics<br />
Colloidal structures inside solutions are usually considered as rigid bodies or linear springs. However,<br />
recent experimental results show a strongly nonlinear mechanical response <strong>of</strong> large clusters.<br />
In this contribution, the nonlinear elastic behavior <strong>of</strong> the colloidal structures inside polymeric<br />
solutions is studied. So far, the influences <strong>of</strong> initial length and fractal dimension on the elastic response<br />
<strong>of</strong> colloidal structures have mostly been considered by scaling theory. Here, we additionally<br />
take into account a deformation induced evolution <strong>of</strong> the aggregate structure which is mainly influenced<br />
by inter-particle interactions. To this end, central and lateral (non-central) inter-particle<br />
forces are considered separately. Next, the directional stiffness <strong>of</strong> the colloidal structure is evaluated<br />
by using the concept <strong>of</strong> a backbone chain. The backbone chain is a unique path between two<br />
ends <strong>of</strong> the colloidal structure that carries the main portion <strong>of</strong> load. The mechanical response <strong>of</strong><br />
the backbone chain depends on aggregate geometry, deformation history and moreover, on the<br />
nature and the strength <strong>of</strong> the inter-particle interactions. The aggregate geometry is described by<br />
means <strong>of</strong> the angular averaging concept. The so-obtained model can further be generalized for all<br />
types <strong>of</strong> colloidal structures with central and lateral inter-particle forces.<br />
S6.5: Phase Transformations I Wed, 13:30–15:30<br />
Chair: Markus Lazar, Wolfgang Dreyer S1|01–A03<br />
A thermodynamically consistent framework for martensitic phase transformations<br />
interacting with plasticity<br />
Thorsten Bartel, Andreas Menzel (TU Dortmund) Schedule<br />
We propose constitutive relations for martensitic phase transformations at large strains which<br />
captures the interactions between phase transformations, plasticity and the local heating <strong>of</strong> the<br />
material due to the inelastic processes. For the kinematics <strong>of</strong> finite deformations we make use<br />
<strong>of</strong> logarithmic Hencky-strains. The total strain is additively decomposed into elastic, plastic and<br />
transformation related parts, where the latter quantities are motivated by crystallographic considerations.<br />
The thermodynamically consistent framework is based on a representative macroscopic<br />
energy density and an inelastic potential in terms <strong>of</strong> a dual dissipation functional. With these<br />
quantities at hand, thermodynamical driving forces as well as rate-independent evolution equations<br />
are derived in a canonical way. In this regard, the proposed model states an alternative to the<br />
models described in [1,2]. Referring to [3], the local heating <strong>of</strong> the material is realised by a consistently<br />
derived temperature evolution equation capturing the effect <strong>of</strong> self heating. The solution<br />
<strong>of</strong> the obtained local system <strong>of</strong> equations is challenging and demands a sophisticated algorithmic<br />
treatment. To this end, we present a scheme which avoids cumbersome and time-consuming active<br />
set searches by the use <strong>of</strong> Fischer-Burmeister NCP functions and furthermore prevents the<br />
occurence <strong>of</strong> redundant equations by a specific condensation strategy. The numerical examples<br />
emphasize the capabilities <strong>of</strong> the proposed model which is, among other aspects, exemplified by<br />
a transformation induced anisotropy. Furthermore, special attention is paid to the simulation <strong>of</strong><br />
the complex material behaviour <strong>of</strong>, e.g., TRIP-steels.<br />
[1] T. Bartel, A. Menzel, B. Svendsen, Thermodynamic and relaxation-based modeling <strong>of</strong> the<br />
interaction between martensitic phase transformations and plasticity, J. Mech. Phys. Sol.<br />
Vol. 59, 1004-1019, 2011,<br />
[2] R. Ostwald, T. Bartel, A. Menzel, A one-dimensional computational model for the interaction<br />
<strong>of</strong> phase-transformations and plasticity, Int. Journal <strong>of</strong> Structural Changes in Solids Vol. 3,<br />
63-82, 2011,<br />
[3] J. C. Simo, C. Miehe, Associative coupled thermoplasticity at finite strains: Formulation,
Section 6: Material modelling in solid mechanics 131<br />
numerical analysis and implementation, Comp. Meth. Appl. Mech. Engrg. Vol. 98, 41-104,<br />
1992<br />
Deformation induced martensite transformation in a cold-worked forming process <strong>of</strong><br />
austenitic stainless steel<br />
Tim Dally, Kerstin Weinberg (<strong>Universität</strong> Siegen) Schedule<br />
Within the last years the goal <strong>of</strong> industrial manufacturing processes - such as tube forming - has<br />
shifted towards an optimization <strong>of</strong> technological as well as mechanical properties <strong>of</strong> the manufactured<br />
structures. For example, during the forming procedure <strong>of</strong> sheets made <strong>of</strong> austenitic stainless<br />
steel X5CrNi18-10, the content <strong>of</strong> strain-induced martensite needs to be controlled. In order to<br />
achieve optimal structural properties <strong>of</strong> the manufactured tube with respect to very high-cycle<br />
fatigue (VHCF), a martensite ratio <strong>of</strong> approximately 25% needs to be obtained.<br />
On the basis <strong>of</strong> experimental investigations our contribution deals with the numerical simulation<br />
<strong>of</strong> the forming process with special consideration <strong>of</strong> the martensite ratio c as a function <strong>of</strong><br />
temperature and deformation field:<br />
c = c(T, ε p ).<br />
In particular, we study the interaction <strong>of</strong> processing temperature, friction, plastic deformation<br />
and stress state during forming. We will further present different approaches <strong>of</strong> modelling the<br />
martensite evolution as well as the extension <strong>of</strong> an existing martensite model on polyaxial states<br />
<strong>of</strong> stress and compare experimental results and numerical simulations for the modified model.<br />
Additionally a facility to calculate the hardening due to martensitic phase transformation will be<br />
presented.<br />
Finally, we will propose a strategy to control the martensite evolution during the tube-forming<br />
process that enables us to achieve the optimal c mentioned above.<br />
Micromechanical modeling <strong>of</strong> bainitic phase transformation<br />
A. Schneidt, R. Mahnken (<strong>Universität</strong> Paderborn), T. Antretter (Montanuniversität Leoben)<br />
Schedule<br />
We develop a micromechanical material model for phase transformation from austenite to bainite<br />
for a polycrystalline low alloys steel. In this material (e.g. 51CrV4) the phase changes from<br />
austenite to perlite-ferrite, bainite or martensite, respectively. This work is concerned with phase<br />
transformation between austenite and n-bainite variants in different orientated grains. Characteristic<br />
<strong>of</strong> bainite are the combination <strong>of</strong> time-dependent transformation kinetics and lattice shearing<br />
in the microstructure. These effects are considered on the microscale and by means <strong>of</strong> homogenisation<br />
scale in the polycrystalline macroscale with stochastically orientated grains. Furthermore, the<br />
numerical implementation <strong>of</strong> our model with a Newton projection algorithm into a finite-element<br />
program is presented, based on the algorithm in [1].<br />
[1] R. Mahnken and S. Wilmanns, A projected Newton algorithm for simulation <strong>of</strong> multivariant<br />
textured polycrystalline shape memory alloys. Computational Materials Science 50,<br />
25352548, 2011.
132 Section 6: Material modelling in solid mechanics<br />
Effects <strong>of</strong> heat treatment on phase transformation in powder metallurgical multifunctional<br />
coating<br />
Reza Kebriaei, Jan Frischkorn, Stefanie Reese (RWTH Aachen) Schedule<br />
Heat treatment is an indispensable part <strong>of</strong> the manufacturing <strong>of</strong> metallic products, especially in<br />
powder coating process. It provides an efficient way to manipulate the properties <strong>of</strong> the metal as<br />
e.g. hardness, yield stress and tensile stress by controlling the rate <strong>of</strong> diffusion and the rate <strong>of</strong><br />
cooling within the microstructure.<br />
The process-integrated powder coating by radial axial rolling <strong>of</strong> rings is a new hybrid production<br />
technique which is introduced in [1]. It takes advantage <strong>of</strong> the high temperatures and high<br />
forces <strong>of</strong> the ring rolling process not only to increase the rings diameter, but also to integrate<br />
the application and compaction <strong>of</strong> powder metallurgical multi-functional coatings to the solid<br />
substrate rings within the same process [2]. The applied temperatures in hot rolling are within<br />
the range <strong>of</strong> austenitizing temperatures for the investigated steels. Therefore, controlled cooling<br />
can be conducted directly from process heat subsequent to the deformation process.<br />
The talk is concerned with the finite element (FE) simulation <strong>of</strong> the process-integrated powder<br />
coating by radial axial rolling <strong>of</strong> rings and the integration <strong>of</strong> heat treatment <strong>of</strong> the rolled ring<br />
into the subsequent cooling process. Finally parameter studies are performed to analyse the<br />
temperature pr<strong>of</strong>ile and phase transformation in the rings cross-section.<br />
[1] J. Frischkorn, S. Reese, Modelling and Simulation <strong>of</strong> Process-integrated Powder Coating by<br />
Radial Axial Rolling <strong>of</strong> Rings, Archive <strong>of</strong> Applied Mechanics 81 (2011)<br />
[2] R. Kebriaei, J. Frischkorn, S. Reese, Influence <strong>of</strong> Geometric Parameters on Residual Porosity<br />
in Process-integrated Powder Coating by Radial Axial Rolling <strong>of</strong> Rings, Steel Research<br />
International 163 (2011)<br />
Simulation <strong>of</strong> phase-transformations based on numerical minimization <strong>of</strong> intersecting<br />
Gibbs energy potentials<br />
Richard Ostwald, Thorsten Bartel (TU Dortmund), Andreas Menzel (U Dortmund / Lund University)<br />
Schedule<br />
We present a novel approach for the simulation <strong>of</strong> solid to solid phase-transformations in polycrystalline<br />
materials. To facilitate the utilization <strong>of</strong> a non-affine micro-sphere formulation with<br />
volumetric-deviatoric split, we introduce Helmholtz free energy functions depending on volumetric<br />
and deviatoric strain measures for the underlying scalar-valued phase-transformation model.<br />
As an extension <strong>of</strong> affine micro-sphere models [3], the non-affine micro-sphere formulation with<br />
volumetric-deviatoric split allows to capture different Young’s moduli and Poisson’s ratios on the<br />
macro-scale [1]. As a consequence, the temperature-dependent free energy assigned to each individual<br />
phase takes the form <strong>of</strong> an elliptic paraboloid in volumetric-deviatoric strain space, where<br />
the energy landscape <strong>of</strong> the overall material is obtained from the contributions <strong>of</strong> the individual<br />
constituents.<br />
For the evolution <strong>of</strong> volume fractions, we use an approach based on statistical physics—taking<br />
into account actual Gibbs energy barriers and transformation probabilities [2]. The computation<br />
<strong>of</strong> individual energy barriers between the phases considered is enabled by numerical minimization<br />
<strong>of</strong> parametric intersection curves <strong>of</strong> elliptic Gibbs energy paraboloids. The framework provided<br />
facilitates to take into account an arbitrary number <strong>of</strong> solid phases <strong>of</strong> the underlying material,<br />
though we restrict ourselves to the simulation <strong>of</strong> three phases, namely an austenitic parent phase<br />
and a martensitic tension and compression phase. It is shown that the model presented nicely
Section 6: Material modelling in solid mechanics 133<br />
reflects the temperature-dependent effects <strong>of</strong> pseudo-elasticity and pseudo-plasticity, and thus<br />
captures experimentally observed behaviour at different temperatures.<br />
[1] I. Carol and Z. Bažant, Damage and plasticity in microplane theory, Int. J. Sol. Struct. 34,<br />
3807–3835 (1997)<br />
[2] S. Govindjee and G.J. Hall, A computational model for shape memory alloys, Int. J. Sol.<br />
Struct. 37, 735–760 (2000)<br />
[3] R. Ostwald, T. Bartel and A. Menzel, A computational micro-sphere model applied to the<br />
simulation <strong>of</strong> phase-transformations, J. Appl. Math. Mech. 90(7-8), 605–622 (2010)<br />
S6.6: Elasticity, Viscoelasticity, -plasticity I Wed, 13:30–15:30<br />
Chair: Merab Svanadze, Daniel Balzani S1|01–A1<br />
Thermoviscoplasticity deduced from enhanced rheological models<br />
Christoph Bröcker, Anton Matzenmiller (<strong>Universität</strong> Kassel) Schedule<br />
In the concept <strong>of</strong> rheological models, basic elements like springs (ideal elastic), dashpots (ideal<br />
viscous) or friction elements (ideal plastic) are assembed to networks for representing complex<br />
material behaviour [1]. In case <strong>of</strong> viscoelastic material models, the phenomenological constitutive<br />
equations are usually deduced directly from a rheological network. However, in the case <strong>of</strong> elastoplasticity,<br />
the rheological models are <strong>of</strong>ten used only to visualise the fundamental structure <strong>of</strong><br />
the related material model.<br />
In the presentation, a new ideal body is defined for isotropic hardening besides minor modifications<br />
<strong>of</strong> some well–known basic elements from the literature [2, 3]. Hence, a rheological model <strong>of</strong><br />
thermoviscoplasticity may be assembled with linear isotropic and kinematic hardening and nonlinear<br />
strain rate sensitivity. The related constitutive equations including the yield function and the<br />
flow rule are directly deduced from the kinematics and the stress equilibrium <strong>of</strong> the rheological<br />
network and results in a well–known model. By evaluating the dissipation inequality, the heat<br />
conduction equation is obtained with the dissipative power term, driven by plastic deformations.<br />
Moreover, nonlinear isotropic and kinematic hardening as well as an improved description<br />
<strong>of</strong> energy storage and dissipation are accomplished by introducing several additional dissipative<br />
strain elements into the viscoplastic arrangement <strong>of</strong> the rheological model [see also 4], which<br />
corresponds to a generalization <strong>of</strong> an ideal body already used in [2, 3]. Again, the constitutive<br />
equations may be deduced from the rheological network, its kinematics, and the stress equilibrium.<br />
For that purpose, however, the dissipation inequality has to be utilized.<br />
[1] M. Reiner, Rheologie in elementarer Darstellung, Carl Hanser Verlag, 1969.<br />
[2] A. Krawietz, Materialtheorie, Springer, 1986.<br />
[3] A. Lion, Constitutive modelling in finite thermoviscoplasticity: a physical approach based on<br />
nonlinear rheological models, Int. J. Plast. 16 (2000), 469–494.<br />
[4] A. Matzenmiller, C. Bröcker, Modelling and simulation <strong>of</strong> coupled thermoplastic and thermoviscous<br />
structuring and forming processes, In: Maier et al. (eds.): Functionally graded<br />
materials in industrial mass production, Verlag Wissenschaftliche Skripten, Auerbach, 2009,<br />
235–250.
134 Section 6: Material modelling in solid mechanics<br />
Steady vibrations problems in the theory <strong>of</strong> viscoelasticity for Kelvin-Voigt materials<br />
with voids<br />
Maia M. Svanadze (<strong>Universität</strong> Göttingen) Schedule<br />
Viscoelastic materials play an important role in many branches <strong>of</strong> engineering, technology and<br />
biomechanics. The modern theories <strong>of</strong> viscoelasticity and thermoviscoelasticity for materials with<br />
microstructure have been a subject <strong>of</strong> intensive study in recent years. Recently, the theory <strong>of</strong><br />
thermoviscoelastic materials with voids is constructed by Iesan (2011).<br />
In this paper the linear theory <strong>of</strong> viscoelasticity for Kelvin-Voigt materials with voids is considered<br />
and the basic internal and external boundary value problems <strong>of</strong> steady vibrations are investigated.<br />
The formulae <strong>of</strong> integral representations <strong>of</strong> regular vectors are obtained. The single-layer,<br />
double-layer and volume potentials are constructed and their basic properties are established.<br />
The uniqueness and existence <strong>of</strong> regular solutions <strong>of</strong> the boundary value problems are proved by<br />
means <strong>of</strong> the potential method.<br />
Modelling <strong>of</strong> predeformation- and frequency-dependent material behavior <strong>of</strong> filled<br />
rubber under large predeformations superimposed with harmonic deformations <strong>of</strong><br />
small amplitudes<br />
D. Wollscheid, A. Lion (<strong>Universität</strong> der Bundeswehr München) Schedule<br />
Viscoelastic materials show a frequency- and predeformation-dependent behavior under loadings<br />
that consist <strong>of</strong> large predeformations with superimposed harmonic deformations <strong>of</strong> small amplitudes.<br />
In order to consider this materialbehavior, some static and dynamic experiments are<br />
developed. Based on Haupt & Lion [1] and Lion, Retka & Rendek [2] we introduce a recently<br />
developed constitutive approach <strong>of</strong> finite viscoelasticity in the frequency domain that is able to<br />
describe the frequency- and predeformation-dependent materialbehavior with respect to storageand<br />
loss-modulus. The constitutive equations are evaluated in the frequency domain and geometrically<br />
linearized in the neighbourhood <strong>of</strong> the predeformation. Furthermore a formulation for<br />
incompressible material behavior is introduced and the corresponding dynamic modulus tensors<br />
are derived. Besides constitutive modelling and experiments, parameter identification and some<br />
numerical simulations are presented.<br />
[1] P. Haupt, A. Lion, On finite linear viscoelasticity <strong>of</strong> incompressible isotropic materials, Acta<br />
Mechanica 159 (2002), 87 – 124.<br />
[2] A. Lion, J.Retka, M.Rendek On the calculation <strong>of</strong> predeformation-dependent dynamic modulus<br />
tensors in finite nonlinear viscoelasticity, Mechanics Research Communications 36<br />
(2009), 653 – 658.<br />
A multi-scale modelling approach for bituminous asphalt<br />
Thorsten Schüler, Ralf Jänicke, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
Bituminous asphalt is a standard material e.g. in road constructions. However, the term asphalt<br />
involves an extremly broad class <strong>of</strong> complex multi-scale and multi-phase materials. Typically,<br />
asphalt consists <strong>of</strong> a mineral filler (e.g. crushed rock), a bituminous binding agent (possibly including<br />
further additive compounds) and pores. The various constituents are to be adapted for<br />
the particular application.
Section 6: Material modelling in solid mechanics 135<br />
Nowadays, requirements on noise reduction <strong>of</strong> road constructions become more and more important.<br />
In our ongoing research activities, we focus on the solid-borne acoustic properties <strong>of</strong> the<br />
asphalt cover layer, i.e. the top layer <strong>of</strong> the entire asphalt-construction. In order to predict the<br />
macro-scale effective material properties <strong>of</strong> asphalt we apply a numerical homogenisation scheme<br />
based on volume averaging techniques. The main advandtage <strong>of</strong> this numerical approach is, that<br />
the effective material properties can be determined in knowledge <strong>of</strong> the micro-scale properties.<br />
Hence, the first step towards an overall model for bituminous asphalt is the quantification <strong>of</strong><br />
the micro-scale mechanical properties. Against the background <strong>of</strong> solid-borne acoustical properties<br />
we restrict ourselves to a geometrically linear description involving only small deformations<br />
on both, macro- and micro-scale. Doing so, the linear-elastic properties <strong>of</strong> the stiff, granular filler<br />
can be adopted from relevant literature. The viscoelastic behaviour <strong>of</strong> the bituminous phase is<br />
characterized by rheological experiments (dynamic shear rheometer with plate-plate geometry).<br />
The numerical implementation on the micro-scale is realized using a generalized Zener model (3d).<br />
Making use <strong>of</strong> the numerical homogenization approach, the effective viscoelastic properties on<br />
the macro-scale are investigated within transient experiments (relaxation/creep test). In particular<br />
we are interested in the particular relaxation mechanisms and the related characteristic frequencies<br />
to be observed on the macro-scale. The influence <strong>of</strong> micro-scale boundary conditions will be<br />
taken into account. In order to study the interaction between micro-constituents as well as their<br />
geometrical morphology on the one hand and the effective viscoelastic properties on the other,<br />
we introduce artificially produced periodic unit cells based on simplified geometries with varying<br />
volume and surface fractions <strong>of</strong> the mineral filler.<br />
Jumps <strong>of</strong> the critical tracking loadings for viscoelastic beams with vanisihing internal<br />
viscosity<br />
S.A.Agafonov (Moscow State Technical University), D.V.Georgievskii (Moscow State University)<br />
Schedule<br />
Transverse vibrations <strong>of</strong> a viscoelastic beam under action <strong>of</strong> a tracking loading are considered.<br />
The constitutive relation represents the following non-linear connection <strong>of</strong> stress σ(t), strain ε(t)<br />
and strain rate ˙ε(t):<br />
σ = Eε +<br />
where E is the Young modulus, k (n)<br />
i<br />
N�<br />
n�<br />
n=1 i=1<br />
k (n)<br />
i ε2(n−i) ˙ε 2i−1 , N ≥ 1<br />
> 0 are the coefficients <strong>of</strong> internal viscosity.<br />
Analytical and numerical investigation <strong>of</strong> dynamic stability in case N = 3, k (1)<br />
1 = 0, k (2)<br />
1 = 0,<br />
k (1)<br />
2 = 0 shows that if k (3)<br />
α → 0 (k (3)<br />
β<br />
= 0, k(3)<br />
γ = 0; (α, β, γ) may be some permutation <strong>of</strong> (1, 2, 3))<br />
then three critical values <strong>of</strong> tracking loading corresponding to each nonzero coefficient <strong>of</strong> viscosity<br />
k (3)<br />
α less than the value for elastic system by a finite quantity.<br />
Numerical modeling <strong>of</strong> a non-linear viscous flow in order to determine how parameters<br />
in constitutive relations influence the entropy production<br />
Wolfgang H. Müller, B. Emek Abali (TU Berlin) Schedule<br />
Some rheological materials like melting polymers, cosmetic creams, ketchup, toothpaste can be<br />
modeled as non-Newtonian fluids by using a non-linear constitutive relation. Flow <strong>of</strong> this kind<br />
<strong>of</strong> amorphous matter can be considered as a thermodynamic process, and a solution <strong>of</strong> pressure,<br />
velocity and temperature fields describe it fully. Since flow processes are generally irreversible,<br />
entropy is produced leading to dissipation in the system. This energy loss can be measured
136 Section 6: Material modelling in solid mechanics<br />
indirectly in a cone/plate viscometer which is used to determine viscosity <strong>of</strong> a Bingham fluid.<br />
While dissipation is a measurable quantity we want to be able to calculate it. Thus the goal <strong>of</strong><br />
this work is to explain how to calculate entropy production using balance equations in a spatial<br />
frame.<br />
Starting from balance <strong>of</strong> mass, linear momentum, internal energy and employing method<br />
<strong>of</strong> weighted residuals, we get a non-linear coupled set <strong>of</strong> partial differential equations in space<br />
and time. A space discretization in finite elements method and a time discretization in finite<br />
difference method leads to an approximation after a successful linearization. We achieve to solve<br />
the problem without any stabilization or usage <strong>of</strong> specific type <strong>of</strong> elements and show here the<br />
entropy production and its variation subject to material parameters for the sake <strong>of</strong> a better<br />
intuitive understanding <strong>of</strong> dissipation. This may lead to an inverse problem where the calculated<br />
dissipation is measured and material parameters are determined out <strong>of</strong> it, which is left to future<br />
research.<br />
S6.7: Phase Transformations II Wed, 16:00–18:00<br />
Chair: Wolfgang Dreyer S1|01–A03<br />
Nonsingular Dislocation Loops in Gradient Elasticity<br />
Markus Lazar (TU <strong>Darmstadt</strong>) Schedule<br />
This work studies the fundamental problem <strong>of</strong> nonsingular dislocations in the framework <strong>of</strong> the<br />
theory <strong>of</strong> gradient elasticity. A general theory <strong>of</strong> nonsingular dislocations is developed for linearly<br />
elastic, infinitely extended, homogeneous, isotropic media. Using gradient elasticity, we give the<br />
nonsingular fields produced by arbitrary dislocation loops. We present the ‘modified’ Mura, Peach-<br />
Koehler and Burgers formulae in the framework <strong>of</strong> gradient elasticity theory. These formulae are<br />
given in terms <strong>of</strong> an elementary function, which regularizes the classical expressions, obtained<br />
from the Green tensor <strong>of</strong> generalized Navier equations. Using the mathematical method <strong>of</strong> Green’s<br />
functions and the Fourier transform, we found exact, analytical and nonsingular solutions. The<br />
obtained dislocation fields are nonsingular due to the regularization <strong>of</strong> the classical singular fields.<br />
On a paradox within the phase field modeling <strong>of</strong> storage systems and its resolution<br />
Clemens Guhlke, Wolfgang Dreyer (WIAS Berlin) Schedule<br />
We study two import storage problems: The storage <strong>of</strong> lithium in an electrode <strong>of</strong> a lithium-ion<br />
battery and the storage <strong>of</strong> hydrogen in hydrides.<br />
When foreign atoms are reversibly stored in a crystal, there may be a regime where two coexisting<br />
phases with low and high concentration <strong>of</strong> the stored atoms occur. Furthermore hysteretic<br />
behavior can be observed, i.e. the processes<strong>of</strong> loading and unloading follow different paths.<br />
We apply a viscous Cahn-Hilliard model with mechanical coupling to calculate the voltagecharge<br />
diagram <strong>of</strong> the battery, respectively the pressure-charge diagram <strong>of</strong> a hydrogen system.<br />
The diagrams exhibit phase transition and hysteresis. However, we show that the model can only<br />
describe the observed phenomena for fast but nor for slow loading.<br />
We relate the reason for failure to the microstructure <strong>of</strong> modern storage systems. In fact these<br />
consist <strong>of</strong> an ensemble <strong>of</strong> nano-sized interconnected storage particle. Each particle is described by<br />
a non-monotone chemical potential function but on the time scale <strong>of</strong> slow loading <strong>of</strong> the ensemble,<br />
the coexisting phases are unstable within an individual particle and cannot be observed on the<br />
time scale <strong>of</strong> the loading.<br />
In the slow loading regime, the occurence <strong>of</strong> two coexisting phases phases is a many-particle<br />
effect <strong>of</strong> the ensemble. The nucleation and evolution <strong>of</strong> the phases is embodied by a nonlocal
Section 6: Material modelling in solid mechanics 137<br />
conservation law <strong>of</strong> Fokker-Planck type.<br />
Numerical Simulation <strong>of</strong> Coarsening in Metallic Alloys<br />
Uli Sack, Carsten Gräser, Ralf Kornhuber (FU Berlin) Schedule<br />
Phase separation phenomena in alloys, such as spinodal decomposition and Ostwald ripening<br />
can be described by phasefield models <strong>of</strong> Cahn-Hilliard-type. Realistic models based on thermodynamically<br />
correct logarithmic free energies contain highly nonlinear and singular terms as<br />
well as drastically varying length scales (cf. [1]). We present a globally convergent nonsmooth<br />
Schur-Newton Multigrid method for vector-valued Cahn-Hilliard-type equations ([2, 3]) and a<br />
numerical study <strong>of</strong> coarsening in a binary eutectic AgCu alloy taking into account elastic effects.<br />
Vector-valued Cahn-Hilliard computations open the perspective to multicomponent simulations.<br />
[1] W. Dreyer, W.H. Müller, F. Duderstadt and T. Böhme, “Higher Gradient Theory <strong>of</strong> Mixtures”,<br />
WIAS-Preprint No 1286 (2008)<br />
[2] C. Gräser and R. Kornhuber, “Nonsmooth Newton Methods for Set-valued Saddle Point<br />
Problems”, SIAM J. Numer. Anal. (2009) 47 (2)<br />
[3] C. Gräser, R. Kornhuber, “Schur-Newton Multigrid Methods for Vector-Valued Cahn–Hilliard<br />
Equations”, in prep<br />
A Phase Field Model for Martensitc Transformations<br />
Regina Schmitt, Ralf Müller, Charlotte Kuhn (TU Kaiserslautern) Schedule<br />
Considering the microscopic level <strong>of</strong> steel, there are different structures with different mechanical<br />
properties. Under mechanical deformation the metastable austenitic face-centered cubic phase<br />
transforms into the tetragonal martensitic phase at which transformation induced eigenstrain<br />
arises. On the other hand, the mircostructure affects the macroscopic mechanical behavior <strong>of</strong><br />
the specimen. In order to take the complex interactions into account, a phase field model for<br />
martensitic transformation is developed. Within the phase field approach, an order parameter<br />
is introduced to indicate different material phases. Its time derivative is assumed to follow the<br />
time-dependent Ginzburg-Landau equation. The coupled field equations are solved using finite<br />
elements together with an implicit time integration scheme. With the aid <strong>of</strong> this model, the effects<br />
<strong>of</strong> the elastic strain minimization on the formation <strong>of</strong> microstructure can be studied so that the<br />
evolution <strong>of</strong> the martensitic phase is predictable. The applicability <strong>of</strong> the model is illustrated<br />
through different numerical examples.<br />
Investigation <strong>of</strong> the strain localization behavior with application <strong>of</strong> the phase transition<br />
approach<br />
M. Ievdokymov, H. Altenbach, V.A. Eremeyev (<strong>Universität</strong> Magdeburg) Schedule<br />
Metal foams found recently many applications in civil, airspace and mechanical engineering. In<br />
particular, foams have a good energy absorption property. This property relates to the phenomenon<br />
<strong>of</strong> localization <strong>of</strong> strains in foams under loading. In porous materials the localization <strong>of</strong><br />
strains leads to change <strong>of</strong> mass density <strong>of</strong> material and appearance <strong>of</strong> areas with low and high<br />
densities separated by sharp interface. This behavior is similar to the phase transitions in solids<br />
with sharp interfaces.<br />
In this paper we use the methods <strong>of</strong> modelling <strong>of</strong> phase transitions in solids to the description <strong>of</strong><br />
strain localization in foams. We assume that the foam consist <strong>of</strong> two phases with different densities
138 Section 6: Material modelling in solid mechanics<br />
and mechanical properties. The results <strong>of</strong> modelling <strong>of</strong> one- and two-dimensional problems are<br />
discussed. The calculations are performed by Abaqus and script language Python.<br />
S6.8: Elasticity, Viscoelasticity, -plasticity II Wed, 16:00–18:00<br />
Chair: Ismail Caylak S1|01–A1<br />
A New Continuum Approach to the Coupling <strong>of</strong> Shear Yielding and Crazing with<br />
Fracture in Glassy Polymers<br />
Lisa Schänzel, Christian Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
Over the past decades, considerable effort was made to develop constitutive models that account<br />
for finite viscoplasticity and failure in glassy polymers. Recently, we developed a new model<br />
<strong>of</strong> ductile thermoviscoplasticity <strong>of</strong> glassy polymers in the logarithmic strain space [1]. However,<br />
depending on thermal and loading rate conditions to which the material is subjected, the response<br />
might change from ductile to brittle. This brittle response is characterized by inelastically deformed<br />
zones, so-called crazes, having the thickness <strong>of</strong> micrometers and spanning at some fractions <strong>of</strong><br />
a millimeter [2]. The crazing is associated with considerable dilatational plasticity, containing a<br />
dense array <strong>of</strong> fibrils interspersed with elongated voids. The shear yielding and crazing are not<br />
completely independent excluding each other. In this lecture, we outline an extension <strong>of</strong> the ductile<br />
plasticity model [1] towards the description <strong>of</strong> (i) volumetric directional plasticity effect due to<br />
crazing and (ii) the modeling <strong>of</strong> the local failure due to fracture. To this end, the first extension<br />
accounts for a (i) dilatational plastic deformation mechanism in the direction <strong>of</strong> the maximum<br />
principle tensile stress. The ultimate amount <strong>of</strong> this volumetric plastic craze strain is bounded<br />
by a limiting value, where failure occurs. Then, in a second step, the (ii) modeling <strong>of</strong> subsequent<br />
failure mechanisms is realized by the introduction <strong>of</strong> a fracture phase field, characterizing via an<br />
auxiliary variable the crack topology. Here, we adopt structures <strong>of</strong> a recently developed continuum<br />
phase field model <strong>of</strong> fracture in brittle solids [3], and modify it for a fracture driving term related<br />
to the volumetric plastic deformation <strong>of</strong> the crazes. We demonstrate the performance <strong>of</strong> proposed<br />
formulation by means <strong>of</strong> representative boundary value problems.<br />
[1] Miehe, C.; Mendez, J.; Göktepe, S.; Schänzel, L. [2011]: Coupled thermoviscoplasticity <strong>of</strong><br />
glassy polymers in the logarithmic strain space based on the free volume theory. International<br />
Journal <strong>of</strong> Solids and Structures, 48: 1799–1817.<br />
[2] Kramer, E. J.[1983]:Microscopic and Molecular Fundamentals <strong>of</strong> Crazing. Advances in Polymer<br />
Science, 52/53: 1–56.<br />
[3] Miehe, C; H<strong>of</strong>acker, M.; Welschinger, F. [2010]: A phase field model for rate-independent<br />
crack propagation: Robust algorithmic implementation based on operator splits. Computer<br />
Methods in Applied Mechanics and Engineering, 199: 2765-2778.<br />
Anisotropic finite strain hyperelasticity based on the multiplicative decomposition <strong>of</strong><br />
the deformation gradient<br />
Raad Al-Kinani, Kaveh Talebam, Stefan Hartmann (TU Clausthal) Schedule<br />
Frequently, the case <strong>of</strong> finite strain anisotropy, particularly, the case <strong>of</strong> transversal isotropy, is<br />
applied to biological applications or to model fiber-reinforced composite materials. In this article<br />
the multiplicative decomposition <strong>of</strong> the deformation gradient into one part constrained in the direction<br />
<strong>of</strong> the axis <strong>of</strong> anisotropy and one part describing the remaining deformation is proposed.
Section 6: Material modelling in solid mechanics 139<br />
Accordingly, a form <strong>of</strong> additively decomposed strain-energy function is proposed. This leads to a<br />
clear assignment <strong>of</strong> deformation and stress states in the direction <strong>of</strong> anisotropy and the remaining<br />
part. The decomposition <strong>of</strong> the case <strong>of</strong> transversal isotropy is explained. The behavior <strong>of</strong> the<br />
model is investigated at different simple analytical examples, such as uniaxial tension along and<br />
perpendicular to the axis <strong>of</strong> anisotropy, and simple shear. In addition, the model is also studied for<br />
the case <strong>of</strong> a thick-walled tube under internal pressure, where a second order ordinary differential<br />
equation (two-point boundary-value problem) is obtained.<br />
Experimental characterization <strong>of</strong> the viscoelastic behaviour <strong>of</strong> discontinuous glass<br />
fibre reinforced thermoplastics<br />
B. Brylka, T. Böhlke (KIT) Schedule<br />
In automotive applications short and long glass fibre reinforced thermoplastics are commonly used<br />
for non-structural parts. Due the versatile possibilities <strong>of</strong> manufacturing, forming, joining and<br />
recycling, thermoplastic matrix based composites are increasingly used also for semi-structural<br />
parts. Thermoplastics like e.g. polypropylene show a high temperature and strain-rate dependency,<br />
especially in the temperature and strain-rate ranges which are relevant for automotive<br />
applications. Additionally, the non-linear influence <strong>of</strong> the viscoelastic behaviour <strong>of</strong> the matrix<br />
material on the effective material behaviour <strong>of</strong> the composite is <strong>of</strong> high interest.<br />
The dynamic mechanical analysis (DMA) technique is an effective method to investigate the<br />
elastic and viscoelastic stiffness response <strong>of</strong> materials under cyclic loading. After a short introduction<br />
into the DMA technique, experimental results for a polypropylene and polypropylene based<br />
composite material will be presented. The composite under consideration is an discontinuous glass<br />
fibre reinforced polypropylene. In the manufacturing process, which is commonly compression or<br />
injection moulding, the flow <strong>of</strong> the mould induces an heterogeneous and anisotropic distribution<br />
<strong>of</strong> fibre orientations. Therefore, the effective properties as well as the temperature and strain-rate<br />
dependency has been investigated taking into account an anisotropic material behaviour. The<br />
comparison <strong>of</strong> the elastic and viscoelastic material response <strong>of</strong> the matrix and the composite will<br />
be discussed in detail. Additionally, a parameter identification for common viscoelastic material<br />
models will be presented.<br />
[1] Middendorf, P.: Viskoelastisches Verhalten von Polymersystemen, Fortschritt-Berichte VDI,<br />
Reihe 5, VDI Verlag (2002).<br />
[2] Deng, S., Hou, M., Ye, L.: Temperature-dependent elastic moduli <strong>of</strong> epoxies measured by<br />
DMA and their correlations to mechanical testing data, Polym. Test., 26, 803-813 (2007).<br />
[3] Schledjewski, R., Karger-Kocsis, J.: Dynamic mechanical analysis <strong>of</strong> glass mat-reinforced<br />
polypropylene (GMT-PP), J. Thermoplast. Compos., 7, 270-277 (1994).<br />
A solid-shell finite element for fibre reinforced composites<br />
J.-W. Simon, B. Stier, S. Reese (RWTH Aachen) Schedule<br />
Fibre reinforced composites are typically characterized by high Young’s modulus at low density,<br />
which makes them very attractive for lightweight constructions. The fibre composites considered<br />
here consist <strong>of</strong> several layers, each <strong>of</strong> which is composed <strong>of</strong> a woven fabric embedded in a matrix<br />
material. This structure makes the constitutive behavior <strong>of</strong> fibre composites anisotropic. Moreover,<br />
it is generally highly nonlinear, and the materials’ response in tension and compression can
140 Section 6: Material modelling in solid mechanics<br />
differ significantly. In order to describe this rather complex behavior, we use a modification <strong>of</strong><br />
a micromechanically motivated model proposed by Reese [1]. Therein, an anisotropic model has<br />
been presented for the hyperelastic material behavior <strong>of</strong> membranes reinforced with roven-woven<br />
fibres, which is particularly suitable for the present fibre reinforced composites.<br />
The use <strong>of</strong> a fully three-dimensional material model strongly suggests using solid elements.<br />
On the other hand, fibre composites are mostly applied in thin shell-like structures, where shell<br />
elements should usually be preferred. Therefore, we use a solid-shell element presented by Schwarze<br />
and Reese [2] which combines the advantages <strong>of</strong> both solid elements and shell elements at the<br />
same time. This element allows for displaying realistically the three-dimensional geometry while<br />
still providing the suitable shape for thin structures.<br />
In addition, the present solid-shell formulation utilizes a reduced integration scheme within the<br />
shell plane using one integration point, whereas a full integration is used in thickness direction.<br />
Thus, an arbitrary number <strong>of</strong> integration points can be chosen over the shell thickness. Thereby,<br />
different fibre orientations <strong>of</strong> the layers can be taken into account easily, since the material<br />
parameters can be defined for each integration point separately.<br />
Moreover, the proposed solid-shell formulation removes all potential locking phenomena. In<br />
particular, volumetric locking in case <strong>of</strong> (nearly) incompressible materials as well as Poisson<br />
thickness locking in bending problems <strong>of</strong> shell-like structures are eliminated by use <strong>of</strong> the enhanced<br />
assumed strain (EAS) concept. In addition, to cure the transverse shear locking which is present<br />
in standard eight-node hexahedral elements, the assumed natural strain (ANS) method is applied.<br />
[1] S. Reese. A micromechanically motivated material model for the thermo-viscoelastic material<br />
behaviour <strong>of</strong> rubber-like polymers, Int J Plast, 19, 909–940, 2003.<br />
[2] M. Schwarze, S. Reese. A reduced integration solid-shell finite element based on the EAS and<br />
the ANS concept - large deformation problems, Int J Numer Methods Engng, 85, 289–329,<br />
2011.<br />
On consistent tangent operator derivation and comparative study <strong>of</strong> rubber-like material<br />
models at finite strains<br />
Mokarram Hossain, Paul Steinmann (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
The overall micro-structure <strong>of</strong> rubber-like materials can be idealized by chain-like macromolecules<br />
which are connected to each other at certain points via entanglements or cross-links. Such<br />
special structure leads to a completely random three-dimensional network [2,3]. To model the<br />
mechanical behaviour <strong>of</strong> such randomly-oriented micro-structure, several phenomenological and<br />
micro-mechanically motivated network models for nearly incompressible hyperelastic polymeric<br />
materials have been proposed in the literature. To implement these models for polymeric material<br />
(undoubtedly with widespread engineering applications) in finite element method, one would<br />
require two important ingredients, e.g. the stress tensor and the consistent fourth-order tangent<br />
operator where the latter is the result <strong>of</strong> linearization <strong>of</strong> the former.<br />
In this contribution, an extensive overview on several hyperelastic rubber-like material models<br />
has been presented. Special focus is given particularly to derive the accurate stress tensors and<br />
tangent operators which yield quadratic convergence when the governing nonlinear equations for<br />
a boundary value problem are solved by the Newton-like iterative schemes. A simple but efficient<br />
algorithm will be demonstrated to testify the correctness <strong>of</strong> the tangent operator locally <strong>of</strong> a<br />
particular model without going into details <strong>of</strong> the finite element implementation [1].
Section 6: Material modelling in solid mechanics 141<br />
[1] Steinmann P, Hossain M, Possart G (2011), Hyperelastic models for rubber-like materials:<br />
Consistent tangent operators and suitability for Treloar’s data. Archive <strong>of</strong> Applied Mechanics,<br />
In review (2011)<br />
[2] Boyce MC, Arruda EM (2000), Constitutive models <strong>of</strong> rubber elasticity: a review. Rubber<br />
Chemistry and Technology, 73: 504-523, 2000<br />
[3] Marckmann G, Verron E (2006), Comparison <strong>of</strong> hyperelastic models for rubber-like materials.<br />
Rubber Chemistry and Technology, 79 (2006) 835-858<br />
Accelerating constitutive modeling by automatic tangent generation<br />
Steffen Rothe, Stefan Hartmann (TU Clausthal) Schedule<br />
Nowadays models become more and more complex. Within the framework <strong>of</strong> finite elements a<br />
material, i.e. consistent, tangent is required for the overall Newton-like method. Obtaining these<br />
derivatives is time consuming and error-prone which contradicts to the goal <strong>of</strong> changing the model<br />
during the developing process. On the one hand the calculation by hand can be very expensive<br />
and on the other hand also the implementation has to be done with high diligence. Therefore, a<br />
fast and safe way <strong>of</strong> consistent tangent generation will be presented with the help <strong>of</strong> automatic<br />
differentiation (AD) techniques.<br />
Analytical tangents have the advantage that they are exact. However during the constitutive<br />
modeling process a change <strong>of</strong> the model is natural. Thus, the effort is very high to calculate<br />
the derivative after every modification. Numerical tangents computed by finite differences are<br />
easy to compute, but can lead to a significant slowdown or even to a failure <strong>of</strong> the simulation<br />
due to numerical errors. Tangents generated by OpenAD have no round-<strong>of</strong>f errors and are easily<br />
computed by the help <strong>of</strong> automatic differentiation.<br />
These three methods (analytical, numerical and automatic differentiation) for tangent generation<br />
will be analyzed concerning the simulation time and applicability for a number <strong>of</strong> different<br />
constitutive models.<br />
S6.9: Microheterogeneous Materials Thu, 13:30–15:30<br />
Chair: Johannes Schnepp, Eleni Agias<strong>of</strong>itou S1|01–A03<br />
The boundary value problems <strong>of</strong> the full coupled theory <strong>of</strong> poroelasticity for materials<br />
with double porosity<br />
Merab Svanadze (Ilia State University, Tbilisi) Schedule<br />
Porous materials play an important role in many branches <strong>of</strong> engineering, e.g., the petroleum industry,<br />
chemical engineering, geomechanics, and, in recent years, biomechanics. The construction<br />
and the intensive investigation <strong>of</strong> the theories <strong>of</strong> continua with microstructures arise by the wide<br />
use <strong>of</strong> porous materials into engineering and technology.<br />
The general 3D theory <strong>of</strong> poroelasticity for materials with single porosity was formulated by<br />
Biot (1941). The double porosity model was first proposed by Barenblatt and coauthors (1960).<br />
The quasi-static theory <strong>of</strong> poroelasticity for materials with double porosity in the framework <strong>of</strong><br />
mixture theory was presented by Aifantis and his co-workers (1982).<br />
In this paper the full coupled theory <strong>of</strong> poroelasticity for materials with double porosity is<br />
presented. This theory unifies the earlier proposed quasi-static model <strong>of</strong> Aifantis <strong>of</strong> consolidation<br />
with double porosity. The boundary value problems (BVPs) <strong>of</strong> the steady vibrations are investigated.<br />
The fundamental solution <strong>of</strong> system <strong>of</strong> equations <strong>of</strong> steady vibrations is constructed. The
142 Section 6: Material modelling in solid mechanics<br />
basic properties <strong>of</strong> plane waves and the radiation conditions for regular vector are established. The<br />
uniqueness theorems <strong>of</strong> the internal and external BVPs <strong>of</strong> steady vibrations are proved. The basic<br />
properties <strong>of</strong> elastopotentials are established. The representation <strong>of</strong> general solution <strong>of</strong> equations<br />
<strong>of</strong> steady vibrations is obtained. The existence <strong>of</strong> regular solution <strong>of</strong> the BVPs by means <strong>of</strong> the<br />
boundary integral method and the theory <strong>of</strong> singular integral equations are proved.<br />
Application <strong>of</strong> an anisotropic growth and remodelling formulation to computational<br />
topology optimisation<br />
Tobias Waffenschmidt (TU Dortmund), Andreas Menzel (TU Dortmund / Lund University) Schedule<br />
A classical topology optimisation problem consists <strong>of</strong> a problem-specific objective function which<br />
has to be minimised in consideration <strong>of</strong> particular constraints with respect to design and state<br />
variables. In this contribution we present a conceptually different approach for the optimisation or<br />
rather improvement <strong>of</strong> the topology <strong>of</strong> a structure which is not based on a classical optimisation<br />
technique. Instead, we establish a constitutive micro-sphere-framework in combination with an<br />
energy-driven anisotropic microstructural growth formulation, which was originally proposed for<br />
the simulation <strong>of</strong> adaptation and remodelling phenomena in hard biological tissues such as bones.<br />
The key aspect <strong>of</strong> this contribution is to investigate this anisotropic growth formulation with<br />
a special emphasis on its topology-optimising characteristics or rather topology-improving properties.<br />
To this end, several illustrative three-dimensional benchmark-type boundary value problems<br />
are discussed and compared qualitatively with the results obtained by classic topologyoptimisation<br />
strategies. The simulation results capture the densification effects and clearly identify<br />
the main load bearing regions. It turns out, that even though making use <strong>of</strong> this conceptually<br />
different growth formulation as compared to the procedures used in the more classic topologyoptimisation<br />
context, we identify qualitatively very similar topologies. Moreover, in contrast to<br />
common topology optimisation strategies, which mostly aim to optimise merely the structure,<br />
i.e. size, shape or topology, our formulation also contains the optimisation or improvement <strong>of</strong> the<br />
material itself, whichapart from the structural improvementresults in the generation <strong>of</strong> problemspecific<br />
local material anisotropy and textured evolution.<br />
Amplification damping properties <strong>of</strong> multiphase composites with spherical and fibers<br />
inclusions<br />
Sergey Lurie (Institute <strong>of</strong> Applied Mechanics, RAS), Natalia Tuchkova (Dorodnicyn Computing<br />
Centre, RAS), Juri Soliaev (Institute <strong>of</strong> Applied Mechanics, RAS) Schedule<br />
We consider composite materials reinforced with spherical and fibrous inclusions coated with a<br />
layer <strong>of</strong> lossy viscoelastic material. For the coating layers, typical viscoelastic properties <strong>of</strong> a polymer<br />
at and well above the glass transition region are assumed. It is shown that the remarkable loss<br />
amplification mechanism is also operative in such particulate-morphology materials. The aim <strong>of</strong><br />
our study is to determine the effective loss modulus composites, which formally defines the rate<br />
<strong>of</strong> energy dissipation per unit volume. We use a combination <strong>of</strong> modeling and numerical tools<br />
to study composite materials consisting <strong>of</strong> a matrix filled with spherical and fibrous inclusions<br />
coated with a layer <strong>of</strong> lossy viscoelastic material.<br />
The method <strong>of</strong> the four phases is used to describe the damping properties <strong>of</strong> composites<br />
filled with multiphase spherical inclusions and monolayer with multiphase fibrous inclusions. The<br />
constituent phases are supposed to be isotropic. Using the Eshelby method the effective moduli<br />
are determined self-consistently, by requiring that the average strain in the composite inclusion<br />
is the same as the macroscopic strain imposed at infinity. The analytical solution <strong>of</strong> this problem<br />
were received. The effective dynamic modulus and loss modulus were found using a viscoelastic
Section 6: Material modelling in solid mechanics 143<br />
analogy.<br />
It is shown[1] that the analytical give very similar, practically indistinguishable predictions<br />
from the numerical solutions which were received using finite element method. Hence, when<br />
studying such systems one can rely on the predictions <strong>of</strong> the four-phase sphere model, which<br />
are much easier to achieve than the finite element ones. a polymer at and well above the glass<br />
transition region are assumed. It is shown that by optimizing the thickness <strong>of</strong> the layers, one can<br />
achieve multiphase materials with effective loss characteristics significantly exceeding those <strong>of</strong> the<br />
individual materials constituents. It was found that for the considered composites have place the<br />
additional peak damping properties, which is realized for very small thicknesses <strong>of</strong> the viscoelastic<br />
phase. This peak is still about a factor 20 or so compared to the loss modulus <strong>of</strong> the pure matrix.<br />
We demonstrated that by introducing thin layers <strong>of</strong> a viscoelastic material, one can significantly<br />
increase the loss characteristics <strong>of</strong> discrete morphology multiphase materials. The layered fibers<br />
composites are also considered. It is shown that for such materials may be implemented at the<br />
same time as high elastic properties, and abnormally high damping properties.<br />
[1] A.A.Gusev , S.A. Lurie, Loss amplification effect in multiphase materials with viscoelastic<br />
interfaces. Macromolecules (2009) 42,14, 5372 – 5377.<br />
Modeling <strong>of</strong> composite structural elements made from aramid fiber using the method<br />
<strong>of</strong> features objects<br />
Michał Majzner, Andrzej Baier (Silesian University <strong>of</strong> Technology) Schedule<br />
The use <strong>of</strong> modern materials such as composite materials, enabling the production <strong>of</strong> new or modifying<br />
existing design solutions, improve their technical characteristics, while use in the process<br />
<strong>of</strong> design and engineering and manufacturing, will allow the modification <strong>of</strong> endurance, physical<br />
and chemical properties to match the features and functionality that are comply with. In research<br />
studies, it is proposed to systematize and formalize elementary objects in the context <strong>of</strong> modeling<br />
and fabrication <strong>of</strong> objects created on the basis <strong>of</strong> structural fiber composites. Application <strong>of</strong> features<br />
objects methods was shows on an example <strong>of</strong> modeling the structural element, in the form<br />
<strong>of</strong> an existing manufactured from steel, which was modified and converted with aramid fiber. It<br />
was necessary to carry out research in the form <strong>of</strong> numerical analysis, examining the strength <strong>of</strong><br />
the modified object.<br />
On the fibres shape effect for non-linear and unidirectional stationary heat conduction<br />
in two-phase hollow cylinder with radially graded material properties<br />
Piotr Ostrowski (Technical University <strong>of</strong> Lodz) Schedule<br />
The main aim <strong>of</strong> this paper is to consider unidirectional and stationary heat conduction in the<br />
infnite two-phase hollow cylinder with temperature dependent material properties. The deterministic<br />
microstructure <strong>of</strong> this composite is periodic (for a fixed radius) along the angular axis<br />
and has slowly varying effective properties in the radial direction. Therefore, we deal here with<br />
a special case <strong>of</strong> functionally graded materials, FGM, c.f. Suresh, Mortensen (1998). One <strong>of</strong> the<br />
components is called fibre, which is arranged in considered hollow cylinder with circular pattern.<br />
The physical phenomenon <strong>of</strong> the heat transfer is described by well known Fourier’s equation<br />
c ˙ θ − ∇(K∇θ) = 0, (1)<br />
which contains temperature dependent (in this case), highly oscillating and discontinuous coefficients<br />
<strong>of</strong> K = K(θ) - heat conduction tensor, and c = c(θ) - specific heat. To this macroscopic<br />
model the tolerance averaging approximation will be used, cf. Wozniak, Wierzbicki (2000). The
144 Section 6: Material modelling in solid mechanics<br />
general approach to the description <strong>of</strong> longitudinally graded stratified media can be found in<br />
[Wozniak, Michalak, Jedrysiak 2008]. The fibres width function g = g(r) <strong>of</strong> radius r will be examined<br />
and its effects on the temperature field. The averaged differential equation has smooth<br />
and slowly varying coefficients, hence in some special cases, for boundary value problem, analytical<br />
solution can be obtained. In other cases, numerical methods have to be used. This model<br />
takes into account the effect <strong>of</strong> microstructure size on the overall heat transfer behaviour.<br />
[1] S. SURESH, A. MORTENSEN, Fundamentals <strong>of</strong> functionally graded materials, Cambridge,<br />
The University Press, 1998.<br />
[2] Cz. WOZNIAK, B. MICHALAK, J. JEDRYSIAK (eds), Thermomechanics <strong>of</strong> micro-heterogeneous<br />
solids and structures. Tolerance averaging approach, Wydawnictwo Politechniki Lodzkiej,<br />
Lodz, 2008.<br />
S6.10: Elasticity, Viscoelasticity, -plasticity III Thu, 13:30–15:30<br />
Chair: Daniel Balzani S1|01–A1<br />
Network evolution model: thermodynamics consistency, parameter identification and<br />
finite element implementation<br />
Vu Ngoc Khiêm, Roozbeh Dargazany, Mikhail Itskov (RWTH Aachen) Schedule<br />
In this contribution, the previously proposed network evolution model [1] for carbon black filled<br />
elastomers is further studied. First, we show that the model does not contradict the second law <strong>of</strong><br />
thermodynamics and is thus thermodynamically consistent. On the basis <strong>of</strong> new experimental data<br />
the influence <strong>of</strong> filler concentration on the material parameters is further examined. Accordingly,<br />
this influence concerns only three material parameters and is approximated by phenomenological<br />
relations. These relations enable one to simulate rubbers based on the same compound with<br />
various filler concentrations. Finally, the model is implemented to the FE-S<strong>of</strong>tware ABAQUS and<br />
illustrated by a number <strong>of</strong> numerical examples. The examples demonstrate good agreement with<br />
experimental results with respect to the Mullins-Effect, permanent set and induced anisotropy.<br />
[1] R. Dargazany and M. Itskov, A network evolution model for the anisotropic Mullins effect<br />
in carbon black filled rubbers, International Journal <strong>of</strong> Solids and Structures 46 (2009),<br />
2967–2977.<br />
Shakedown analysis <strong>of</strong> periodic composites with kinematic hardening material model<br />
Min Chen, A. Hachemi, D. Weichert (RWTH Aachen) Schedule<br />
Lower-bound limit and shakedown analysis <strong>of</strong> periodic composites with the consideration <strong>of</strong> kinematic<br />
hardening are investigated on the representative volume element. With the combination <strong>of</strong><br />
homogenization theory, the homogenized macroscopic admissible loading domains are evaluated.<br />
Furthermore, the strengths <strong>of</strong> periodic composites <strong>of</strong> elastic-perfectly plastic, unlimited and linear<br />
limited kinematic hardening material models are calculated and compared in this paper.<br />
Theory <strong>of</strong> mixture based material modeling - An inelastic material model for a 12%chromium<br />
steel<br />
Andreas Kutschke, Konstantin Naumenko, Holm Altenbach (<strong>Universität</strong> Magdeburg) Schedule
Section 6: Material modelling in solid mechanics 145<br />
Components composed <strong>of</strong> advanced heat resistant steels face a complex loading <strong>of</strong> mechanical and<br />
thermal stresses under cyclic and long-term conditions. Additionally, a failure <strong>of</strong> these components<br />
usually has serious outcome, because <strong>of</strong> the extreme working conditions. From this follows the<br />
need <strong>of</strong> a reliable material model for the construction process.<br />
Classical technical guidelines are historically grown and the experience <strong>of</strong> engineers contributed<br />
to their development, but it turns out that these classical guidelines face their limit <strong>of</strong> use. Recently<br />
more sophisticated material models are developed to reach the real limit <strong>of</strong> the materials and to<br />
predict their behavior with more accuracy.<br />
Starting with the theoretical concept <strong>of</strong> Prandtl, who introduced the idea <strong>of</strong> a hardening<br />
substance in a material, and the investigations <strong>of</strong> Mughrabi, who established a composite model<br />
for chromium steels, the advanced steels are treated as a composition <strong>of</strong> at least two continua, in<br />
the sense <strong>of</strong> the theory <strong>of</strong> mixture.<br />
Therefore the general balance equations for a mixture will be presented. The example <strong>of</strong> a<br />
12% chromium steel will be used to illustrate this approach and to derive a material model for<br />
a mixture <strong>of</strong> two constituents. It will be shown that the model predicts tension-, compression-,<br />
cyclic-creep, uniaxial monotonic tension und low-cycle-fatigue loading in a satisfying manner in<br />
comparison with experimental results.<br />
Zur Abtragssimulation beim Strömungsschleifen (AFM)<br />
Joachim Schmitt, Stefan Diebels (<strong>Universität</strong> des Saarlandes) Schedule<br />
Im Zuge konkurrenzfähiger Produktionsverfahren werden seit einigen Jahren schwer zugängliche<br />
Kanten im Inneren von komplex aufgebauten Fertigungsteilen (wie beispielsweise die Gehäuse von<br />
Einspritzanlagen) mittels des Strömungsschleifens (Abrasive flow machining - AFM) verrundet<br />
bzw. oberflächenvergütet. Dazu wird eine mit Schleifpartikeln versetzte Silikonpaste mehrfach<br />
durch das Bauteil gepresst. Das viskose Verhalten der Paste ist dabei für die effektive Wirkung<br />
dieses Verfahrens sehr wichtig. Beim Überströmen von Kanten steigt die Schergeschwindigkeit und<br />
damit auch die Viskosität je nach Materialmodell überproportional an. Die so geänderten Druckund<br />
Geschwindigkeitsverhältnisse an der Bauteiloberfläche verändern auch den Materialabtrag<br />
durch die Schleifpaste.<br />
Im Rahmen dieser Studie werden zunächst die viskosen Eigenschaften der Paste anhand von<br />
Experimenten untersucht und die Modellparameter bestimmt. Im zweiten Teil wird die Paste<br />
hinsichtlich ihrer abrasiven Eigenschaften vorgestellt und eine Abschätzung des Materialabriebs<br />
vorgenommen. Ein daraus gebildetes einfaches Abtragsmodell wird mittels einer FEM-Simulation<br />
an elementaren Bauteilgeometrien umgesetzt und qualitativ überprüft.<br />
Material parameter identification using model reduction to uniaxial tensile tests<br />
Stephan Krämer, Steffen Rothe, Stefan Hartmann (TU Clausthal) Schedule<br />
Uniaxial tensile tests are commonly used for material parameter identification. It is also common<br />
to use one-dimensional formulations <strong>of</strong> a constitutive model to identify the corresponding<br />
material constants, although these material parameters are not necessarily identical to the material<br />
parameters in the three-dimensional material model. We present an easy way to reduce a<br />
three-dimensional material routine to the case <strong>of</strong> uniaxial tension and to use the reduced form<br />
to derive material parameters using common trust-region algorithms. With this approach one<br />
is able to use the full three-dimensional model for parameter identification. Instead <strong>of</strong> using a<br />
full finite element s<strong>of</strong>tware, one is able to use the material driver routine, which leads to a more<br />
straight forward calculation <strong>of</strong> material parameters. In this respect, it is shown that the classical<br />
structure <strong>of</strong> stress algorithms and consistent tangent operators are necessary within the three-
146 Section 6: Material modelling in solid mechanics<br />
to one-dimensional problem reduction. This procedure is also extendable to further homogeneous<br />
stress- and strain-states.<br />
Systematic representation <strong>of</strong> the yield criteria for isotropic materials<br />
Vladimir A. Kolupaev (DKI <strong>Darmstadt</strong>), Holm Altenbach (<strong>Universität</strong> Magdeburg) Schedule<br />
The theory <strong>of</strong> plasticity operates with different flow criteria <strong>of</strong> incompressible material behavior.<br />
These criteria have hexagonal symmetry in the π-plane and do not distinguish between tension<br />
and compression (non-SD-effect). Many tasks in the engineering practice are treated on the basis<br />
<strong>of</strong> these criteria and the flow rule.<br />
Selection <strong>of</strong> an appropriate criterion for a specific material is challenging. The models <strong>of</strong> Tresca<br />
and Schmidt-Ishlinsky, representing two regular hexagons in the π-plane, define accordingly the<br />
lower and the upper limit <strong>of</strong> convexity. The criteria <strong>of</strong> Sokolovskij and Ishlinsky-Ivlev describe<br />
the regular dodecagons in the π-plane and have only geometrical meaning. In difference to these<br />
four criteria, the model <strong>of</strong> von Mises has no singular corners and delivers unique results by the<br />
strain rates calculation.<br />
The evaluation <strong>of</strong> the measurements shows that the material behavior differs from the idealized<br />
models. The models proposed by Drucker, Dodd-Naruse, Edelman-Drucker and Hershey aim to<br />
better adapt the flow surface. These models are the functions <strong>of</strong> one parameter. They have no<br />
claims on the generality and are used only for the approximation <strong>of</strong> the measurements.<br />
Three models with one parameter are known as generalized models: Unified Yield Criterion<br />
(UYC) <strong>of</strong> Yu, Bi-Cubic Model (BCM), and Multiplicative Ansatz (MA) [1]. These models include<br />
the models <strong>of</strong> Tresca and Schmidt-Ishlinsky. They allow approximating <strong>of</strong> existing measurements<br />
better than other models.<br />
This work compares the flow criteria. For this aim their geometries in the π-plane will be<br />
considered in polar coordinates R and ϕ. The radii <strong>of</strong> the surface at the angles <strong>of</strong> ϕ = 15 and<br />
30 ◦ are related to the radius at ϕ = 0 ◦ : h = R(15 ◦ )/R(0 ◦ ), k = R(30 ◦ )/R(0 ◦ ). On the basis <strong>of</strong><br />
these two relations, well-known criteria will be systematized and shown in the h − k–diagram.<br />
New criteria will be introduced. The convexity limits for them will be stated.<br />
From the h−k–diagram, it is clear that UYC and MA set left and right boundary <strong>of</strong> convexity.<br />
Thus, the extreme solutions for parts can be found. The two models UYC and MA are the<br />
functions <strong>of</strong> the parameter k. The linear combination <strong>of</strong> UYC and MA provides a universal model<br />
with two parameters k and ξ ∈ [0, 1] describing all convex surfaces <strong>of</strong> incompressible material<br />
behavior <strong>of</strong> hexagonal symmetry in the π-plane.<br />
The proposed consideration <strong>of</strong> the flow criteria simplifies the selection <strong>of</strong> the model and is<br />
suitable for didactic purposes. All known and new flow criteria can be described by universal<br />
model, and thus can be omitted.<br />
[1] Kolupaev, V. A., Altenbach, H.: Considerations on the unified strength theory due to Mao-<br />
Hong Yu, Forschung im Ingenieurwesen 74(3), (2010).<br />
S6.11: Special Methods in Material Modeling Thu, 16:00–18:00<br />
Chair: Bernhard Eidel, Markus Scholle S1|01–A03<br />
Modeling <strong>of</strong> Carbon Nanotubes by Molecular Mechanics<br />
Oliver Eberhardt, Thomas Wallmersperger (TU Dresden) Schedule<br />
Carbon Nanotubes (CNTs) are structures in the nanoscale consisting <strong>of</strong> carbon atoms which are<br />
arranged in a hexagonal lattice. Hence, they can be imagined as a plane sheet <strong>of</strong> graphene rolled
Section 6: Material modelling in solid mechanics 147<br />
into a seamless tube. By doing so we obtain a so called Single Wall Carbon Nanotube (SWCNT).<br />
Besides Single Wall Carbon Nanotubes also Double Wall Carbon Nanotubes (DWCNT) and, in<br />
general, Multi Wall Carbon Nanotubes (MWCNT) exist. Their high stiffness and active deformation<br />
<strong>of</strong> approx. 1 % at applied low electric voltages (approx. 1 V) make the Carbon Nanotubes a<br />
very promising material for applications e.g. in new classes <strong>of</strong> composites and actuators/sensors.<br />
In this research the approach to model Carbon Nanotubes is made by using molecular mechanics.<br />
The aim <strong>of</strong> these efforts is to determine the mechanical properties, for example the Young’s<br />
modulus. The Molecular Mechanics method originates in the investigation <strong>of</strong> the properties <strong>of</strong><br />
big molecules which due to their size cannot be handled by quantum mechanical methods. In<br />
Molecular Mechanics the behavior <strong>of</strong> the covalent bonds in a Single Wall Carbon Nanotube is<br />
represented by a set <strong>of</strong> potentials. Here every single potential expression describes a corresponding<br />
bond deformation. As a result <strong>of</strong> the description <strong>of</strong> the bonds by potentials, the force acting<br />
between the atoms can be calculated as the derivatives <strong>of</strong> the potentials with respect to their<br />
corresponding displacement variable. Hence, the Carbon Nanotube is modeled by point masses<br />
representing the carbon atoms and a set <strong>of</strong> springs or beam elements representing the bonds. Regarding<br />
Multi Wall Carbon Nanotubes this model can be extended by adding the van-der-Waals<br />
interactions, described by another potential.<br />
During the process <strong>of</strong> modeling and also during the evaluation <strong>of</strong> the results we have to rise<br />
several challenges. Since the Molecular Mechanics method is a so called semi-empiric method we<br />
have to choose between different sets <strong>of</strong> potentials. Some <strong>of</strong> these potentials - leading to linear<br />
or nonlinear behavior <strong>of</strong> the interaction forces between the atoms - are investigated regarding<br />
their advantages and disadvantages. In order to illustrate this we compare the (theoretical) results<br />
available in literature with our numerical results, which we obtain by using the model to<br />
conduct a virtual tensile test. The dependance <strong>of</strong> the Young’s modulus on type and diameter <strong>of</strong><br />
the Carbon Nanotubes is discussed.<br />
Dislocation Dynamics in Quasicrystals<br />
Eleni Agias<strong>of</strong>itou, Markus Lazar (TU <strong>Darmstadt</strong>), Helmut Kirchner (Leibniz Institut für neue<br />
Materialien, Saarbrücken) Schedule<br />
In this work, we present a theoretical framework <strong>of</strong> dislocation dynamics in quasicrystals [1] according<br />
to the continuum theory <strong>of</strong> dislocations. Quasicrystals have been discovered by Shechtman<br />
et al [2] in 1982 opening a new interdisciplinary research field. A comprehensive presentation <strong>of</strong><br />
the current state <strong>of</strong> the art <strong>of</strong> this research field, focused on the mathematical theory <strong>of</strong> elasticity,<br />
can be found in the recently published book <strong>of</strong> Fan [3].<br />
We start presenting the fundamental theory <strong>of</strong> moving dislocations in quasicrystals giving<br />
the dislocation density tensors and introducing the dislocation current tensors for the phonon<br />
and phason fields, including the Bianchi identities. In the literature, there exist different versions<br />
<strong>of</strong> generalized linear elasticity theory <strong>of</strong> quasicrystals. The difference <strong>of</strong> these versions lies in the<br />
dynamics <strong>of</strong> phonon and phason fields. In the present work, we deal with the elastodynamic as well<br />
as the elasto-hydrodynamic model <strong>of</strong> quasicrystals. According to the first model, the equations <strong>of</strong><br />
motion are <strong>of</strong> wave-type for both phonons and phasons while according to the second model the<br />
equations <strong>of</strong> motion for the phonons are equations <strong>of</strong> wave-type and for the phasons are equations<br />
<strong>of</strong> diffusion-type. Therefore, we give the equations <strong>of</strong> motion for the incompatible elastodynamics<br />
as well as for the incompatible elasto-hydrodynamics <strong>of</strong> quasicrystals.<br />
We continue with the derivation <strong>of</strong> the balance law <strong>of</strong> pseudomomentum thereby obtaining<br />
the generalized forms <strong>of</strong> the Eshelby stress tensor, the pseudomomentum vector, the dynamical<br />
Peach-Koehler force density and the Cherepanov force density for quasicrystals. Moreover, we<br />
deduce the balance law <strong>of</strong> energy that gives rise to the generalized forms <strong>of</strong> the field intensity
148 Section 6: Material modelling in solid mechanics<br />
vector and the elastic power density <strong>of</strong> quasicrystals. The above balance laws are produced for<br />
both models. The differences between the two models and their consequences are revealed. The<br />
influences <strong>of</strong> the phason fields as well as <strong>of</strong> the dynamical terms are also discussed.<br />
[1] E. Agias<strong>of</strong>itou, M. Lazar and H. Kirchner, Generalized dynamics <strong>of</strong> moving dislocations in<br />
quasicrystals, J. Phys.: Condens. Matter 22 (2010), 495401 (8pp).<br />
[2] D. Shechtman, I. Blech, D. Gratias and J. W. Cahn, Metallic phase with long-range orientational<br />
order and no translational symmetry, Phys. Rev. Lett. 53 (1984), 1951 – 1953.<br />
[3] T. Fan, Mathematical Theory <strong>of</strong> Elasticity <strong>of</strong> Quasicrystals and its Applications, Science<br />
Press Beijing and Springer-Verlag Berlin, 2011.<br />
On inverse form finding based on an ALE formulation<br />
Sandrine Germain, Paul Steinmann (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
A challenge in the design <strong>of</strong> functional parts in forming processes is the determination <strong>of</strong> the<br />
initial, undeformed shape such that under a given load a part will obtain the desired deformed<br />
shape. Two numerical methods might be used to solve this problem, which is inverse to the<br />
standard kinematic analysis in which the undeformed shape is known and the deformed shape<br />
unknown.<br />
The first method deals with the formulation <strong>of</strong> an inverse mechanical problem, where the<br />
spatial (deformed) configuration and the mechanical loads are given. Hence the objective is to<br />
find the inverse deformation map that determines the (undeformed) material configuration.<br />
The second method deals with shape optimization that predicts the initial shape in the sense<br />
<strong>of</strong> an inverse problem via successive iterations <strong>of</strong> the direct problem. In [1] a nodes-based shape<br />
optimization approach for elastoplastic materials based on logarithmic strains is presented. An<br />
update <strong>of</strong> the reference configuration is considered in order to avoid mesh distortions, which <strong>of</strong>ten<br />
occur in nodes-based optimization problems. The principal drawback is the high computational<br />
costs. An alternative is an Arbitrary-Lagrangian-Eulerian (ALE) formulation [2,3], which is neither<br />
purely Lagrangian (the nodes are not attached to the material) nor purely Eulerian (the nodes<br />
are not fixed in space). The nodes are free to move in space independently <strong>of</strong> the material.<br />
In this contribution we review the ALE formulation [2,3] for anisotropic hyperelastic materials<br />
and its application in shape optimization. Several examples illustrate the ALE approach in<br />
hyperelasticity. Results and computational costs are compared with the ones obtained with the<br />
approach in [1].<br />
This work is supported by the German Research Foundation (DFG) within the Collaborative<br />
Research Centre SFB Transregio 73.<br />
[1] S. Germain and P. Steinmann. Towards form finding methods for a sheet-bulk-metal (DC04),<br />
15th ESAFORM, Key Engineering Materials submitted (<strong>2012</strong>).<br />
[2] E. Kuhl et al., An ALE formulation based on spatial and material settings <strong>of</strong> continuum<br />
mechanics. Part 1: Generic hyperelastic formulation, Comput. Methods Appl. Mech. Engrg.<br />
193 (2004), 4207 – 4222.<br />
[3] H. Askes et al., An ALE formulation based on spatial and material settings <strong>of</strong> continuum<br />
mechanics. Part 2: Classification and applications, Comput. Methods Appl. Mech. Engrg.<br />
193 (2004), 4223 – 4245.
Section 6: Material modelling in solid mechanics 149<br />
On the direct connection <strong>of</strong> rheological elements in nonlinear continuum mechanics<br />
Ralf Landgraf, Jörn Ihlemann (TU Chemnitz) Schedule<br />
The direct connection <strong>of</strong> rheological elements is a widely used concept to develop material models<br />
for one-dimensional deformation processes at small strains. This concept is based on the decomposition<br />
<strong>of</strong> the total strain into several subparts and the formulation <strong>of</strong> single material laws for<br />
idealized phenomena (e.g. nonlinear elastic behaviour and viscous or plastic yielding). Several<br />
<strong>of</strong> those elements are then assembled to one complex material model. This can be achieved by<br />
enforcing the equilibrium <strong>of</strong> stresses on the connecting points between rheological elements.<br />
Within the scope <strong>of</strong> nonlinear continuum mechanics there also exists the concept <strong>of</strong> rheological<br />
elements. The kinematics is described by the deformation gradient which gets multiplicatively<br />
decomposed into several sub deformation gradients. For the definition <strong>of</strong> the material behaviour,<br />
a common approach is to formulate a free energy function as a sum <strong>of</strong> sub free energy functions<br />
attributed to the defined sub deformation gradients. By the evaluation <strong>of</strong> the Clausius-Duheminequality<br />
and under consideration <strong>of</strong> constitutive assumptions a system <strong>of</strong> equations describing<br />
a thermodynamically consistent material behaviour can be derived. Depending on particular definitions,<br />
those materials can include a mixture <strong>of</strong> elastic, viscous and plastic material behaviour.<br />
An alternative approach has been presented by Ihlemann (2006). It is based on the additive<br />
decomposition <strong>of</strong> the stress power density and leads to a system <strong>of</strong> equations for the derivation<br />
<strong>of</strong> the stress equilibrium on defined intermediate configurations as well as the derivation <strong>of</strong> the<br />
total stresses. Special attention has to be given to the definition <strong>of</strong> accurate stress measures on<br />
the intermediate configurations. By this approach, a formal procedure for the direct connection <strong>of</strong><br />
single elements at large deformation processes can be obtained. The procedure itself is independent<br />
<strong>of</strong> the concrete material behaviour.<br />
The concept <strong>of</strong> direct connection <strong>of</strong> rheological elements in nonlinear continuum mechanics<br />
and some examples for its application will be presented. Furthermore, a numerical strategy for<br />
the direct implementation <strong>of</strong> this concept will be demonstrated.<br />
[1] J. Ihlemann (2006), Beobachterkonzepte und Darstellungsformen der nichtlinearen Kontinuumsmechanik,<br />
Habilitation, <strong>Universität</strong> Hannover<br />
A stochastic model for the direct and the inverse problem <strong>of</strong> adhesive materials<br />
N. Nörenberg, R. Mahnken (<strong>Universität</strong> Paderborn) Schedule<br />
This work deals with the generation <strong>of</strong> artificial data [1] based on experimental data for adhesive<br />
materials and the application <strong>of</strong> this data to the inverse and the direct problem. In reality there are<br />
only a very limited number <strong>of</strong> experimental data available. Therefore, the prediction <strong>of</strong> material<br />
behaviour is difficult and a statistical analysis with a stochastic proved thesis is nearly impossible.<br />
In order to increase the number <strong>of</strong> tests a method <strong>of</strong> stochastic simulation based on time series<br />
analysis [2] is applied. With artificial data an arbitrary number <strong>of</strong> data is available and the<br />
process <strong>of</strong> the parameter identification can be statistically analysed. Additionally, two examples<br />
are shown, which adapt the analysed material parameter to the direct problem. The stochastic<br />
finite element method [3] is used to take into account the distribution and deviation <strong>of</strong> the fracture<br />
strain.<br />
[1] S. Schwan, Identifikation der Parameter inelastischer Werkst<strong>of</strong>fmodelle: Statistische Analyse<br />
und Versuchsplanung. Diss. Shaker, 2000.
150 Section 6: Material modelling in solid mechanics<br />
[2] P. J. Brockwell and R. A. Davis, Time series: theory and methods. Springer, 2009<br />
[3] I. Babuška, R. Tempone and G. E. Zouraris, Galerkin finite element approximations <strong>of</strong> stochastic<br />
elliptic partial differential equations. SIAM Journal on Numerical Analysis 42(2)<br />
(2005), 800 – 825<br />
Analysis <strong>of</strong> nanoindentation experiments by means <strong>of</strong> rheological models<br />
Holger Worrack, Wolfgang H. Müller (TU Berlin) Schedule<br />
The nanoindentation technique, which is similar to the instrumented indentation hardness according<br />
to MARTENS, is established in the field <strong>of</strong> material characterization at small dimensions.<br />
It is daily practice to analyze nanoindentation data with an almost classical formula based on<br />
the publications by Oliver and Pharr and Fischer-Cripps. In this formula the gradient at the<br />
beginning <strong>of</strong> the unloading curve is used to determine Youngs modulus <strong>of</strong> the tested material,<br />
which is one <strong>of</strong> the material parameters <strong>of</strong> interest.<br />
The procedure works well for elastic time-independent plastic material behavior, for example<br />
copper and the calibration material fused silica, even at higher test temperatures. However, low<br />
melting solder materials are susceptible to creep behavior, especially at the higher indentation<br />
temperatures where the homologous temperature is > 0.5. As a result <strong>of</strong> the creep effects the<br />
beginning <strong>of</strong> the unloading curve <strong>of</strong>ten shows a bulge. This discrepancy from the ideal unloading<br />
curve complicates the correct determination <strong>of</strong> the unloading stiffness and finally yields to<br />
incorrect results for Youngs modulus.<br />
For this reason, additional analysis procedures are required to determine the material parameters<br />
more precisely. In this paper the authors want to give an introduction to an enhanced<br />
analysis <strong>of</strong> nanoindentation data based on rheological models, which are <strong>of</strong>ten used to describe<br />
the time-dependence <strong>of</strong> material response. Two examples <strong>of</strong> such models are the MAXWELL- and<br />
the KELVIN-body. In these models springs and dashpots connected in series and/or in parallel are<br />
used to describe the time-dependent material response. The viscous parameters, determined from<br />
the recorded data during the nanoindentation experiment, can be used to identify the mechanical<br />
material parameters. The authors present miscellaneous viscoeleastic and viscoplastic rheological<br />
models in connection with the corresponding equations which are used to extract the material<br />
properties from the recorded data. Results <strong>of</strong> the analysis are presented and discussed in context<br />
with the results from the classical Oliver and Pharr procedure and with the material parameters<br />
published in the literature. Finally, the models are assessed by their applicability <strong>of</strong> modeling the<br />
time-dependent material response <strong>of</strong> low melting solder materials.<br />
S6.12: Special Material Behavior Thu, 16:00–18:00<br />
Chair: Lurie Sergey, Jaan-Willem Simon S1|01–A1<br />
Carbon Fibre Prepregs: Simulation <strong>of</strong> a Thermo-Mechanical-Chemical Coupled Problem<br />
F. Hankeln, R. Mahnken (<strong>Universität</strong> Paderborn) Schedule<br />
In automotive industry research is done to replace high strength steel by combinations <strong>of</strong> steel<br />
and carbon-fibre prepregs (pre-impregnated fibres). It is planned to form both steel and uncured<br />
prepregs in one step followed by the curing process under pressure in the forming die [1]. The<br />
ability to simulate the mechanical behaviour during forming and curing would allow more economical<br />
processes. The simulation <strong>of</strong> prepregs must regard highly anisotropic, viscoelastic and<br />
thermal- chemical properties. For this the model is split into an anisotropic elastic part, which
Section 6: Material modelling in solid mechanics 151<br />
represents the fibre fraction and an isotropic, viscoelastic part, representing the matrix. This part<br />
also contains curing, causing a dependency on time and temperature. During deep-drawing large<br />
deformations are occurring, so a large strain model regarding anisotropy[2], viscoelasticity [3]<br />
and curing [4] has been developed. Also experiments were made to validate this model. Current<br />
progress is the identification <strong>of</strong> material parameters.<br />
[1] Homberg, W., Dau, J., Damerow, U. Combined Forming <strong>of</strong> Steel Blanks with Local CFRP<br />
Reinforcement, in: G. Hirt, A. E. Tekkaya (Eds.), steel research int., Special Edition: Proceedings<br />
<strong>of</strong> the 10th International Conference on Technology <strong>of</strong> Plasticity, Wiley-VCH,<br />
Weinheim, 2011, pp. 441-446<br />
[2] Menzel, A., Modelling and Computation <strong>of</strong> Geometrically Nonlinear Anisotropic Inelasticity,<br />
Dissertation, University <strong>of</strong> Kaiserlautern, 2002<br />
[3] Tschoegl, N.W. The Phenomenologial Theory <strong>of</strong> Linear Viscoelastic Behaviour, Springer<br />
Verlag, 1989<br />
[4] Lion, A. and Höfer, P., On the phenomenological representation <strong>of</strong> curing phenomena in<br />
continuum mechanics, Arch. Mech. 59, 2007<br />
On the axially compressed multiple walled carbon nanotubes<br />
Ligia Munteanu (Institute <strong>of</strong> Solid Mechanics <strong>of</strong> Romanian Academy) Schedule<br />
A new approach is proposed in this paper, which combines elements <strong>of</strong> Toupin-Mindlin strain<br />
gradient theory and the Molecular Mechanics to include the inlayer van der Waals atomistic<br />
interactions for axially compressed multiple walled carbon nanotubes. The neighboring walls <strong>of</strong><br />
a multiwalled nanotube are coupled through van der Waals interactions, and the shell buckling<br />
would initiate in the outermost shell, when nanotubes are short. The load-unloaded-displacement<br />
curve, the critical buckling and the appropriate values for elastic moduli are obtained. The theoretical<br />
results obtained show a good agreement with the experimental data reported by Waters,<br />
Gudury, Jouzi and Xu (2005). The size dependence <strong>of</strong> the hardness with respect to the depth<br />
and the radius <strong>of</strong> the indenter is also investigated. Results show a peculiar size influence on the<br />
hardness, which is explained via the shear resistance between the neighboring walls during the<br />
buckling <strong>of</strong> the multiwalled nanotubes. The present method can be further extended to investigate<br />
the stress-strain relations and the fracture behaviors <strong>of</strong> S/MWCNT<br />
From vortices to dislocations: How fluid mechanics can inspire solid mechanics<br />
Markus Scholle (Hochschule Heilbronn) Schedule<br />
Although it is known for nearly a century that production and movement <strong>of</strong> dislocations are the<br />
elementary processes responsible for the plastic deformation <strong>of</strong> a solid body, all attempts to derive<br />
a continuum theory <strong>of</strong> plasticity from the discrete micro–theory <strong>of</strong> dislocations did not succeed<br />
in universally valid field equations like e.g. Navier–Stokes equations in fluid dynamics.<br />
In this paper an approach is presented based on an analogy between dislocations and vortex<br />
lines in fluid flow. Since the dynamics <strong>of</strong> the latter ones is well understood in terms <strong>of</strong> the Navier–<br />
Stokes equations, it is near at hand to make use <strong>of</strong> this analogy in order to establish a kind <strong>of</strong><br />
’Navier–Stokes equations for the distorsion tensor’.<br />
Starting from Clebsch’s variational formulation for inviscid flow, a relation beween the symmetries<br />
<strong>of</strong> the Lagrangian and the balance <strong>of</strong> vorticity resulting from it is shown giving rise for<br />
the construction <strong>of</strong> another Lagrangian from which the respective dislocation balance results.
152 Section 6: Material modelling in solid mechanics<br />
The present state <strong>of</strong> the theory is discussed.<br />
On the connection <strong>of</strong> dissipation and deviatoric stress in the continuum theory <strong>of</strong><br />
defects<br />
Johannes Schnepp (RWTH Aachen) Schedule<br />
Continuous distributions <strong>of</strong> defects (e. g. dislocations) can be described as differential geometric<br />
properties <strong>of</strong> the material manifold. Material forces and the Eshelby tensor are also quantities<br />
in this three-dimensional material space. The relation to defects has been treated <strong>of</strong>ten in the<br />
literature and various theories for the dynamics <strong>of</strong> defects have been proposed.<br />
Moving defects lead to differential geometric quantities changing with time. This has motivated<br />
some authors to augment the three space-like coordinates in the material space by a time-like<br />
coordinate. In this way one gets a four-dimensional material space-time manifold, analogous to<br />
the four-dimensional physical space-time in the theory <strong>of</strong> relativity. A connection <strong>of</strong> a time-like<br />
material coordinate to temperature can be found in the literature on relativistic elasticity. These<br />
ideas will be brought together in this contribution and some implications will be developed.<br />
A time-like vector field in the material space-time can be associated with temperature and<br />
heat flux. Together with the three lattice vectors a tetrad field is defined and this field determines<br />
the differential geometric properties <strong>of</strong> the material manifold. If a variational formulation<br />
for a hyper-elastic solid is adopted, the derivatives <strong>of</strong> the Lagrangian density with respect to the<br />
components <strong>of</strong> the tetrad can be arranged in a four-dimensional second-order tensor. This tensor<br />
unifies the information about the three-dimensional Eshelby tensor (material momentum current),<br />
the entropy current, and the entropy density. The time-like component <strong>of</strong> the divergence <strong>of</strong> this<br />
tensor is the entropy production. Besides the entropy production due to heat transfer the theory<br />
yields entropy production due to defect movement which is proportional to deviatoric stress.<br />
Stress Reduction Factor <strong>of</strong> Ceramic Plate to Thermal Shock<br />
Weiguo Li, Tianbao Cheng (College <strong>of</strong> Resources and Environmental Science, Chongqing), Daining<br />
Fang (Peking University) Schedule<br />
In this work, through introducing the analytical solution to transient conduction problem for the<br />
thin rectangular plate with convection into the thermal stress field model <strong>of</strong> the elastic plate, the<br />
stress reduction factor which is useful in determining the thermal stresses in the ceramic plate<br />
subjected to thermal shock was presented in the dimensionless form. The properties and appropriate<br />
conditions <strong>of</strong> the stress reduction factor were analyzed. Then the definitions, origins and<br />
limitations <strong>of</strong> the first and second thermal stress fracture resistance parameters which characterize<br />
the thermal shock resistance <strong>of</strong> brittle ceramics were discussed. Because <strong>of</strong> the demands in<br />
the calculation <strong>of</strong> thermal stress, a new stress reduction factor was defined and compared with<br />
the previous one. For the given Biot number, the previous stress reduction factor first increases<br />
and then reaches a maximum value, and afterwards decreases as the Fourier number increases.<br />
However, the new stress reduction factor decreases as the Fourier number increases. The new<br />
factor is more convenient for calculating the thermal stress in the plate subjected to thermal<br />
shock. The presented results are useful for the calculating <strong>of</strong> the thermal stress and choosing <strong>of</strong><br />
the appropriate thermal stress fracture resistance parameter when the ceramic plate is subjected<br />
to thermal shock.<br />
Modeling Deformation Twinning in FeMn Alloys<br />
Shyamal Roy, Rainer Glüge, Albrecht Bertram (<strong>Universität</strong> Magdeburg) Schedule<br />
Multiple twinning [1] in single crystals is modeled by studying the response at each material<br />
point in order to understand micro-structural evolution and mechanical properties <strong>of</strong> FeMn
Section 6: Material modelling in solid mechanics 153<br />
(TWIP steel). Here the minimum elastic strain energy approach is used. It is well known that the<br />
elastic strain energy <strong>of</strong> an individual material is convex. Since twinning leads to isomorphic structures,<br />
the elastic strain energy <strong>of</strong> a twin material is convex too and hence, forms a non-convex<br />
energy landscape. A smooth strain energy landscape is constructed to avoid the discontinuity<br />
at the transition point from parent to twin material. A controlled viscous relaxation scheme is<br />
incorporated since the boundary value problem <strong>of</strong> the non-convex energy function is ill posed [2].<br />
Dealing with multiple energy wells is numerically very challenging. The solution is not deterministic<br />
as any twin configuration can be activated from the parent configuration, which is unknown<br />
initially. Therefore, to have a complete energy landscape in hand at the beginning is impossible.<br />
The material response is instantaneously calculated depending on which twin configuration is<br />
activated. However, the minimum strain energy approach faces its limitation because <strong>of</strong> elastic<br />
strain energy invariance, which occurs due to the crystallographic equivalence <strong>of</strong> possible twin<br />
configurations. Having identified the preferred twin configuration, the secondary and, hence, the<br />
multiple twinning are modeled.<br />
[1] Christian J. W., Mahajan S., Deformation Twinning, Prog Mat Sci, 39, 1-157 (1995)<br />
[2] Carstensen C., Ten Remarks on Non-convex Minimization for Phase Transition Simulations,<br />
Comp Meth App Mech Eng, 194, 169-193 (2005)
154 Section 7: Coupled problems<br />
Section 7: Coupled problems<br />
Organizers: Marc Kamlah (KIT), Bernd Markert (<strong>Universität</strong> Stuttgart)<br />
S7.1: Porous Media Problems Tue, 13:30–15:30<br />
Chair: Bernd Markert S1|03–223<br />
Investigations <strong>of</strong> wave induced fluid flow in heterogeneously and partially-saturated<br />
porous media<br />
Christian Becker, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
Wave induced fluid flow in partially-saturated porous media is a multiscale phenomenon. First<br />
evidence <strong>of</strong> this was gained by the fact that damping mechanisms that were forecast by models<br />
based on a macroscopic poroelastic approach differed from the results <strong>of</strong> conducted experiments.<br />
Based on the macroscopic models several enhancements were provided that allowed for the incorporation<br />
<strong>of</strong> flows occuring on the microscopic (squirt flow, cf.[1]) and mesoscopic scale (mesoscopic<br />
loss, cf.[2-3])<br />
In our contribution the physical phenomena <strong>of</strong> wave induced fluid flow processes are revisited<br />
briefly. Furthermore a thermodynamically sound three-phase model, developed in the framework<br />
<strong>of</strong> the Theory <strong>of</strong> Porous Media, suitable for the numerical analysis <strong>of</strong> partially-saturated porous<br />
media is presented. Representative elementary volumes (REVs) with layerwise-varying saturation<br />
and no-flux boundary condition on all boundaries are numerically investigated. Layers <strong>of</strong> varying<br />
saturation are oriented perpendicular to the flow direction. This setup will induce interlayer flow<br />
and is hence responsible for the mesoscopic loss.<br />
To identify and quantify mesoscopic loss mechanisms on the effective damping behaviour,<br />
relaxation- and creep-like one-dimensional numerical analyses are performed and discussed.<br />
[1] R. O’Connell, B. Budiansky, Seismic velocities in dry and saturated cracked solids, J. Geophys.<br />
Res. 79 (1974), 5412–5426.<br />
[2] J. E. White, Computed seismic speeds and attenuation in rocks with partial gas saturation,<br />
Geophysics 40 (1975), 224–232.<br />
[3] J. E. White, N. G. Mikhaylova, F. M. Lyakhovitskiy, Low-frequency seismic waves in fluid<br />
saturated layered rocks, Izvestija Academy <strong>of</strong> Sciences USSR, Phys. Solid Earth 11 (1975),<br />
654–659.<br />
Simulation <strong>of</strong> Freezing and Thawing Processes with Capillary Effects in fluid filled<br />
porous media<br />
Wolfgang Moritz Blossfeld, Joachim Bluhm (<strong>Universität</strong> Duisburg-Essen), Tim Ricken (TU Dortmund)<br />
Schedule<br />
In many branches <strong>of</strong> engineering, e.g. soil constructions, material science and geotechnics, freezing<br />
and thawing processes <strong>of</strong> fluid filled porous media play an important role. The coupled<br />
fluid-ice-solid behavior is strongly influenced by phase transition, heat and mass transport as<br />
well as interactions <strong>of</strong> fluid-solid/ice pressure depending on the entropy <strong>of</strong> fusion, see [1], and is<br />
accompanied by a volume expansion. The volume increases in space and time corresponds to the<br />
moving freezing front inside the porous solid. In this contribution, within the framework <strong>of</strong> the<br />
Theory <strong>of</strong> Porous Media (TPM) a macroscopic quadruple model consisting <strong>of</strong> the constituents<br />
solid, liquid (freezable water), ice and gas will be presented. Particular attention is paid to the
Section 7: Coupled problems 155<br />
description <strong>of</strong> the distribution <strong>of</strong> fluid pressure and solid stresses before, during and after the ice<br />
formation in consideration <strong>of</strong> energetic and capillary effects. For the detection <strong>of</strong> energetic effects<br />
regarding the characterization and the control <strong>of</strong> phase transition <strong>of</strong> water and ice, a physically<br />
motivated evolution equation for the mass exchange based on the local balance <strong>of</strong> the heat flux<br />
vector is used, see [2]. Furthermore, the porosity change <strong>of</strong> the porous materiel is considered, i.e.,<br />
the variation <strong>of</strong> permeability during ice formation can be simulated. Numerical examples will be<br />
presented to demonstrate the practical application <strong>of</strong> the model.<br />
[1] O. Coussy, Poromechanics <strong>of</strong> freezing materials, Journal <strong>of</strong> the Mechanics and Physics <strong>of</strong><br />
Solids 53, (2005), 1689 – 1718.<br />
[2] J. Bluhm, T. Ricken, W.M. Blossfeld, Ice-Formation in Porous Media, In Lecture Notes in<br />
Applied and Computational Mechanics 59, F. Pfeiffer, P. Wriggers, Series Eds., Advances<br />
in Extended and Multifield Theories for Continua, B. Markert, Ed., (2011), 219 p., [978-3-<br />
642-22737-0].<br />
Experimental evaluation <strong>of</strong> phase velocities and tortuosity in fluid-saturated porous<br />
and high-porous media<br />
Ibrahim Gueven, Patrick Kurzeja, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
Quantification <strong>of</strong> sound and ultrasound in high porous media saturated with viscous fluids is<br />
<strong>of</strong> great importance in many research areas with applications in engineering and medical technologies.<br />
In particular, Quantitative UltraSound (QUS) became <strong>of</strong> great interest with respect<br />
to osteoporosis diagnosis, cf. [2]. In order to improve predictive diagnosis tools, physical models<br />
are required. The accuracy <strong>of</strong> such multiphase models, like Biot’s poroelasticity [1,2], depends on<br />
various material parameters <strong>of</strong> the bulk phases but also parameters which take into account coupling<br />
phenomena. One <strong>of</strong> those important coupling parameters is the tortuosity <strong>of</strong> Biot’s theory,<br />
which is a geometrical and frequency-dependent quantity, cf. [1,2]. It accounts for the coupling<br />
<strong>of</strong> the solid and the fluid, especially in the high frequency range where inertia coupling dominates.<br />
In the present contribution, we present a novel method for the determination <strong>of</strong> the high frequency<br />
tortuosity parameter, α∞. Therefore, time-domain measurements <strong>of</strong> ultrasonic signals are<br />
performed with a transmission technique. Systems <strong>of</strong> sintered, monodisperse glassbeads (φ = 0.35)<br />
and aluminium foam (φ = 0.95) in combination with different pore fluids will be under the scope<br />
<strong>of</strong> the experimental investigations. Finally, the results are compared with analytical and numerical<br />
pore-scale wave propagation tests.<br />
[1] M. A. Biot, Theory <strong>of</strong> propagation <strong>of</strong> elastic waves in a fluid-saturated porous solid. I. Lowfrequency<br />
range, J. Acoust. Soc. Am., 28:168-178, II. Higher frequency range, J. Acoust.<br />
Soc. Am., 28:179-191, 1956.<br />
[2] H. Steeb, Ultrasound propagation in cancellous bone, Arch. Appl. Mech., 80:489-502, 2010.<br />
Numerical homogenization approach <strong>of</strong> acoustic attenuation in poroelastic media<br />
Ralf Jänicke, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
Acoustic waves propagating through a poroelastic medium are well-known to undergo certain<br />
attenuation mechanisms related to different length scales. Attenuation can be explained in particular<br />
by local pressure gradients induced by the passing wave and, as a consequence, by the local
156 Section 7: Coupled problems<br />
flow <strong>of</strong> the pore fluid relative to the skeleton. The critical frequency <strong>of</strong> attenuation is dictated by<br />
the range <strong>of</strong> fluid flow. One may distinguish between local effects (e.g. squirt flow, i.e. fluid flow<br />
in/between fractures) and meso scale effects (flow between patches <strong>of</strong> the poroelastic medium<br />
with spatially varying elastic and/or hydraulic coefficients).<br />
In the present contribution we apply a consistent (meanfield) homogenization approach to<br />
predict macroscopic effective properties <strong>of</strong> a mesoscopic poroelastic medium applying relaxation/creep<br />
tests. Whereas the heterogeneous meso scale is described using Biot’s theory <strong>of</strong> poroelasticity,<br />
the homogeneous macro scale is treated as a viscoelastic solid medium. In particular,<br />
we focus on the formulation <strong>of</strong> averaging rules relating meso- and macroscopic quantities and<br />
we comment on the formulation <strong>of</strong> relaxed boundary conditions and its impact on the complex<br />
viscous properties <strong>of</strong> the effective medium.<br />
Finally, we present certain 2-Dim and 3-Dim numerical results obtained by an u-p implementation<br />
in a Finite Element Code.<br />
On the Flow Characteristics <strong>of</strong> a Geothermal Plant in a Heterogeneous Subsurface<br />
David Koch, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
Due to the scarcity <strong>of</strong> fossil fuel with a simultaneous rising in global energy demand, it is important<br />
to develop the use <strong>of</strong> other energy sources. Geothermal energy holds great potential, which is<br />
increasingly studied in recent years [1].<br />
The modelling approach <strong>of</strong> the flow processes in a heterogeneous subsurface proceeds from the<br />
Theory <strong>of</strong> Porous Media (TPM) including an elastically deformable solid, an incompressible fluid,<br />
and a gaseous phase [2]. Starting from the gas-filled porous rock, the fluid phase ist introduced<br />
by a borehole. By the rising pressure gradient, the fluid distributes, displaces the gas and escapes<br />
through a second borehole.<br />
To solve the initial-boundary-value problem, the governing primary variables <strong>of</strong> the strongly coupled<br />
three-phase modell are spatially approximated by mixed finite elements, whereas for the<br />
time-discretisation is carried out by an implicit Euler time-integration scheme. The goal <strong>of</strong> the<br />
presented numerical simulations is to study the specific flow characteristics in a heterogenous<br />
subsurface to find the most suitable geologic structures.<br />
[1] R. DiPippo, Geothermal Power Plants: Principles, Applications, Case Studies and Environmental<br />
Impact, Second Edition, Butterworth Heinemann, Oxford 2008.<br />
[2] W. Ehlers, Challenges <strong>of</strong> porous media models in geo- and biomechanical engineering including<br />
electro-chemically active polymers and gels, Int. J. Adv. Eng. Sci. Appl. Math. 1 (2009), 1<br />
– 24.<br />
Multiphase FEM Modelling <strong>of</strong> Infiltration Processes in Cohesionless Soils<br />
Alexander Schaufler, Christian Becker, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
It is well known, that the application <strong>of</strong> a macroscopical hydraulic gradient to a fluid-saturated<br />
cohesionless soil causes seepage flow. Furthermore, the microstructure <strong>of</strong> the porous skeleton<br />
dominates the physics <strong>of</strong> infiltration processes <strong>of</strong> complex fluids (fluid & fines) and thus the<br />
evolution <strong>of</strong> the hydraulic and mechanical properties <strong>of</strong> the soil [1]. From a modelling point <strong>of</strong><br />
view, approaches taking into account the macro- and the micro-scale physics are yet not well<br />
established. The transportation process <strong>of</strong> fines through the pore network strongly depends a)<br />
on the mentioned hydraulic boundary conditions and b) on the microscopic topology <strong>of</strong> the pore
Section 7: Coupled problems 157<br />
space.<br />
The aim <strong>of</strong> this work is to develop a continuum multiphase model to describe infiltration processes<br />
for cohesionless soils. For this purpose, a Representative Volume Element (RVE) is considered and<br />
described by the continuum mixture theory extended by the concept <strong>of</strong> volume fractions (Theory<br />
<strong>of</strong> Porous Media - TPM). The thermodynamically consistent TPM is a macroscopical multiphase<br />
modelling approach, extended from classical single-phase continuum mechanics [2,3].<br />
In the present context, we further extend the concept <strong>of</strong> volume fractions by certain distribution<br />
functions <strong>of</strong> microscopical quantities. Initially, the fluidizable fraction <strong>of</strong> the soil is determined<br />
from the Grain Size Distribution (GSD) curve [4]. Implementing this multi-scale approach into a<br />
Finite Element code, the computational expense <strong>of</strong> the method is one <strong>of</strong> the key points.<br />
The present contribution is focused on a critical study <strong>of</strong> that issue. On the one hand, different<br />
methods for evaluating the GSD are compared. Finally, we discuss a specific approach which<br />
could be used in multiphase FEM models. The resulting numerical model is applied to different<br />
infiltration applications. One specific application <strong>of</strong> the proposed model is situated in mechanized<br />
tunneling. In that case, the infiltration <strong>of</strong> grout in the surrounding soil leads to the evolution <strong>of</strong><br />
hydraulic properties <strong>of</strong> the soil and is finally responsible for deformations on the surface.<br />
[1] Santamarina, J.C., Soils and Waves, John Wiley & Sons Ltd (2001).<br />
[2] Steeb, H., Internal erosion in gas-flow weak conditions, AIP Conf. Series 1227 (2011), 115 –<br />
134.<br />
[3] Ehlers, W., & Bluhm, J., Foundations <strong>of</strong> multiphasic and porous materials. In Porous Media:<br />
Theory, Experiments and Numerical Applications (2002), 3 – 86, Berlin: Springer.<br />
[4] Steeb, H. & Scheuermann, A., Modelling internal erosion: A continuum- based model enriched<br />
by microstructural information, J. Geotech. Geoenviron., under review (2011).<br />
S7.2: Multifield Problems 1: Polymers Tue, 13:30–15:30<br />
Chair: Marc Kamlah S1|03–226<br />
Numerical Modeling <strong>of</strong> Dielectric Elastomer Actuators<br />
Ralf Müller, Markus Klassen (TU Kaiserslautern) Schedule<br />
In modern actuator design the dielectric elastomer is considered as a new actuation material. The<br />
main advantage <strong>of</strong> this dielectric material is the possibility to achieve large deformations under<br />
the influence <strong>of</strong> an electric field. The mechanical deformation is produced by the polarization <strong>of</strong><br />
the elastomer due to the influence <strong>of</strong> the electric field. Since the actuation range <strong>of</strong> dielectric<br />
elastomer actuators (DEAs) is similar the the one <strong>of</strong> natural muscles, one <strong>of</strong> the interesting application<br />
fields is the realization <strong>of</strong> artificial muscles. In the present work the fundamental concepts<br />
for the numerical modeling <strong>of</strong> electromechanical coupled problems are introduced in first place.<br />
After the introduction some concepts <strong>of</strong> the material modeling <strong>of</strong> the elastomer are discussed.<br />
Here the neo-Hooke and the Yeoh model are taken into consideration. Furthermore the issue <strong>of</strong><br />
incompressibility is addressed. Based on these modeling concepts, a numerical study is performed<br />
to investigate the influence <strong>of</strong> microstructural inhomogeneities in the elastomer structure. For this<br />
purpose a capacitor structure consisting <strong>of</strong> a dielectric elastomer between two compliant electrodes<br />
serves as a benchmark. With the help <strong>of</strong> inserting material inhomogeneities in the capacitor<br />
structure the compression behavior is modified. As a final aspect the numerical modeling <strong>of</strong> the
158 Section 7: Coupled problems<br />
dynamics <strong>of</strong> DEAs is presented. Here the focus lies on the study <strong>of</strong> the dynamic behavior <strong>of</strong> DEAs<br />
under the influence <strong>of</strong> an oscillating electric field.<br />
Inverse-motion-based form finding for electro-active polymers<br />
Ralf Denzer (TU Dortmund), Andreas Menzel (TU Dortmund/Lund University) Schedule<br />
Electroactive polymers (EAP) exhibit large mechanical deformation under an applied electrical<br />
field. This electro-mechanical coupling is an attractive property for actuators, e.g., artificial<br />
muscles for micro-robotics. In this presentation we focus on the theoretical and computational<br />
aspects <strong>of</strong> computing the undeformed and load free configuration B0 for a given deformed configuration<br />
Bt and given boundary conditions in the case <strong>of</strong> electro-active polymers. This is <strong>of</strong> practical<br />
interest for the design <strong>of</strong> actuators or grippers. We first formulate the inverse motion problem<br />
for coupled electro-mechanical problems and then show how a straight-forward Bubnov-Galerkin<br />
discretization leads to an attractive simulation scheme to solve such inverse motion problems. We<br />
discuss implementation issues <strong>of</strong> the proposed method and give some numerical results for model<br />
problems.<br />
A three-phase model for polymer curing including diffusive motion and agglomeration<br />
<strong>of</strong> inclusions.<br />
Bernd Lenh<strong>of</strong>, Stefan Diebels (<strong>Universität</strong> des Saarlandes) Schedule<br />
The material properties <strong>of</strong> cured polymers with inclusions <strong>of</strong> different sizes depend strongly on<br />
the location and the size <strong>of</strong> the inclusions. Hence, an appropriate curing model has to take into<br />
account diffusive motion <strong>of</strong> the inclusions. A side effect <strong>of</strong> the relative motion <strong>of</strong> the inclusions<br />
is potentially agglomeration <strong>of</strong> fines and, as an implication, separation <strong>of</strong> agglomerates. Obviously,<br />
diffusion as well as agglomeration/separation are coupled to the curing state <strong>of</strong> the polymer.<br />
In this contribution, only one type <strong>of</strong> inclusion-material is assumed, still, the moving inclusions<br />
may agglomerate. A three-phase continuum model will be shown, where one phase represents the<br />
curing polymer, while the remaining two phases represent the inclusion in the fine state and the<br />
agglomerated state. With respect to the inclusion phases, the model contains not only the diffusion<br />
terms, but also terms modelling phase exchange between the inclusion states. With respect<br />
to the polymer phase, the model includes curing effects. Mixture theory is utilized to formulate<br />
the pertinent time dependent balance equations and the FE-method is used to obtain numerical<br />
solutions. As to the FE-s<strong>of</strong>tware, the equations were implemented into the open-source library<br />
deal.II.<br />
Mechanical behavior <strong>of</strong> a pH-sensitive hydrogel ring used in a micro-optical device<br />
Nicolas Zalachas (Clermont Université), Shengqiang Cai, Zhigang Suo (Harvard University), Yuri<br />
Lapusta (Clermont Université) Schedule<br />
A hydrogel is a polymer network that can absorb a large quantity <strong>of</strong> solvent and swell due to a<br />
physical or chemical stimulus. Hydrogels are more and more used as smart materials in recent<br />
micro-applications. This fact requires the development <strong>of</strong> adequate models and simulation tools<br />
for their large deformation behavior. These models must also predict the onset <strong>of</strong> instabilities,<br />
such as folding or creasing [1]. In this work, we study an interesting application <strong>of</strong> adaptive optical<br />
microsystem [2] using a previously developed theory <strong>of</strong> inhomogeneous large deformation<br />
<strong>of</strong> a pH-sensitive hydrogel [3]. The devices function is based on the swelling <strong>of</strong> a ring made <strong>of</strong><br />
a pH-sensitive hydrogel. The latter controls the focal length <strong>of</strong> the liquid microlens. Our aim is<br />
to analyze major design parameters that affect the hydrogel ring behavior and the function <strong>of</strong><br />
the micro-optical device. The problem is solved numerically with the finite element commercial<br />
s<strong>of</strong>tware ABAQUS. Various modes <strong>of</strong> large deformation and the influence <strong>of</strong> the rings aspect ratio
Section 7: Coupled problems 159<br />
on the behavior <strong>of</strong> the micro-device are investigated. Results show that, for relatively short rings,<br />
a stable swelling takes place. Rings with a relatively big aspect ratio can have an unstable swelling<br />
with the propagation <strong>of</strong> a creasing instability.<br />
[1] W. Hong, X. H. Zhao, Z. G. Suo : Formation <strong>of</strong> creases on the surfaces <strong>of</strong> elastomers and<br />
gels. Applied Physics Letters, 95, 111901 (2009).<br />
[2] L. Dong, A. K. Agarwal, D. J. Beebe, H. R. Jiang : Adaptive liquid microlenses activated by<br />
stimuli responsive hydrogels. Nature, 442, 551-554 (2006).<br />
[3] R. Marcombe, S. Q. Cai, W. Hong, X. H. Zhao, Y. Lapusta and Z. G. Suo : A theory <strong>of</strong><br />
constrained swelling <strong>of</strong> a pH-sensitive hydrogel, S<strong>of</strong>t Matter, 6, 784-793 (2010).<br />
Numerical Modeling and Simulations <strong>of</strong> Dielectric Elastomer Actuators for Thin<br />
Structures<br />
Sandro Zwecker, Sven Klinkel (TU Kaiserslautern) Schedule<br />
The contribution is concerned with a finite element formulation that deals with thin structures<br />
made from dielectric elastomer material. For that a special solid shell formulation, which uses<br />
eight nodes per element and four degrees <strong>of</strong> freedom (three displacements and one for the electric<br />
potential) per node, is presented. It is based on a Hu-Washizu mixed variational principle using<br />
six independent fields: displacements, electric potential, strains, electric field, mechanical stresses,<br />
and dielectric displacements. In recent years structures made from dielectric elastomers have<br />
been investigated by many researchers. This interest is caused by the ability <strong>of</strong> such devices to<br />
efficiently transform electric energy into mechanical work at inexpensive cost <strong>of</strong> production. The<br />
efficiency increases with a higher area to thickness ratio, thus the need to accurately simulate thin<br />
structures is well-founded. On the other hand a 3d description <strong>of</strong> the constitutive behaviour is necessary<br />
to capture all nonlinear effects arising from the material. Thus a 3d constitutive law with<br />
respect to the electro-mechanical coupling incorporated in a finite element solid shell formulation<br />
is presented. Some examples demonstrate how it deals with finite strains and large deformations<br />
<strong>of</strong> thin structures applying electrical loading conditions. The analysed devices respond with<br />
elongation, bending, or buckling, depending on the mode <strong>of</strong> activation. The electrically induced<br />
buckling can be utilized to obtain large deformations.<br />
Modeling <strong>of</strong> healing processes in a polymer matrix<br />
Joachim Bluhm, Jörg Schröder, Steffen Specht (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
Traditionally, engineers are focused to design new materials with increasing durability to ensure<br />
a long lifetime cycle, but they can eventually fail. In contrast, natural materials, e.g. biological<br />
tissues, are dealing with failures in a more efficient way: by self-healing. A material is called selfhealing<br />
material, when it has the ability to recover its strength, stiffness and fracture toughness<br />
after a crack has occurred. One approach to transfer self-healing ability to manufactured materials<br />
is achieved by using a capsule-based healing system. Here, the encapsulated healing agent and<br />
catalyst are embedded in the polymer matrix. If a crack tip brakes through a capsule, the healing<br />
material flows out, polymerized by reaction with the catalyst and close the crack.<br />
In this contribution, for the simulation <strong>of</strong> such a self healing system, a macroscopic multiphase<br />
model based on the Theory <strong>of</strong> Porous Media (TPM) is presented. The healing process <strong>of</strong> the solid<br />
matrix consisting <strong>of</strong> the phases solid, healing material (catalysts, liquid healing and solid healed<br />
materials) and gas (cracks and damaged material). The modeling <strong>of</strong> healing is associated with
160 Section 7: Coupled problems<br />
the formulation criteria regarding the onset <strong>of</strong> the healing process, i.e., the break open <strong>of</strong> the<br />
capsules in connection with the subsequent motion <strong>of</strong> the liquid healing material and change <strong>of</strong><br />
the aggregate state from liquid healing to solid healed material. The transition from the liquid-like<br />
healing material to the solid-like healed material will be captured by introducing mass exchange<br />
between the mentioned constituents. For simplification <strong>of</strong> the model it will be assumed that the<br />
motion <strong>of</strong> solid, healing agents and catalysts as well as the solidified healing-material at a pointed<br />
moment are all equal. Numerical examples will be presented to demonstrate the applicability <strong>of</strong><br />
the model in view <strong>of</strong> the description <strong>of</strong> healing processes.<br />
S7.3: Numerical Solution Methods Tue, 16:00–18:00<br />
Chair: Bernd Markert S1|03–223<br />
A flexible multi-physics coupling interface for partitioned solution approaches<br />
S. Brändli, A. Düster (TU Hamburg-Harburg) Schedule<br />
A common way <strong>of</strong> solving multi-physics problems is the use <strong>of</strong> a partitioned approach. To this end<br />
specialised solvers are utilized for the different subproblems and linked via a common communication<br />
interface. A partitioned approach to be developed should allow to solve different types <strong>of</strong><br />
coupled problems. These might be either volume coupled problems with different physical fields<br />
in one domain or surface coupled problems with different physical fields in different domains.<br />
Examples for these different types <strong>of</strong> coupled problems are thermoelasticity and fluid-structure<br />
interaction (FSI). The use <strong>of</strong> a MPI-library allows for a fast data exchange, whereas special care<br />
has to be taken to perform an accurate interpolation <strong>of</strong> the different fields. In addition one has<br />
to ensure numerical stability and efficiency <strong>of</strong> the coupling algorithm. As a consequence an implicit<br />
algorithm including relaxation-techniques, predictors and convergence criteria is developed<br />
to solve different types <strong>of</strong> coupled problems.<br />
In previous works, FSI problems were solved utilizing a p-FEM solver, which was coupled to a<br />
Lattice Boltzmann Method (LBM) [1] and a Boundary Element Method (BEM) [2]. In [2] also a<br />
FEM-RANSE coupling approach was presented. The interface used in [1,2] for the communication<br />
between the simulation codes was strongly attached to the p-FEM solver. In order to be more<br />
flexible to treat different types <strong>of</strong> coupled problems and to include different simulation codes,<br />
a new coupling interface is designed, which is solver independent and <strong>of</strong>fers the aforementioned<br />
features.<br />
The relaxation techniques to accelerate the convergence <strong>of</strong> the implicit iteration include standard<br />
underrelaxation, Aitken underrelaxation and variants <strong>of</strong> the quasi Newton method. The<br />
flexibility and performance <strong>of</strong> the proposed coupling approach will be demonstrated by different<br />
examples ranging from thermo-mechanical problems to fluid-structure interaction. The emphasis<br />
will be placed on fluid-structure interaction presenting several benchmark examples.<br />
Keywords: FSI, fluid-structure interaction, coupled problems, partitioned approaches, convergence<br />
acceleration<br />
[1] Kollmannsberger S.; Geller S.; Düster A.; Tölke J.; Sorger C.; Krafczyk M.; Rank E.: Fixedgrid<br />
fluid-structure interaction in two dimensions based on a partitioned Lattice Boltzmann<br />
and p-FEM approach. IJNME 79, p. 817ff., 2009.<br />
[2] Brändli S.; Abdel-Maksoud M.; Düster A.: A FEM-BEM approach for Fluid-Structure Interaction.<br />
PAMM Vol. 11, 2011.
Section 7: Coupled problems 161<br />
Stability Analysis <strong>of</strong> Decoupled Solution Strategies for Coupled Multi-field Problems<br />
- A General Framework<br />
Seyedmohammad Zinatbakhsh, Bernd Markert, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
The mathematical modelling <strong>of</strong> coupled problems <strong>of</strong>ten results in systems <strong>of</strong> coupled partial<br />
differential equations (PDE) in space and time, which are usually solved numerically following a<br />
monolithic or decoupled solution algorithm.<br />
Employing an implicit time integration, monolithic schemes result in unconditionally stable numerical<br />
solutions independent <strong>of</strong> the machine accuracy and occurring errors. However, using a<br />
monolithic solver, one considers the coupled problem as a whole, regardless <strong>of</strong> the specialised<br />
solvers that may exist for different subsystems. This has motivated the development <strong>of</strong> various<br />
decoupled solution strategies. However, decoupled integrators can be detrimental to the stability<br />
<strong>of</strong> the solution and must always be accompanied by an exhaustive stability analysis.<br />
The first goal <strong>of</strong> this contribution is to propose a feasible algorithm for the stability analysis <strong>of</strong><br />
this family <strong>of</strong> solutions. The algorithm is used to study the stability behaviour <strong>of</strong> selected volumetrically<br />
and surface-coupled problems in d dimensions, d = {1, 2, 3}. As the first example,<br />
two decoupled solution methods for the linear problem <strong>of</strong> thermo-elastodynamics as presented<br />
in [1] are considered and the influence <strong>of</strong> implicit and explicit predictors on the stability <strong>of</strong> the<br />
solution algorithm is demonstrated. The respective necessary stability condition for 1-d, 2-d and<br />
3-d problems are established. It is shown that using an explicit predictor yields conditional stability<br />
<strong>of</strong> the solution scheme. The coupled problem <strong>of</strong> porous media dynamics serves as the second<br />
example. There, the independence <strong>of</strong> the obtained stability condition for the decoupled solution<br />
scheme proposed in [2] from the permeability factor is investigated. In the last example, the importance<br />
<strong>of</strong> the order <strong>of</strong> integration and its impact on the critical time-step size for the problem<br />
<strong>of</strong> structure-structure interaction (SSI) is studied.<br />
[1] F. Armero, J.C. Simo, A new unconditionally stable fractional step method for non-linear<br />
coupled thermomechanical problems, Int. J. Numer. Meth. Eng. 35 (1992), 737 – 766.<br />
[2] B. Markert, Y. Heider, W. Ehlers, Comparison <strong>of</strong> monolithic and splitting solution schemes<br />
for dynamic porous media problems, Int. J. Numer. Meth. Eng. 82 (2010), 1341 – 1383.<br />
Acceleration <strong>of</strong> partitioned coupling schemes for problems <strong>of</strong> thermoelasticity<br />
P. Erbts, A. Düster (TU Hamburg-Harburg) Schedule<br />
A partitioned coupling scheme for problems <strong>of</strong> thermoelasticity at small strains is presented<br />
utilizing the p-version <strong>of</strong> the finite element method. The coupling between the mechanical and<br />
thermal field is one <strong>of</strong> the most important multi-physics problem. Typically two different strategies<br />
are used to find an accurate solution for both fields: Partitioned or staggered coupling schemes, in<br />
which the mechanics and heat transfer is treated as a single field problem, or a monolithic solution<br />
<strong>of</strong> the full problem. Monolithic formulations have the drawback <strong>of</strong> a non-symmetric system which<br />
may lead to extremely large computational costs. Because partitioned schemes avoid this problem<br />
and allow for numerical formulations which are more flexible, we consider a staggered coupling<br />
algorithm which decouples the mechanical and the thermal field into partitioned symmetric subproblems.<br />
In [1], [2] this algorithmic decoupling has been referred to as the isothermal operatorsplit<br />
methodology.<br />
Since a partitioned coupling algorithm requires fast data exchange, a flexible coupling interface has<br />
been developed which is not restricted only to thermomechanical problems. In order to accelerate
162 Section 7: Coupled problems<br />
the convergence <strong>of</strong> the algorithm, numerical relaxation methods have been implemented. Such<br />
methods are well-known from other multi-physic problems, especially in fluid-structure-interaction<br />
analysis they have been applied with great success. The influence <strong>of</strong> three different relaxation types<br />
are analyzed: Static under-relaxation with constant relaxation coefficients, its dynamic variant<br />
with a residual based relaxation coefficient and a Quasi Newton method.<br />
The numerical solution <strong>of</strong> the thermal and mechanical part is computed by using a high order finite<br />
element code. Several numerical simulations <strong>of</strong> quasi-static problems are presented investigating<br />
the performance <strong>of</strong> accelerated coupling schemes.<br />
Keywords<br />
thermoelasticity, staggered coupling algorithm, convergence acceleration<br />
[1] Miehe C. : Entropic thermoelasticity at finite strains: Aspects <strong>of</strong> the formulation and numercial<br />
implementation. Computer Methods in Applied Mechanics and Engineering, 79:243-269,<br />
1995.<br />
[2] Simo, J.C.; Miehe, C. : Associative coupled thermoplasticity at finite strains: Formulations,<br />
numerical analysis and implementation. Computer Methods in Applied Mechanics and Engineering,<br />
98:41-104, 1992.<br />
A Class <strong>of</strong> Fluid-Structure Interaction Solvers with a Nearly Incompressible Elasticity<br />
Model<br />
Huidong Yang (Johann Radon Institute for Computational and Applied Mathematics) Schedule<br />
In this work, we present some numerical studies on two partitioned fluid-structure interaction solvers:<br />
a preconditioned GMRES solver and a Newton based solver for a class <strong>of</strong> fluid-structure interaction<br />
problems with a nearly incompressible elasticity model in a classical mixed (displacementpressure)<br />
formulation. Both solvers are highly relying on the robust solvers for the structure and<br />
the fluid sub-problems discretized by extended and stabilized finite element methods on hybrid<br />
meshes, for which we use a special class <strong>of</strong> algebraic multigrid solvers.<br />
A finite element contact implementation to investigate rubber friction with themomechanical<br />
coupling effects<br />
Thang Xuan Duong, Roger A. Sauer (RWTH Aachen) Schedule<br />
The knowledge <strong>of</strong> friction when rubber-like material is in contact with a hard material is practically<br />
important for the design and production <strong>of</strong> mechanical parts made <strong>of</strong> rubber, e.g., tires, wiper<br />
blades, seals, etc. In theoretical studies, simple phenomenological friction models, like Coulomb’s<br />
law are usually used to describe the friction behavior. However, for the mechanisms underlying<br />
rubber friction, like mechanical surface interlocking, material hysteresis and adhesion, these<br />
models may fail to predict the results. Thus, our aim is to use numerical experiments with the<br />
structural approach to formulate friction models that can capture such phenomena <strong>of</strong> rubber<br />
friction. In order to do this, coarse-graining techniques can be used to investigate the mechanisms<br />
in detail and to determine their effective behaviors. For this purpose, we provide a framework to<br />
characterize the influence <strong>of</strong> material hysteresis on rough surface friction. The work includes the<br />
implementation <strong>of</strong> a model for 3D finite deformation viscoelastic materials used for rubber-like<br />
materials proposed by S. Reese and S. Govindjee [1], which is valid not only for large deformations<br />
but also large perturbation away from the thermodynamic equilibrium due to the nonlinearity<br />
<strong>of</strong> the evolution equation. For the consideration <strong>of</strong> the thermo-mechanical coupling effects, the
Section 7: Coupled problems 163<br />
thermo-viscoelasticity constitutive model by S. Reese and S. Govindjee [2] is used. The implementation<br />
is then integrated into a suitable finite element formulation solving contact problems<br />
<strong>of</strong> a viscoelastic body on rough surfaces. Energy dissipation across the body, which is important<br />
to determine the internal friction <strong>of</strong> rubber during contact, are computed and visualized. Some<br />
results <strong>of</strong> parametric studies are presented to show the impact <strong>of</strong> relaxation time, normal pressure<br />
and the rough surface parameters on the frictional behavior <strong>of</strong> the rubber material.<br />
[1] S. Reese and S. Govindjee, A theory <strong>of</strong> finite viscoelasticity and numerical aspects, International<br />
Journal <strong>of</strong> Solids and Structures 35 (1998),3455-3482.<br />
[2] S. Reese and S. Govindjee, Theoretical and numerical aspects in the thermo-viscoelastic material<br />
behaviour <strong>of</strong> rubber-like polymers, Mechanics <strong>of</strong> Time-Dependent Materials 1 (1998),<br />
357-396.<br />
Approximate Galerkin method applied to an analysis <strong>of</strong> vibration <strong>of</strong> continuous mechanical<br />
systems<br />
Marek Płaczek (Silesian University <strong>of</strong> Technology) Schedule<br />
Paper presents fundamental assumptions <strong>of</strong> the approximate Galerkin method application in order<br />
to vibration analysis <strong>of</strong> continuous mechanical systems with different form <strong>of</strong> vibration and<br />
different boundary conditions. Flexural vibration <strong>of</strong> beams, longitudinal vibration <strong>of</strong> rods and<br />
torsional vibration <strong>of</strong> shafts with all possible ways <strong>of</strong> fixing were considered. Analyzed mechanical<br />
systems were treated as subsystems <strong>of</strong> mechatronic systems with piezoelectric transducers. This<br />
work was done as an introduction to the analysis <strong>of</strong> mechatronic systems with piezoelectric transducers<br />
used as actuators or passive vibration dampers. It is impossible to use an exact Fourier<br />
method in this case. This is the reason why the approximate Galerkin method was chosen and<br />
analysis <strong>of</strong> its exactness was done as a first step <strong>of</strong> this work. Dynamic flexibilities <strong>of</strong> considered<br />
mechanical systems were calculated twice, using exact and approximate methods. Obtained results<br />
were juxtaposed and it was proved that in some cases the approximate method should be<br />
corrected while in the other it is precise enough. A correction method was proposed and it was<br />
assumed that the approximate method can be used in mechatronic systems analysis.<br />
S7.4: Multifield Problems 2: Electromechanics Tue, 16:00–18:00<br />
Chair: Marc Kamlah S1|03–226<br />
Uncertainty Analysis for Piezoelectric Models<br />
Tom Lahmer (<strong>Universität</strong> Weimar), Jürgen Ilg (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
In the recent years many publications have appeared dealing with the characterization <strong>of</strong> all entries<br />
in the material tensors for the description <strong>of</strong> the piezoelectric effect. The strategies proposed<br />
differ in the methods used and in particular in the type <strong>of</strong> measurements evaluated. Also the<br />
dependency <strong>of</strong> single parameters, e.g., on effects like temperature changes or large-signal loading<br />
are under investigation.<br />
Generally, the approaches are very ambitious, since all parameters shall be identified with highest<br />
accuracy while using a limited number <strong>of</strong> specimens. In particular for less influential parameters<br />
confidence intervals might be large.<br />
It remains unclear, to which extend remaining uncertainties in the parameters influence the response<br />
<strong>of</strong> the model and if these uncertainties are actually critical for the prognosis for which the<br />
model is used for.
164 Section 7: Coupled problems<br />
Therefore, we propose a variance based uncertainty analysis <strong>of</strong> piezoelectric models in order to<br />
identify sources <strong>of</strong> uncertainty and to quantify every parameters influence to the model output.<br />
By considering both, first order and total order effects, interactions between the parameters can<br />
be assessed additionally.<br />
Semi-analytical investigations <strong>of</strong> R-curve behavior in ferroelectric materials considering<br />
different scales<br />
Roman Gellmann, Andreas Ricoeur (<strong>Universität</strong> Kassel) Schedule<br />
Due to the brittleness <strong>of</strong> ferroelectric materials fracture mechanical approaches are playing an essential<br />
role in the modern research. The strength <strong>of</strong> these materials, in terms <strong>of</strong> the critical stress<br />
intensity factors, is significantly determined by nonlinear ferroic effects arising on the mesoscopic<br />
scale.<br />
In the present work we study the effective fracture toughness <strong>of</strong> ferroelectrics by taking the mesoscopic<br />
as well as the macroscopic level into account. On the macroscopic scale we apply an<br />
extended theory <strong>of</strong> stresses at interfaces in dielectric solids [1]. Further, on the mesoscopic scale,<br />
nonlinear effects are introduced by applying the small scale switching approximation, i.e. the effects<br />
are limited to a small region around the crack tip. Finally, we discuss the effective fracture<br />
toughness and crack resistance curves for different loading and poling conditions. The analysis<br />
is done considering the full anisotropy and electromechanical coupling <strong>of</strong> the material by using<br />
piezoelectric weight functions [2]. In contrast to previous approaches, the presented model also<br />
takes the inverse switching (180 degree) into account yielding a contribution to the electric<br />
displacement intensity factor.<br />
[1] R. Gellmann, A. Ricoeur, Arch. Appl. Mech., 2011<br />
[2] R. McMeeking, A. Ricoeur, Int. J. Solids Struct., 2003<br />
A micromechanically motivated method to develop switching surfaces in ferroelectroelasticity<br />
Sebastian Stark, Peter Neumeister, Herbert Balke (TU Dresden) Schedule<br />
Macroscopic phenomenological models are widely used to predict the irreversible material behaviour<br />
<strong>of</strong> polycristalline ferroelectroelastic ceramics under electromechanical loading conditions.<br />
Usually, these models are based upon a thermodynamically consistent continuum mechanics framework<br />
involving the choice <strong>of</strong> a switching surface, which separates the domains <strong>of</strong> reversible and<br />
irreversible material behaviour. The switching surfaces proposed in the literature are typically<br />
suitable to represent the material behaviour found in experiments for simple loading conditions,<br />
such as bipolar electric cycling and uniaxial compression. However, their predictive capabilities<br />
in the case <strong>of</strong> complex, electromechanical loadings are not satisfactory yet. Therefore, a better<br />
understanding <strong>of</strong> the properties <strong>of</strong> switching surfaces is desirable. In this talk, a micromechanically<br />
motivated method to develop switching surfaces is proposed and applied to predict the<br />
shape <strong>of</strong> the initial switching surface <strong>of</strong> a virgin ceramic. The approach is based upon energetic<br />
considerations leading to maximum dissipation. The results obtained are discussed with respect<br />
to the electromechanical generalisation <strong>of</strong> the Tresca and von Mises yielding surfaces known<br />
from metal plasticity. Furthermore, a comparison to experimental results is given, showing that<br />
the presented approach is appropriate to describe the onset <strong>of</strong> switching under proportional electromechanical<br />
loading.<br />
On the released energy in nonlinear electro-elastostatics<br />
Duc Khoi Vu, Paul Steinmann (<strong>Universität</strong> Erlangen-Nürnberg) Schedule
Section 7: Coupled problems 165<br />
In this work the change <strong>of</strong> energy under a change <strong>of</strong> material configuration <strong>of</strong> an electro-sensitive<br />
body subjected to electric stimulations is considered by taking into account the free space surrounding<br />
the body. The free space can have a significant impact on the electric field and on the<br />
deformation field inside a body made <strong>of</strong> materials with low electric permittivity like the so-called<br />
electronic electroactive polymers (EEAPs). By using a stored energy density function for both<br />
the material body and the free space, the formulas for the part <strong>of</strong> energy that is released from<br />
the system material body - applied forces in response to a change in the material configuration<br />
are formulated. These formulas are useful in the study <strong>of</strong> defects like crack propagation.<br />
Dynamic response <strong>of</strong> dielectric elastomer actuators with the sandwich structure<br />
Bai-Xiang Xu (TU <strong>Darmstadt</strong>), Anika Theis, Markus Klassen, Ralf Mueller (TU Kaiserslautern),<br />
Dietmar Gross (TU <strong>Darmstadt</strong>) Schedule<br />
As potential material for artificial muscles and haptic displays, dielectric elastomer provides large<br />
deformations with lower cost and high efficiency. The material behaves nonlinearly in both the<br />
geometry and the constitutive relation. The nonlinear modeling and simulation <strong>of</strong> the material<br />
in the static case has received considerable investigation. However, the material is mostly expected<br />
to perform under dynamic situations in applications with high frequencies, e.g. pumps and<br />
loudspeakers. Therefore the modeling <strong>of</strong> the dynamic response <strong>of</strong> the dielectric elastomer is also<br />
<strong>of</strong> importance.<br />
In this work, a theoretical model is proposed to study the dynamic behavior <strong>of</strong> a dielectric<br />
elastomer actuator with a standard sandwich structure. The nonlinear equation <strong>of</strong> motion can<br />
be obtained through the Euler-Langrange equation or a variational analysis. Unlike in most <strong>of</strong><br />
the cases studied in the literature, the ordinary differential equation for the motion involves<br />
additionally the first time derivative <strong>of</strong> the deformation, due to the exact formulation <strong>of</strong> the kinetic<br />
energy in space. Numerical solutions for exemplary cases will be presented, i.e. the vibration under<br />
a constant potential and the forced oscillation under harmonic excitation. In particular, resonance<br />
phenomenon and damping effects are investigated. Results will be discussed in comparison with<br />
those <strong>of</strong> the related topics in the literature.<br />
S7.5: Phase Change and Interface Problems Wed, 13:30–15:30<br />
Chair: Bernd Markert S1|03–226<br />
Modeling and simulation <strong>of</strong> binary and ternary reactive systems<br />
Kerstin Weinberg, Denis Anders (<strong>Universität</strong> Siegen) Schedule<br />
For the production and design <strong>of</strong> functional materials reaction-diffusion systems gain more and<br />
more importance.<br />
In this contribution the spinodal decomposition in multicomponent systems subjected to chemical<br />
reactions is studied. To this end, the classical Cahn-Hilliard phase field model is extended<br />
by additional contributions accounting for chemical reactions. After a thorough derivation <strong>of</strong> the<br />
reaction-diffusion model in a thermodynamically consistent way, numerical simulations <strong>of</strong> binary<br />
and ternary chemically reactive phase separating systems are presented.<br />
Finite element methods for solid-liquid phase transitions with free melt surface<br />
Mischa Jahn, Andreas Luttmann, Alfred Schmidt (<strong>Universität</strong> Bremen), Jordi Paul (<strong>Universität</strong><br />
Erlangen) Schedule<br />
The modelling and computation for a problem with solid-liquid phase transition and a free boundary<br />
surface will be discussed. The main components <strong>of</strong> the used model are heat conduction, a<br />
moving phase boundary, and its coupling with the Navier-Stokes equations.
166 Section 7: Coupled problems<br />
We present FE methods using two different approaches for the phase boundary, namely a<br />
sharp interface with moved mesh, and an energy conservation based approach with mushy-region<br />
elements. By combining both methods in a proper way, we benefit from the advantages <strong>of</strong> the<br />
respective approach.<br />
The methods are applied to the accumulation <strong>of</strong> material by melting the tip <strong>of</strong> thin steel wires<br />
using laser heating. The beneficial ratio <strong>of</strong> surface tension and gravity enables the generation <strong>of</strong><br />
functional parts in micro scale metallic components. Simulation and experimental results will be<br />
presented.<br />
Carbon-dioxide storage and phase transitions: towards an understanding <strong>of</strong> crack<br />
development in the cap-rock layer<br />
Kai Häberle, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
Supercritical CO2 can be injected into deep saline aquifers to reduce the amount <strong>of</strong> CO2 in the<br />
atmosphere and thus, lessen the impact on the global warming. Qualified reservoirs should be in a<br />
sufficient depth to guarantee the thermodynamical environment for the supercritical state <strong>of</strong> CO2<br />
and should be confined by an impermeable cap-rock layer. It is crucial to guarantee the safety<br />
<strong>of</strong> the storage site. Therefore, deformation processes and crack development <strong>of</strong> the rock matrix<br />
and the cap-rock layer, which might be induced by the high pressure injection <strong>of</strong> CO2, must be<br />
investigated. If cracks occur, CO2 could migrate into shallower regions, where the temperature and<br />
pressure cannot support the supercritical condition <strong>of</strong> the CO2 anymore. Thus, it is important to<br />
describe the phase transition process between supercritical, liquid and gaseous CO2. The Theory<br />
<strong>of</strong> Porous Media (TPM), see e. g. [1], provides a useful continuum-mechanical basis to describe<br />
real natural systems in a thermodynamically consistent way. Hence, the TPM is applied to model<br />
multiphasic flow <strong>of</strong> CO2 and water and include elasto-plastic solid deformations <strong>of</strong> the porous<br />
matrix. The Peng-Robinson equation, e. g. [2], is implemented as a cubic equation <strong>of</strong> state to<br />
describe the phase behaviour <strong>of</strong> CO2. However, the two-phase region cannot be represented by a<br />
continuously differentiable function such as the Peng-Robinson equation and thus, the Antoine<br />
equation provides additional information <strong>of</strong> the vapourisation curve. The extended Finite Element<br />
Method (XFEM) will be used to account for the discontinuities arising from crack development<br />
due to solid deformations [3]. Herein, special attention has to be paid to the matrix-fracture<br />
interaction <strong>of</strong> the fluid phases. Numerical examples are performed to investigate the injection<br />
<strong>of</strong> CO2 into a saline aquifer. These are computed with the FE program PANDAS, which allows<br />
solutions <strong>of</strong> strongly coupled multiphasic problems in deformable porous media.<br />
[1] W. Ehlers, Foundations <strong>of</strong> multiphasic and porous materials, in: W. Ehlers and J. Bluhm<br />
(eds.), Porous Media: Theory, Experiments and Numerical Applications. Springer-Verlag,<br />
Berlin 2002, pp. 3 – 86.<br />
[2] B. Poling, J. Prausnitz, J. O’Connell, The properties <strong>of</strong> gases and liquids, McGraw-Hill. New<br />
York 2001, 5th edn.<br />
[3] N. Moës, J. Dolbow, T. Belytschko, A finite element method for crack growth without remeshing,<br />
Int. J. Numer. Meth. Eng. 4 (1999), pp. 131 – 150.<br />
Phase Transition in Methane Oxidation Layers - A Coupled FE Multiphase Description<br />
Andrea Sindern, Tim Ricken (TU Dortmund), Renatus Widmann, Martin Denecke (<strong>Universität</strong><br />
Duisburg-Essen) Schedule
Section 7: Coupled problems 167<br />
Worldwide, the most common sites <strong>of</strong> waste disposal are landfills. After solid waste is deposited in<br />
a landfill, physical, chemical, and biological processes ensue and modify the waste. Due to these<br />
reactions, landfill gas is produced inside the landfill body and effuses into the atmosphere at the<br />
outer layer. These processes create environmentally harmful landfill pollutants (methane (CH4))<br />
and carbon dioxide (CO2)). The impact <strong>of</strong> methane on the greenhouse effect is actually 21 - 23<br />
times higher than that <strong>of</strong> carbon dioxide.<br />
In order to estimate potential environmental risk, a second important phenomenon has to be<br />
taken into account: the bacterial methane conversion in the porous cover layer which significantly<br />
reduces the amount <strong>of</strong> methane emitted into the atmosphere. Subsequently, the metabolism <strong>of</strong><br />
different methanotrophic bacteria converts methane and oxygen into carbon dioxide, water, and<br />
biomass.<br />
To model this highly complex and coupled problem we used the well-known theory <strong>of</strong> porous media<br />
to obtain a thermodynamically consistent description which in turn leads to a fully-coupled<br />
finite element (FE) calculation concept. In this talk, the theoretical and numerical framework will<br />
be presented in order to describe the coupled processes occurring during the phase transition by<br />
bacterial activity in the methane oxidation layer. The model analyzes the relevant gas concentrations<br />
<strong>of</strong> methane, carbon dioxide, oxygen, and nitrogen as well as the driving phenomena <strong>of</strong><br />
production, diffusion, and convection. Based on a model predicting gas production in landfills, see<br />
[1,2], a multiphase continuum approach for landfill cover layers is presented. In order to validate<br />
the model, we compare numerical simulations with experimental data.<br />
Acknowledgement: This work was supported by the DFG (Grant No. RI 1202/3-1)<br />
[1] Ricken, T. and Ustohalova, V.: Computational Materials Science, Vol. 32, pp. 498–508, (2005).<br />
[2] Robeck, M. et al.: Waste Management, Vol. 31, pp. 663–669, (2011).<br />
Macroscopic modelling <strong>of</strong> the selective beam melting process<br />
D. Riedlbauer, J. Mergheim, A. McBride, P. Steinmann (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
The selective beam melting process is used for the additive manufacturing <strong>of</strong> three-dimensional<br />
components from particulate media. The component is formed by scanning the beam (electron<br />
or laser) over successively deposited layers. The intense energy imparted by the beam causes<br />
the particles to undergo an irreversible phase change from a powder to a melt and then to a<br />
solid. The accuracy <strong>of</strong> the process is dependent upon numerous parameters (e.g. beam scan path,<br />
rate <strong>of</strong> cooling). Computational modelling can assist the design procedure by providing a virtual<br />
environment in which to test a huge range <strong>of</strong> parameters. The applicability <strong>of</strong> the model is in<br />
turn dependent on its ability to capture the key physical processes such as: the dependence <strong>of</strong> the<br />
material properties on the temperature, the coupling <strong>of</strong> thermal and mechanical processes, and<br />
the phase changes which occur.<br />
The objective here is to detail a thermodynamically consistent continuum model for thermoelasticity<br />
to describe selective beam melting. The implementation <strong>of</strong> the model within the<br />
open-source finite element library deal.ii [2] is also described. In particular, a comparison <strong>of</strong> the<br />
fractional split method [1] and the monolithic approach is presented. In order to accurately describe<br />
the boundary <strong>of</strong> the solid region, an adaptive finite element strategy is adopted.<br />
The accuracy and efficiency <strong>of</strong> the model is demonstrated via a series <strong>of</strong> benchmark problems.<br />
[1] Armero, F., Simo, J. C., 1992. A new unconditionally stable fractional step method for nonlinear<br />
coupled thermomechanical problems. International Journal for Numerical Methods<br />
In Engineering 35, 737–766.
168 Section 7: Coupled problems<br />
[2] Bangerth, W., Hartmann, R., Kanschat, G., 2007. deal.II — a general purpose object oriented<br />
finite element library. ACM Transactions on Mathematical S<strong>of</strong>tware 33 (4), 24.<br />
S7.6: Multifield Problems 3: Magnetomechanics Wed, 16:00–18:00<br />
Chair: Marc Kamlah S1|03–226<br />
Numerical Aspects <strong>of</strong> Three-Dimensional MSMA Modeling<br />
B. Kiefer, T. Bartel, A. Menzel (TU Dortmund) Schedule<br />
Magnetic shape memory alloys (MSMA) exhibit a complex constitutive behavior that combines<br />
the nonlinear, dissipative and thermomechanically-coupled features <strong>of</strong> classical shape memory<br />
response with strong magneto-mechanical coupling. The magnetic shape memory effect is made<br />
possible by the simultaneous occurrence <strong>of</strong> high magnetic anisotropy and high twin boundary<br />
mobility that allows the field-induced reorientation <strong>of</strong> variants in the ferromagnetic martensite<br />
phase.<br />
Several constitutive models for MSMAs have been proposed in the literature. What is missing,<br />
however, are numerical integration schemes for such models that capture the complex multidimensional<br />
thermo-magneto-mechanical behavior <strong>of</strong> MSMAs and can be implemented into finite<br />
element codes solving the coupled field equations. In this work, two main algorithmic versions <strong>of</strong><br />
the Kiefer & Lagoudas internal variable model for MSMAs [1] are presented. The more classical<br />
approach is based on a predictor-corrector-type return mapping scheme. The second approach<br />
employs so-called Fisher-Burmeister NCP functions to avoid the undesired necessity to evaluate<br />
multiple sets <strong>of</strong> Karush-Kuhn-Tucker conditions (cf. [2], or [3] in the context <strong>of</strong> phase transformations).<br />
Starting from the simplest form <strong>of</strong> the MSMA model in which only field-induced martensitic<br />
variant reorientation is considered, the macroscopic phenomenological model is extended to include<br />
the local magnetization rotation and magnetic domain wall motion mechanisms, through the<br />
evolution <strong>of</strong> additional internal state variables. Special attention is paid to three-dimensional response<br />
modeling, in which additional martensitic variants must be considered. Finally, FE-based<br />
simulations <strong>of</strong> the coupled global response are discussed.<br />
[1] B. Kiefer and D. C. Lagoudas, Modeling the Coupled Strain and Magnetization Response <strong>of</strong><br />
Magnetic Shape Memory Alloys under Magnetomechanical Loading, Journal <strong>of</strong> Intelligent<br />
Material Systems and Structures Vol. 20, 143–170, 2009.<br />
[2] A. Fischer, A Special Newton-Type Optimization Method, Optimization Vol. 24, 269–284,<br />
1992.<br />
[3] T. Bartel and K. Hackl, A Micromechanical Model for Martensitic Phase-Transformations in<br />
Shape-Memory Alloys Based on Energy-Relaxation, Zeitschrift für Angewandte Mathematik<br />
und Mechanik Vol. 89, 792–809, 2009.<br />
XFEM-modelling <strong>of</strong> stationary magnetic and coupled magneto-mechanical boundary<br />
value problems<br />
J. Goldmann, C. Spieler, M. Kästner, V. Ulbricht (TU Dresden) Schedule<br />
The goal <strong>of</strong> this work is to analyse a composite material with magnetically switchable stiffness<br />
properties. To this end, the coupling between the magnetic and the mechanical field has to be
Section 7: Coupled problems 169<br />
considered. This presentation features one step towards the long-time objective <strong>of</strong> predicting the<br />
effective behavior <strong>of</strong> the composite using a homogenisation algorithm.<br />
The magnetic problem here is reduced to magnetostatics, allowing for a weak coupling <strong>of</strong><br />
magnetic and mechanical fields, thus both boundary value problems may be solved separately.<br />
At first the stationary magnetic field is computed in terms <strong>of</strong> the magnetic vector potential. The<br />
existing jumps <strong>of</strong> the magnetic field quantities across material interfaces cause a non vanishing<br />
force distribution at the interface. This traction at the interface is obtained by a total stress tensor<br />
split into an electromagnetic and a mechanical part according to [1]. The calculated nodal forces<br />
are then transferred to the structural pass.<br />
The numerical solution <strong>of</strong> the coupled field problem is performed using the eXtended Finite<br />
Element Method (XFEM). Over the past decade XFEM has been applied to a variety <strong>of</strong> mechanical<br />
and non-mechanical problems involving weak and strong discontinuities [2]. Still magnetic<br />
problems have not been considered in lots <strong>of</strong> publications. Therefor special attention will be paid<br />
to the magnetic calculation and the coupling. To this end two demostration problems featuring<br />
resulting concentrated loads as well as distributed loads will be presented. The numerical solutions<br />
will be analysed using known analytical solutions. In this context different types <strong>of</strong> elements<br />
will be compared.<br />
[1] Eringen, A. C.; Maugin, G. A. Electrodynamics <strong>of</strong> continua, Springer, New York, 1990<br />
[2] Fries, T.-P.; Belytschko, T. The extended/generalized finite element method: An overview <strong>of</strong><br />
the method and its applications, Int. J. Numer. Meth. Engng 84 (2010), 253–304<br />
Effects <strong>of</strong> different crack-face boundary conditions on the dynamic intensity factors<br />
in linear magnetoelectroelastic solids<br />
Michael Wünsche, Chuanzeng Zhang (<strong>Universität</strong> Siegen) Schedule<br />
Keywords: magnetoelectroelastic materials, non-linear crack-face boundary conditions, impact<br />
loading, dynamic intensity factors<br />
New multifield materials for the development <strong>of</strong> smart devices and structures are receiving<br />
increasing attentions. Composite materials consisting <strong>of</strong> piezoelectric and piezomagnetic phases<br />
with an additional magnetoelectric coupling effect <strong>of</strong>fer advanced opportunities and may be used<br />
for broadband sensing, actuating devices and many other smart devices and structures which are<br />
required in engineering sciences. Static and dynamic crack analysis <strong>of</strong> magnetoelectroelastic solids<br />
is <strong>of</strong> special importance because such solids are <strong>of</strong>ten very brittle and the corresponding results<br />
have a direct relevance to the design and optimization <strong>of</strong> real structures. Since analytical solutions<br />
are usually limited to very simple crack and loading configurations, numerical solution algorithms<br />
have to be used in general cases. The boundary element method (BEM) has been shown to be very<br />
attractive and efficient for solving dynamic crack problems in linear magnetoelectroelastic solids.<br />
A critical issue in the numerical simulation <strong>of</strong> crack problems in linear magnetoelectroelastic solids<br />
is a realistic description <strong>of</strong> the mechanical and electromagnetical crack-face boundary conditions.<br />
The aim <strong>of</strong> this paper is the investigation <strong>of</strong> different electrical, magnetic and mechanical crackface<br />
boundary conditions and their influences on the static and dynamic intensity factors in twodimensional<br />
and linear magnetoelectroelastic solids subjected to different mechanical, electrical,<br />
magnetic and combined loadings. Iterative algorithms are developed to handle the semi-permeable<br />
electrical and magnetic crack-face boundary conditions. To solve the non-linear crack-face contact
170 Section 7: Coupled problems<br />
problem when a physically unacceptable crack-face intersection occurs, an additional iterative<br />
scheme is implemented. Numerical examples will be presented and discussed.<br />
Geometrical Aspects in the Incremental Variational Formulation for Phase Field<br />
Modeling in Micromagnetics<br />
Gautam Ethiraj, Christian Miehe (<strong>Universität</strong> Stuttgart) Schedule<br />
Magnetic materials have been finding increasingly wide areas <strong>of</strong> application in industry ranging<br />
from magnetic cores <strong>of</strong> transformers, motors, inductors, generators to high density magnetic recording<br />
devices. There is therefore an increased interest in the modeling <strong>of</strong> such materials that<br />
have an inherent coupling between the magnetic and mechanical characteristics. In a previous<br />
work we presented a phase field model within an incremental variational framework to describe<br />
the formation and quasi-static evolution <strong>of</strong> magnetic domains. Such a model incorporates characteristic<br />
size-effects that are observed and reported in literature. The associated time evolution<br />
arising from this incremental potential is shown to be consistent with the Landau-Lifschitz equation,<br />
containing the damping term <strong>of</strong> the Landau-Lifschitz-Gilbert equation to describe the time<br />
evolution <strong>of</strong> the magnetization. A particular challenge in the modeling <strong>of</strong> such materials is the<br />
algorithmic preservation <strong>of</strong> the geometric constraint on the magnetization director field, that remains<br />
constant in magnitude. We presented a novel finite element formulation for the treatment<br />
<strong>of</strong> the variational-based, symmetric three-field problem, considering the mechanical displacement,<br />
the magnetization director, and the magnetic potential induced by the magnetization as the<br />
primary fields where the geometric property <strong>of</strong> the magnetization director is exactly preserved<br />
pointwise by nonlinear rotational updates at the nodes. In the current work however, we present an<br />
alternative approach that involves a standard finite element solution followed by a projection step<br />
for the magnetization vector. This method has provides significant advantages in terms <strong>of</strong> speed<br />
and ease <strong>of</strong> implementation at the cost <strong>of</strong> some drawbacks. The current work therefore presents<br />
comparative study <strong>of</strong> the the two methods by means <strong>of</strong> a spectrum <strong>of</strong> benchmark problems.<br />
S7.7: Surface-Coupled Problems Thu, 13:30–15:30<br />
Chair: Thomas-Peter Fries, Ralf Müller S1|03–226<br />
Fluid-Structure-Interaction-Analysis concerning Damping Features <strong>of</strong> Viscous Fluids<br />
Vilmar Fuchs, Olaf Wünsch (<strong>Universität</strong> Kassel) Schedule<br />
Fluid-Structure-Interaction (FSI) concerning technological constructions on sea are becoming very<br />
important in view <strong>of</strong> growing consumption <strong>of</strong> renewable energy sources. Sea constructions like<br />
<strong>of</strong>fshore wind farms are exposed to extreme weather conditions due to sea storms which cause<br />
enormous loads by wind and waves. In the long term these exposures may lead to serious damage<br />
<strong>of</strong> the load-bearing piles. On that account this work deals with the damping characteristics <strong>of</strong><br />
viscous liquids which are determined to protect the structure. We modeled a damping element<br />
prototype consisting essentially <strong>of</strong> an elastic cover that is attached to the cylindrical mono pile<br />
foundation at a height <strong>of</strong> waves. The chamber between the flexible structure and the mono pile<br />
is filled with a viscous fluid. The damping element has been constructed as a test object in the<br />
laboratory scale in a water channel. In order to measure the hydrodynamic loads on the test object,<br />
we placed 16 piezoelectric sensors on the stagnation point <strong>of</strong> the mono pile. The experiments<br />
<strong>of</strong> the interaction process <strong>of</strong> wave loads on the damping element are set up to determinate the<br />
damping influence <strong>of</strong> fluids with different viscosity. Within the framework <strong>of</strong> FSI the impact <strong>of</strong><br />
breaking waves on a three-dimensional model <strong>of</strong> a damping element prototype corresponding to<br />
[1] is simulated. In order to measure the influence <strong>of</strong> different liquid properties on the damping <strong>of</strong>
Section 7: Coupled problems 171<br />
the impact, the calculations are set up using newtonian and non-newtonian fluids with varying<br />
viscosity. The newtonian results are compared with experiments showing good agreements. For<br />
the non-newtonian investigation verification is carried out with a CFD model.<br />
[1] V. Fuchs, O. Wünsch, Numerical Simulation <strong>of</strong> Free Surface-Structure-Interaction with Multi-<br />
Regional Mesh Deformation, accepted proceeding PAMM (2011).<br />
Numerical simulations <strong>of</strong> dense fluid-particle flows using computational fluid (CFD)<br />
dynamics and discrete element method (DEM)<br />
N. Iqbal, C. Rauh, A. Delgado (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
Particle loaded flows are <strong>of</strong> significant importance in various industrial applications including<br />
chemicals, fertilizers and energy processes.With the increase <strong>of</strong> computational capacity, it has<br />
become possible to simulate such flows with a reasonable complexity level such as flow pattern,<br />
particle tracking and reaction kinematics as well. There are two basic approaches to model particleladen<br />
flows: namely Eulerian-Eulerian (two-fluid models) and Eulerian-Lagrangian. In this work<br />
the later that is also known as CFD-DEM approach is used. Fluid phase is modelled using<br />
continuum approach considering transient, compressible and turbulent nature <strong>of</strong> the flow and<br />
particles are modelled with Lagrangian approach. Generally in this approach for dilute complex<br />
flows the particle tracking is simulated using Lagrangian approach and particle-particle interaction<br />
is neglected. That is not appropriate in dense flows as the collision phenomena have prevailing<br />
effects on the formation and evolution <strong>of</strong> heterogeneous structures. In current study, the particle<br />
tracking as well as particle-particle interactions are taken into account. This model is capable <strong>of</strong><br />
simulating flows with a wide range <strong>of</strong> particulate void fractions. Momentum exchange between the<br />
phases is modelled by combining the well-known Ergun’s equation and Wen and Yu relation. These<br />
relations are used by several researchers [1,2]. Collision forces between particles are calculated<br />
using s<strong>of</strong>t sphere model (spring, slider and dashpot model).<br />
The framework <strong>of</strong> OpenFOAM an open source CFD simulation code is used. In the current<br />
study, fluidized bed simulation is considered. The coupled mass and momentum balance equations<br />
are used to calculate the flow behavior, particle fluidization and bubble formation. The dimensions<br />
<strong>of</strong> the simulation domain are similar to Link et al. (2005)but with different stiffness <strong>of</strong> particles.<br />
The higher velocity <strong>of</strong> fluid relative to particles entering through a jet causes the particles to<br />
fluidize. The particles behavior, fluidization, bubble formation and the velocity vectors <strong>of</strong> particles<br />
show a good agreement with the literature. The results are compared with the two-fluid model<br />
(TFM) that clearly shows that the DEM based model captures the heterogeneous structure in<br />
more detail than the TFM. The quantitative comparison is planned in near future. Preliminary<br />
work on simulations with heat transfer between the phases and chemical reactions is also done.<br />
[1] Y. Tsuji, T. Kawaguchi and T. Tanaka: Discrete particle simulation <strong>of</strong> two-dimensional fluidized<br />
bed. Powder Technology, 77 (1993) 79-87.<br />
[2] J.M. Link, L.A. Cuypers, N.G. Deen, J.A.M. Kuipers: Flow regimes in a spout-fluid bed:<br />
A combined experimental and simulation study. Chemical Engineering Science 60 (2005)<br />
3425-3442<br />
Simulation <strong>of</strong> the elastohydrodynamic contact with a piezo-viscous fluid<br />
Thomas Leitz, K. Willner (<strong>Universität</strong> Erlangen-Nürnberg) Schedule
172 Section 7: Coupled problems<br />
For the purpose <strong>of</strong> simulating the lubrication in bush bearings, the Reynolds equations, derived<br />
from the Navier-Stokes equations, are widely accepted to be suitable. Since high pressures have<br />
an impact both on the viscosity <strong>of</strong> the fluid as well as causing an elasic deformation <strong>of</strong> the<br />
boundary surface, a piezo viscous model and an elasto-hydrodynamic model have been included<br />
as an extension <strong>of</strong> the purely isoviscous model.<br />
First a numerical solution based on the finite element method for the simple model consisting<br />
<strong>of</strong> purely isoviscous flow bounded by rigid surfaces and being described by the 2D Reynolds equations<br />
will be presented. A comparison <strong>of</strong> the numerical results to the analytical solution <strong>of</strong> the<br />
Reynolds equations verifies the implementation. Secondly the coupling with two different models<br />
for piezo viscosity, namely Barus and Roelands, has been investigated. Furthermore, to allow<br />
elastic deformation <strong>of</strong> the surfaces, an elasto-hydrodynamic coupling based on a halfspace model<br />
for the displacements has been included into the implementation. Combining the methods for<br />
simulating piezo viscosity and elastic deformation, we expect to obtain more realistic simulations<br />
<strong>of</strong> the lubrication in bush bearings.<br />
Analysis and Modeling <strong>of</strong> the Hydro-Mechanics <strong>of</strong> Deformable Fractures<br />
Carlo Vinci, Jörg Renner, Holger Steeb (<strong>Universität</strong> Bochum) Schedule<br />
High pressure fluid injection into rock formations, e.g. hydraulic fracturing <strong>of</strong> reservoir rocks,<br />
causes several coupled physical phenomena in the rock and in the fluid. In the present contribution,<br />
we investigate and model the flow <strong>of</strong> a viscous fluid into a single deformable fracture and<br />
the associated elastic deformation <strong>of</strong> the surrounding porous rock. In fact, fluid injection into a<br />
fractured porous rock causes deformation, in particular dilatation, <strong>of</strong> existing fractures affecting<br />
their hydraulic properties and generally leading to an increase <strong>of</strong> the effective permeability <strong>of</strong> the<br />
rock. Otherwise, the elastic crack deformation influences the current pressure distribution in the<br />
fracture, and, therefore, the diffusion process <strong>of</strong> the pore fluid in the joint. A deep and detailed<br />
understanding <strong>of</strong> the coupling between fluid pressure diffusion and elastic deformation is needed<br />
in order to model the infiltration process <strong>of</strong> a viscous fluid into a single fracture.<br />
Despite the substantial number <strong>of</strong> previous modeling approaches, a clear insight into the numerical<br />
solution procedure <strong>of</strong> high pressure fluid injection in a fracture has not been gained. Therefore, we<br />
present numerical solution strategies to solve the system <strong>of</strong> a single joint in a porous rock matrix.<br />
Due to the coupled nature <strong>of</strong> the problem, conceptually and technically different strategies have<br />
be applied to model and solve the resulting hydro-mechanical system. We use different staggered<br />
finite element-based solution schemes and compare them to a fully coupled one. The latter is<br />
based on Biots quasi-static poroelastic equations. Rather than relying on a heuristic formulation<br />
<strong>of</strong> the associated diffusion equation, we derive this from the conservation <strong>of</strong> mass avoiding any<br />
<strong>of</strong> the frequently used approximations or simplifications. The physically-based model takes into<br />
account the roles <strong>of</strong> non-linear diffusion <strong>of</strong> the fluid and elastic rock deformation during pumping<br />
operations in boreholes.<br />
We compare and critically discuss the results obtained with the two explored solution approaches.<br />
This information provides an improved understanding <strong>of</strong> physical phenomena accompanying the<br />
hydraulic part and the mechanical response and thus builds the basis for more complex multi-joint<br />
hydraulic fracturing investigations on larger scale.<br />
Numerical Simulation <strong>of</strong> organic binder decomposition and combined seepage- and<br />
diffusive transport <strong>of</strong> the gaseous reaction products through a porous green body<br />
during thermal debinding <strong>of</strong> ceramic parts.<br />
I. Schmidt, H. Riedel (Fraunh<strong>of</strong>er Institut für Werkst<strong>of</strong>fmechanik, Freiburg), J. Svoboda (Czech<br />
Academy <strong>of</strong> Sciences Brno) Schedule
Section 7: Coupled problems 173<br />
In the powder technological production <strong>of</strong> ceramic parts, organic additives are admixed to the<br />
ceramic powder so as to give the green part strength and/or facilitate the compaction. Before the<br />
part is sintered to obtain its final strength and shape, these additives have to be removed from<br />
the green body, e.g. by a thermal debinding process. During this process, the binder undergoes<br />
thermal decomposition into gaseous reaction products which subsequently have to be transported<br />
to the surface through the pore channels. Depending on the heating rate and the green bodys<br />
permeability, a pressure develops inside the body, creating, in turn, stresses in the solid skeleton<br />
which can cause damage. The paper presents a model which describes the chemical decomposition<br />
<strong>of</strong> organic binders, the combined Maxwell-Stefan and Knudsen diffusion and the seepage<br />
flow <strong>of</strong> multiple gaseous reaction products through a porous body and the implementation <strong>of</strong> the<br />
model into a finite element framework. Special attention is paid to the correct formulation and<br />
implementation <strong>of</strong> Robin-type boundary conditions for the multi-component diffusion problem.<br />
Results are presented for a prototype problem, including the computation <strong>of</strong> the solid skeleton<br />
stresses and a discussion <strong>of</strong> the relative importance <strong>of</strong> the different transport mechanisms.<br />
Simulator Coupling for Predicting Nonlinear Rotor/Bearing Interactions<br />
Daixing Lu, Martin Busch, Bernhard Schweizer (<strong>Universität</strong> Kassel) Schedule<br />
Precisely calculating the dynamic oscillations <strong>of</strong> rotors supported in oil film bearings requires very<br />
detailed and accurate bearing models. Performing dynamic simulations <strong>of</strong> rotors with hydrodynamic<br />
bearings, usually models based on look-up tables are used, i.e. the nonlinear stiffness and<br />
damping characteristic <strong>of</strong> the bearings is determined in a preprocessing step and incorporated<br />
into the simulation model for the rotor by means <strong>of</strong> spline-approximation techniques [1]. Such an<br />
approach is very time efficient, but suffers from a reduced physical accuracy. To improve the simulation,<br />
the finite-element models for the bearings are directly coupled with the multibody model<br />
for the rotor. Here, we discuss a weak coupling approach based on a semi-implicit integration<br />
technique in combination with a master/slave simulator coupling strategy [2].<br />
[1] B. Schweizer, Dynamics and Stability <strong>of</strong> Turbocharger Rotors, Archive <strong>of</strong> Applied Mechanics<br />
80(9) (2010), 1017 – 1043.<br />
[2] M. Busch, B. Schweizer, Coupled Simulation <strong>of</strong> Multibody and Finite Element Systems:<br />
An Efficient and Robust Semi-Implicit Coupling Approach, Archive <strong>of</strong> Applied Mechanics<br />
(2011), doi: 10.1007/s00419-011-0586-0.<br />
S7.8: Miscellaneous Coupled Problems Thu, 16:00–18:00<br />
Chair: Christian Linder S1|03–226<br />
The Scattering map in two-linked rocking blocks<br />
Albert Granados (<strong>Universität</strong> Stuttgart), John Hogan (University <strong>of</strong> Bristol), Tere Seara (Universitat<br />
Politècnica de Catalunya) Schedule<br />
The rocking block is not only a paradigm <strong>of</strong> a mechanical system with impacts, but also it is used<br />
to model the behaviour <strong>of</strong> slender structures under an external forcing, such as water tanks or<br />
nuclear fuel rods under earthquake excitation. In addition, the stacked coupling <strong>of</strong> such blocks<br />
is also <strong>of</strong> interest for the modeling <strong>of</strong> structures in civil engineering or nano carbon tubes under<br />
small vibrations.<br />
In this work we consider a generalization <strong>of</strong> a simple model based on two rocking blocks linked<br />
by a spring under a non-autonomous periodic forcing. Considering that the spring constant is
174 Section 7: Coupled problems<br />
small, we treat the model as two impact oscillators under a general perturbation which includes<br />
the forcing and the coupling. This leads to a 5-dimensional non-smooth system with two switching<br />
manifolds.<br />
We then focus on the configuration given by large amplitude oscillations for one block while the<br />
other one oscillates with higher frequency and smaller amplitude. By means <strong>of</strong> the impact map<br />
associated with the fast rocking block, we derive sufficient conditions for the existence <strong>of</strong> heteroclinic<br />
connections and construct the so-called scattering map. The properties <strong>of</strong> this map allows us<br />
to show that, under certain conditions, for any arbitrarily small amplitude <strong>of</strong> the periodic forcing,<br />
energy is accumulated on the fast rocking block at every large oscillation <strong>of</strong> the slow motion rock.<br />
Then, by properly concatenating such movements, it is possible to show that, for large time scales<br />
and arbitrarily small amplitude <strong>of</strong> the forcing, arbitrarily high energy can be accumulated in the<br />
system, hence leading to the instabilities as a consequence <strong>of</strong> the so-called Arnol’d diffusion.<br />
Modeling and Simulation <strong>of</strong> Microwave Heating for Spalling <strong>of</strong> Radioactive Contaminated<br />
Concrete<br />
Andreas Melcher, Thorsten Kayser, Guido Link, John Jelonnek (KIT) Schedule<br />
Microwave heating is becoming <strong>of</strong> growing importance in material sciences in the last ten years.<br />
Due to the volumetric heating effect microwave heating <strong>of</strong>fers an energy efficient way <strong>of</strong> processing<br />
materials in several ways. The modeling and simulation <strong>of</strong> material processing with microwaves<br />
with respect to the material structure is a challengeing task. In this talk we will analyze the<br />
complexity <strong>of</strong> the problem, giving an appropriate modeling which result in a coupled, multiscale<br />
problem in space and time consisting Maxwell equations, the heat equation and a description <strong>of</strong><br />
the electromagnetic material properties <strong>of</strong> the concerning materials. As example we discuss the<br />
ablation <strong>of</strong> concrete with microwaves and give some experimental and simulation results<br />
Quantifying diffusion for an ultrasonic wire bonding process by applying the theory<br />
<strong>of</strong> material forces<br />
Mohamad Sbeiti, Wolfgang H. Müller (TU Berlin), Martin Schneider-Ramelow (Fraunh<strong>of</strong>er Institut<br />
für Zuverlässigkeit und Mikrointegration, Berlin), Ute Geißler (TU Berlin) Schedule<br />
Ultrasonic wire bonding is a method applied in electronic packaging for interconnections between<br />
two devices at ambient temperature. In this process, high frequency vibrations (f = 100 kHz)<br />
combined with pressure are responsible for the deformation <strong>of</strong> a 25µm aluminum wire in vertical<br />
direction and for the formation <strong>of</strong> an Au8Al3 intermetallic phase between the wire and the pad.<br />
Due to the variety and complexity <strong>of</strong> the mechanisms occurring during the bonding process there<br />
is an enormous demand to clarify some open issues for a thorough interpretation <strong>of</strong> the metallurgical<br />
processes that take place at the interface <strong>of</strong> the bond and in the wire.<br />
FE simulations <strong>of</strong> the temperature increase due to ultrasonic energy dissipation and plastic deformation<br />
(Taylor-Quinney effect) during the bonding process show that it is too small in order to<br />
explain the amount <strong>of</strong> intermetallic phase formed in terms <strong>of</strong> classical Fickian diffusion. Therefore<br />
one <strong>of</strong> the open issues is to investigate the mechanical coupling on diffusion in terms <strong>of</strong> the strain<br />
energy densities arising during the bonding process.<br />
For clarification <strong>of</strong> this issue a thermo-mechanical FE model was first created to determine the<br />
stress states and the strain energy densities around the interface. Then a post-processing tool<br />
was written in C++ (based on an existing code developed by R. Müller and his group at the<br />
University <strong>of</strong> Kaiserslautern) in order to calculate the thermo-mechanical driving force in terms<br />
<strong>of</strong> the local jump <strong>of</strong> the Eshelby tensor across the interface.<br />
Within the framework <strong>of</strong> material forces the local jump <strong>of</strong> the Eshelby tensor can be compared<br />
with the thickness <strong>of</strong> the formed intermetallic phase for various bonding parameters. This will
Section 7: Coupled problems 175<br />
allow us to predict an effective diffusion constant which takes temperature and mechanical driving<br />
forces into account. After this relation has been established a subsequent objective <strong>of</strong> our<br />
investigations is to optimize the growth <strong>of</strong> the Au8Al3 intermetallic phase in terms <strong>of</strong> bonding<br />
parameters.<br />
Electronic Structure Calculations with Finite Elements<br />
Volker Schauer, Christian Linder (<strong>Universität</strong> Stuttgart) Schedule<br />
The physical properties <strong>of</strong> materials, as for example electric and thermal conductivity, magnetism,<br />
formation <strong>of</strong> microstructures as well as the mechanical response upon external excitations, are<br />
finally determined by the electronic structure <strong>of</strong> the material. The quantum mechanical description<br />
<strong>of</strong> electronic structure represents a coupled many body problem, consisting <strong>of</strong> the positively<br />
charged atomic cores and the negatively charged, fermionic electrons. By the Hohenberg-Kohn<br />
theorem a method was established to calculate the electron density <strong>of</strong> the ground state <strong>of</strong> an<br />
atomic system as the minimum <strong>of</strong> a density functional [1]. The variation <strong>of</strong> the functional leads to<br />
the Kohn-Sham equations, which represent a nonlinear eigenvalue problem. The originally coupled<br />
problem has therefore been transformed into a nonlinear but single particle problem with<br />
an effective potential that accounts for the Coulomb interactions between the particles as well as<br />
for quantum mechanical effects [2]. The Kohn-Sham equations can be solved iteratively with the<br />
so-called self consistent field algorithm. We implement a real space formulation for the calculation<br />
<strong>of</strong> the electronic structure in the context <strong>of</strong> density functional theory. In a first step a finite element<br />
based solution algorithm for the Kohn-Sham equations is developed, based upon which the<br />
electron density can be obtained in a non periodic setting [3]. We will present the basic elements<br />
<strong>of</strong> our implementation together with some typical examples for the electronic structure.<br />
[1] P. Hohenberg, W. Kohn, Inhomogeneous Electron Gas, Phys. Rev. B 136 (1964), 864-871.<br />
[2] R.M. Martin, Electronic Structure, Cambridge University Press (2004).<br />
[3] P. Suryanarayana, V. Gavini, T. Blesgen, K. Bhattacharya, M. Ortiz, Non-periodic finiteelement<br />
formulation <strong>of</strong> KohnSham density functional theory, Journal <strong>of</strong> the Mechanics and<br />
Physics <strong>of</strong> Solids 58 (2010), 256-280.<br />
Modifications <strong>of</strong> hypergraphs <strong>of</strong> subsystems <strong>of</strong> mechatronic system as an effect <strong>of</strong><br />
their analysis by means <strong>of</strong> different methods<br />
Andrzej Buchacz (Silesian University <strong>of</strong> Technology) Schedule<br />
Purpose <strong>of</strong> this paper is analysis <strong>of</strong> vibrating beams as subsystems <strong>of</strong> transverse vibraing mechatronic<br />
system by the exact and approximate methods and creating the hypergraphs <strong>of</strong> the beams<br />
in case <strong>of</strong> presented methods <strong>of</strong> analysis. Approach was to nominate the relevance or irrelevance<br />
between the characteristics obtained by considered methods - especially concerning the relevance<br />
<strong>of</strong> the natural frequencies-poles <strong>of</strong> characteristics <strong>of</strong> simply beam. The main subject <strong>of</strong> the research<br />
are the continuous beams as the subsystems <strong>of</strong> continous-discrete vibrating mechatoronic<br />
system. Findings this approach is fact, that approximate solutions fulfill conditions for vibrating<br />
beams and can be introduction to synthesis <strong>of</strong> these systems modeled by hypergraphs <strong>of</strong> different<br />
category. Practical implication <strong>of</strong> this study is the main point is the introduction to synthesis<br />
<strong>of</strong> considered mechatronic system. Originality <strong>of</strong> this approach relies on application approximate<br />
method <strong>of</strong> analysis <strong>of</strong> beams and modeling the ones by modifications hypergraphs.
176 Section 8: Multiscales and homogenization<br />
Section 8: Multiscales and homogenization<br />
Organizers: Andreas Menzel (TU Dortmund), Sergiy Nesenenko (TU <strong>Darmstadt</strong>)<br />
S8.1: Multiscale analysis <strong>of</strong> laminated composites Tue, 13:30–15:30<br />
Chair: Andres Menzel, Sergiy Nesenenko S1|01–A01<br />
Non-laminate Microstructures in Monoclinic-I Martensite<br />
Anja Schlömerkemper (<strong>Universität</strong> Würzburg), Isaac Chenchiah (University <strong>of</strong> Bristol) Schedule<br />
The most common shape memory alloys are monoclinic-I martensite. We study their zero energy<br />
states and have two surprising results:<br />
First, there is a five-dimensional continuum in which the energy minimising microstructures<br />
are T3s, i.e. infinite-rank laminates. To our knowledge, this is the first real material in which T3s<br />
occur. We discuss some <strong>of</strong> the consequences <strong>of</strong> this discovery.<br />
Second, there are in fact two types <strong>of</strong> monoclinic-I martensite, which differ by their convexpolytope<br />
structure but not by their symmetry properties. It happens that all known materials<br />
belong to one <strong>of</strong> the two types. We explore whether materials belonging to the other type would<br />
have superior properties since they have different zero-energy states.<br />
Our analysis uses algebraic methods, in particular the theory <strong>of</strong> convex polytopes.<br />
An orientation-distribution-based multi-scale approach for modeling <strong>of</strong> flow-induced<br />
anisotropy <strong>of</strong> polar ice for the EDML deep-drilling site, Antarctica<br />
Swantje Bargmann (TU Dortmund), Hakime Seddik, Ralf Greve (Hokkaido University) Schedule<br />
In this contribution we model the anisotropic flow in polar ice in order to gain a better understanding<br />
for the underlying microstructure and its influence on the deformation process. In<br />
particular, a continuum mechanical, anisotropic flow model, which is based on an anisotropic flow<br />
enhancement factor, the so-called CAFFE model, is applied. The polycrystalline ice is regarded<br />
as a mixture whose grains are characterized by their orientation.<br />
The approach is based on two distinct scales: the underlying microstructure influences the<br />
macroscopic material behavior and is taken into account phenomenologically. To achieve this<br />
the orientation mass density is introduced as a so called mesoscopic field. The classical flow law<br />
<strong>of</strong> Glen is extended by a scalar enhancement factor. Moreover, four different effects (local rigid<br />
body rotation, grain rotation, rotation recrystallization, grain boundary migration) influencing<br />
the evolution <strong>of</strong> the grain orientations are taken into account. A finite volume method is chosen<br />
for the discretization procedure. Numerical results simulating the ice flow in the EPICA ice core<br />
EDML, Antarctica, are presented.<br />
[1] S. Bargmann, H. Seddik, R. Greve. Computational modeling <strong>of</strong> flow-induced anisotropy <strong>of</strong><br />
polar ice for the EDML deep-drilling site, Antarctica: the effect <strong>of</strong> rotation recrystallization<br />
and grain boundary migration. International Journal for Numerical and Analytical Methods<br />
in Geomechanics 2011, accepted for publication, DOI: 10.1002/nag.1034<br />
[2] R. Greve,H. Blatter. (2009). Dynamics <strong>of</strong> Ice Sheets and Glaciers. Springer, Berlin, Germany<br />
[3] L. Placidi, R. Greve, H. Seddik, S.H. Faria. A continuum-mechanical, anisotropic flow model<br />
for polar ice, based on an anisotropic flow enhancement factor. Continuum Mechanics and<br />
Thermodynamics 2009; doi: 10.1007/s00161-009-0126-0<br />
[4] H. Seddik, R. Greve, L. Placidi, I. Hamann, O. Gagliardini. Application <strong>of</strong> a continuummechanical<br />
model for the flow <strong>of</strong> anisotropic polar ice to the EDML core, Antarctica. Journal
Section 8: Multiscales and homogenization 177<br />
<strong>of</strong> Glaciology 2008, 45(187):631-642.<br />
The evolution <strong>of</strong> the crystallographic texture in terms <strong>of</strong> harmonic tensors<br />
Jan Kalisch, Albrecht Bertram (<strong>Universität</strong> Magdeburg) Schedule<br />
The crystallographic texture <strong>of</strong> polycrystals determines the anisotropy <strong>of</strong> both their elastic and<br />
plastic behaviour. The texture is described by the orientation distribution function (ODF) giving<br />
the volume fraction <strong>of</strong> single crystals with similar lattice orientation [1,2,3,4].<br />
The Fourier expansion <strong>of</strong> the ODF on the space <strong>of</strong> orientations provides an infinite list <strong>of</strong> harmonic<br />
tensors, called texture coefficients [1,2]. Alternatively, we can use the maximum entropy<br />
approximation [5] to obtain the pseudo ODF [2]. It involves a finite list <strong>of</strong> harmonic tensors, called<br />
pseudo texture coefficients.<br />
Either set <strong>of</strong> tensors can be used as set <strong>of</strong> internal variables to account for the influence <strong>of</strong> the<br />
crystallographic texture in macro-scale models <strong>of</strong> polycrystals.<br />
Focusing on the crystallographic texture, we consider a single crystal model for which the internal<br />
state is determined completely by the orientation. The homogenisation <strong>of</strong> the flow potential has<br />
been discussed in [3,6].<br />
In polycrystals consisting <strong>of</strong> such single crystals and homogeneous processes (Taylor or Sachs<br />
model), the texture evolution follows an infinite system <strong>of</strong> linear ODEs for the texture coefficients<br />
or a finite system <strong>of</strong> quasilinear ODEs for the pseudo texture coefficients, respectively. We discuss<br />
aspects <strong>of</strong> both systems and provide numerical solutions for simple examples.<br />
[1] J. Kalisch, A. Bertram, On the Evolution <strong>of</strong> the Crystallographic Texture <strong>of</strong> Cubic Polycrystals<br />
in Coaxial Processes, Int. J. Mater. Form. 3 Suppl. 1 (2010), 57 – 60.<br />
[2] T. Böhlke, Texture Simulation based on Tensorial Fourier Coefficients, Comp. Struct., 84<br />
(2006), 1086 – 1094.<br />
[3] T. Böhlke, The Voigt bound <strong>of</strong> the stress potential <strong>of</strong> isotropic viscoplastic FCC polycrystals,<br />
Arch. Mech. 56 (2004), 425 – 445.<br />
[4] B.L. Adams, J.P. Boehler, M. Guidi, E.T. Onat, Group theory and representation <strong>of</strong> microstructure<br />
and mechanical behavior <strong>of</strong> polycrystals, J. Mech. Phys. Solids 40 (1992), 723<br />
– 737.<br />
[5] E. Jaynes, Information theory and statistical mechanics, Phys. Rev. 106 (1957), 620 – 630.<br />
[6] R. Tsotsova, T. Böhlke, Representation <strong>of</strong> effective flow potentials for polycrystals based on<br />
texture data, I. J. Mat. Forming 2 Suppl. 1 (2009), 451 – 454.<br />
A Texture-Based Two-Scale Finite Element Simulation <strong>of</strong> a Multi-Step Can Forming<br />
Process<br />
V. Glavas, T. Böhlke (KIT), D. Daniel (Constellium), C. Leppin (Suisse Technology Partners<br />
AG) Schedule<br />
Aluminum sheets used for beverage cans show a significant anisotropic plastic material behavior<br />
in sheet metal forming operations. In a deep drawing process <strong>of</strong> cups this anisotropy leads to a<br />
non-uniform height, i.e., an earing pr<strong>of</strong>ile. The prediction <strong>of</strong> this earing pr<strong>of</strong>iles is important for<br />
the optimization <strong>of</strong> the forming process. In most cases the earing behavior cannot be predicted
178 Section 8: Multiscales and homogenization<br />
precisely based on phenomenological material models. In the presented work a micromechanical,<br />
texture-based model is used to simulate the first two steps (cupping and redrawing) <strong>of</strong> a can<br />
forming process. The predictions <strong>of</strong> the earing pr<strong>of</strong>ile after each step are compared to experimental<br />
data.<br />
The mechanical modeling is done with a large strain elastic visco-plastic crystal plasticity<br />
material model with a Norton type flow rule for each crystal. The response <strong>of</strong> the polycrystal is<br />
approximated by a Taylor type homogenization scheme. The simulations are carried out in the<br />
framework <strong>of</strong> the finite element method. The shape <strong>of</strong> the earing pr<strong>of</strong>ile from the finite element<br />
simulation is compared to experimental pr<strong>of</strong>iles.<br />
[1] T. Böhlke, G. Risy, A. Bertram, Finite element simulation <strong>of</strong> metal forming operations with<br />
texture based material models. Modelling and Simulation in Material Science and Engineering<br />
(2006) 365–387.<br />
[2] K. Jöchen, T. Böhlke, Preprocessing <strong>of</strong> Texture Data for an Efficient Use in Homogenization<br />
Schemes. Proc. 10th Int. Conf. Techn. Plast. ICTP (2011) 848–853.<br />
[3] G. I. Taylor, Plastic strain in metals. Journal <strong>of</strong> the Institute <strong>of</strong> Metals 62 (1938) 307–322.<br />
Construction <strong>of</strong> Statistically Similar RVEs for 3D Microstructures<br />
Lisa Scheunemann, Daniel Balzani, Dominik Brands, Jörg Schröder (<strong>Universität</strong> Duisburg-Essen)<br />
Schedule<br />
The microstructure <strong>of</strong> advanced high-strength steels influences significantly the overall material<br />
properties and should thus be incorporated in numerical calculations. For this purpose, the<br />
FE 2 method, also known as direct micro-macro transition, is a suitable numerical tool, see e. g.<br />
[1], [2]. In this context, the definition <strong>of</strong> a representative volume element (RVE), which is characterized<br />
by a significantly reduced complexity compared with the real microstructure, reduces time<br />
and memory costs. Therefore, we propose the construction <strong>of</strong> statistically similar RVEs (SSRVEs)<br />
which still represent the mechanical response <strong>of</strong> the material accurately, cf. [3]. The construction<br />
method is based on the minimization <strong>of</strong> a least-square functional considering the differences <strong>of</strong><br />
suitable statistical measures characterizing the inclusion morphology <strong>of</strong> a given real microstructure<br />
and <strong>of</strong> the SSRVE. In 2D the construction <strong>of</strong> SSRVEs turned out to be successfull in a series<br />
<strong>of</strong> numerical examples, cf. [3], [4].<br />
The focus <strong>of</strong> this talk is on the construction <strong>of</strong> three-dimensional SSRVEs based on the inclusion<br />
phase fraction, the spectral density and the lineal-path function. SSRVEs are constructed for a<br />
real microstructure <strong>of</strong> a DP-steel from 3D measurement obtained by 3D Electron Backscatter<br />
Diffraction (EBSD) combined with a Focused Ion Beam (FIB). To demonstrate the performance<br />
<strong>of</strong> the proposed method we discuss several numerical examples.<br />
[1] C. Miehe, J. Schröder, J. Schotte: Computer Methods in Applied Mechanics and Engineering,<br />
171:387–418, 1999.<br />
[2] J. Schröder: Institut für Mechanik (Bauwesen), Lehrstuhl I, <strong>Universität</strong> Stuttgart, Habilitation<br />
thesis, 2000.<br />
[3] J. Schröder, D. Balzani and D. Brands: Archive <strong>of</strong> Applied Mechanics, 81:975-997, 2011.<br />
[4] D. Balzani, D. Brands, J. Schröder, C. Carstensen: <strong>Technische</strong> Mechanik, 30/4:297-315, 2010.
Section 8: Multiscales and homogenization 179<br />
[5] R. N. Singh, N. Zaafarani, D. Raabe, F. Roters and S. Zaefferer: Acta Materialia, 54:1863-<br />
1876, 2006.<br />
S8.2: Discrete-to-continuum and homogenization methods Tue, 16:00–18:00<br />
Chair: Jörg Hohe, Bernhard Eidel S1|01–A01<br />
Numerical quadrature for coarse-grained molecular statics<br />
Bernhard Eidel (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
Recent research in atomistic-to-continuum coupling methods and in particular in the Quasicontinuum<br />
(QC) method has shown a strong interest in numerical quadrature because it largely<br />
determines the methods accuracy and efficiency. Mathematical analyses <strong>of</strong> new quadrature rules<br />
<strong>of</strong>ten restrict to (i) the 1D case <strong>of</strong> atomic chain models, to (ii) simple pair potentials and to (iii)<br />
additional ad-hoc assumptions and simple applications. These simplifications (i)-(iii) make the<br />
problem tractable by analytical means or alleviate numerical analysis. Doing this, mathematics<br />
has brought new insights into atomistic-based finite element methods. However, it is not clear,<br />
how the quadrature rules shall be reformulated without these strongly simplifying assumptions.<br />
The main aim <strong>of</strong> the present contribution is the numerical analysis <strong>of</strong> different quadrature rules<br />
within the QC method in a more realistic physical setting, namely (i) in 3D, (ii) using EAMpotentials<br />
and (iii) analyzing paradigmatic multiscale settings <strong>of</strong> nano- and micromechnics. In<br />
particular, we compare the method proposed by Gunzburger & Zhang (SIAM Multiscale Model.<br />
Simul., 8:571–590, 2010) with the cluster-based summation rule as proposed by Knap & Ortiz<br />
(J. Mech. Phys. Solids 49:1899–1923, 2001). The different quadrature schemes are assessed and<br />
compared in representative numerical examples.<br />
Partial Damping for Weak Coupling between MD and FE models<br />
Wenzhe Shan, Udo Nackenhorst (<strong>Universität</strong> Hannover) Schedule<br />
The weak coupling method enables us to decompose the solution into a high-frequency part and<br />
low-frequency part. The low-frequency part can be approximated by the FE shape functions while<br />
the high-frequency part, without extra treatment, will be reflected back into the MD domain. By<br />
frequency analysis, we found the weak coupling method, despite its complexity, does not <strong>of</strong>fer<br />
smoother transition for mechanical motions between the FE and MD domains, in comparison<br />
the more straightforward bridging domain method. However, the motion decomposition from the<br />
weak coupling method provides us convenient way to handle the transmissible and untransmissible<br />
motions separately. And due to the orthogonality <strong>of</strong> such decomposition, the influences <strong>of</strong> the<br />
manipulation applied to one part are minimized to the other.<br />
When dynamic problems are <strong>of</strong> interest, the high-frequency waves reflected from the coupling<br />
boundary will pollute the solution in the MD domain quickly and render the results from the<br />
multiscale model meaningless. In this contribution, we show that by applying artificial damping<br />
only to the high-frequency part <strong>of</strong> the displacement field in the coupling domain in the weak<br />
coupling method can significantly reduce the reflections in the MD domain while not affecting the<br />
low-frequency part that can be transmitted into the FE domain. The frequency analysis shows<br />
the errors in the magnitudes and phases <strong>of</strong> wave components are orders <strong>of</strong> magnitudes smaller<br />
than that in the bridging domain model or undamped weak coupling model.<br />
Simulation <strong>of</strong> texture evolution during rolling by using a homogenization method <strong>of</strong><br />
Hashin-Shtrikman type<br />
Katja Jöchen, Thomas Böhlke (KIT) Schedule
180 Section 8: Multiscales and homogenization<br />
In this contribution, the development <strong>of</strong> rolling textures in metals is investigated by using a<br />
homogenization method that is based on a homogeneous comparison material [4]. Assuming piecewise<br />
constant stress polarizations in the polycrystalline aggregate and restricting to ellipsoidal<br />
two-point statistics, a localization rule for the strain field is derived. Varying the stiffness <strong>of</strong><br />
the comparison medium, the proposed scheme inherently includes a smooth transition between<br />
Taylor- and Sachs-type textures, the latter are obtained using infinitely stiff and infinitely compliant<br />
comparison materials. As an example, the texture evolution during rolling <strong>of</strong> an aluminum<br />
sheet is simulated with initial orientation data taken from [1]. It is shown that the application <strong>of</strong><br />
different comparison materials in the homogenization scheme leads to the development <strong>of</strong> different<br />
main texture characteristics [3]. Especially the initially dominant cube component shows a strong<br />
dependence on the choice <strong>of</strong> the comparison material.<br />
To speed up the simulations using experimental texture information <strong>of</strong> the polycrystalline material,<br />
the data is representatively reduced by using a partitioning technique <strong>of</strong> the orientation<br />
space [2] before entering the homogenization framework.<br />
[1] L. Delannay, S. R. Kalidindi, and P. Van Houtte, 2002, Quantitative prediction <strong>of</strong> textures<br />
in aluminium cold rolled to moderate strains, Mat. Sci. Eng. A, 336, 233 - 244<br />
[2] K. Jöchen, and T. Böhlke, 2011, Preprocessing <strong>of</strong> texture data for an efficient use in homogenization<br />
schemes, ICTP2011 Proceedings, 848-853<br />
[3] K. Jöchen, and T. Böhlke, 2011/12, Prediction <strong>of</strong> texture evolution in rolled sheet metals by<br />
using homogenization schemes, submitted to Key Engineering Materials, 6 p.<br />
[4] P. Ponte Castañeda, and P. Suquet, 1998, Nonlinear Composites Adv. Appl.Mech. 34, 171-302<br />
Local probabilistic homogenization schemes for assessment <strong>of</strong> material uncertainties<br />
in solid foams<br />
Jörg Hohe, Carla Beckmann (Fraunh<strong>of</strong>er-Institut für Werkst<strong>of</strong>fmechanik) Schedule<br />
Solid foams gain increasing importance as lightweight construction materials e.g. as core materials<br />
in sandwich construction. Their main advantage is their low specific weight due to their high void<br />
volume fraction and the resulting advantageous stiffness-to-weight ratio. On the other hand, solid<br />
foams have the disadvantage <strong>of</strong> a random, disordered microstructure causing a distinct scatter in<br />
their effective stiffness and strength.<br />
The present study is concerned with a local probabilistic homogenization scheme far a stochastic<br />
analysis <strong>of</strong> the effective stiffness and strength <strong>of</strong> solid foams. For this purpose, a standard<br />
homogenization procedure is adopted, defining the effective stresses and strains as their volume<br />
averages with respect to a mesoscopic volume element. In contrast to the homogenization <strong>of</strong><br />
regular microstructured media or randomly microheterogeneous media with small characteristic<br />
internal length scales, especially metallic foams may feature a microstructure with internal lengths<br />
(e.g. cell sizes) which are not much smaller than the smallest characteristic length <strong>of</strong> the macroscopic<br />
structure, e.g. a sandwich core thickness. Hence, a rigorously deterministic homogenization<br />
is not feasible and a stochastic approach is required.<br />
For this purpose, a large-scale, statistically representative volume element is considered. The<br />
volume element features a disordered microstructure defined in terms <strong>of</strong> a set <strong>of</strong> random variables.<br />
The computational foam model is generated randomly using a Voronoï process in Laguerre<br />
geometry. In contrast to previous approaches, the homogenization is performed locally, using the
Section 8: Multiscales and homogenization 181<br />
individual cells <strong>of</strong> the large-scale volume element as small-scale testing volume elements. Alternatively,<br />
a moving-window approach is employed. The testing volume elements themselves are<br />
non-representative, however, the entire set <strong>of</strong> testing volume elements has to be sufficiently large<br />
in order to be representative. Determining the effective stiffness and strength for the individual<br />
testing volume elements provides the mean values and the corresponding probability distributions<br />
for the effective material properties. Furthermore, the spatial correlation <strong>of</strong> the effective properties<br />
and its decay can be analyzed.<br />
As a result, the stochastic information for a probabilistic structural analysis <strong>of</strong> foam structures<br />
on the macroscopic level is obtained, where the material properties are defined in terms <strong>of</strong> random<br />
fields.<br />
Short-fiber reinforced thermoplastics – A geometrically non-linear two-scale approach<br />
V. Müller, B. Brylka, T. Böhlke (KIT) Schedule<br />
Short-fiber-reinforced composites are increasingly used not only because <strong>of</strong> their advantageous<br />
ratio <strong>of</strong> stiffness to weight in comparison to pure thermoplastics but also in consequence <strong>of</strong> the<br />
possibility <strong>of</strong> low-cost manufacturing. Usually composites <strong>of</strong> this kind are manufactured in injection<br />
or compression molding processes. Therefore, short fiber reinforced polymers show heterogeneities<br />
on different length scales concerning micro-structural properties like fiber orientation<br />
distributions [1].<br />
Micromechanical models <strong>of</strong>fer the opportunity <strong>of</strong> a mechanism-based modeling. In contrary<br />
to FE 2 schemes the application <strong>of</strong> mean field approaches at the integration point level <strong>of</strong> the<br />
finite elements represents a compromise between computational effort and accuracy [2]. Mean<br />
field approaches can predict phase averages <strong>of</strong> mechanical fields as well as stress and strain<br />
heterogeneities in the phases based on a simplified description <strong>of</strong> microstructure [3].<br />
In the presentation short-fiber reinforced thermoplastics with spatially varying orientation<br />
distributions <strong>of</strong> fibers are considered. The micromechanically based model is developed in a geometrically<br />
nonlinear setting. To demonstrate the effect <strong>of</strong> the microstructure on the macroscopic<br />
material behavior a model problem is generated with specially heterogeneous orientation distributions<br />
<strong>of</strong> fibers. This data is used within finite element simulations <strong>of</strong> shell type structural<br />
elements.<br />
[1] M. Laspalas, C. Crespo, M.A. Jimènez, B. García, J.L. Pelegay Application <strong>of</strong> micromechanical<br />
models for elasticity and failure to short fibre reinforced composites. Numerical<br />
implementation and experimental validation, Computers and Structures, 2008, 86, 977–987<br />
[2] V. Kouznetsova, W. A. Brekelmans, F.P.T. Baaijens An approach to micro-macro modeling<br />
<strong>of</strong> heterogeneous materials, Computational Mechanics, 2001, 27, 37–48<br />
[3] Charles L. Tucker III, Liang Erwin Stiffness predictions for unidirectional short-fiber composites:<br />
Review and evaluation, Composites Science and Technology, 1999, 59, 655–671<br />
Discrete model <strong>of</strong> a non-symmetric elasticity theory<br />
Maksym Berezhnyi (TU <strong>Darmstadt</strong>) Schedule<br />
We consider a discrete network <strong>of</strong> a large number <strong>of</strong> pin-type homogeneous rods oriented along<br />
a given vector and connected by elastic springs at each point. The asymptotic behavior <strong>of</strong> small<br />
oscillations <strong>of</strong> the discrete system is studied in the case where the distances between the nearest<br />
rods tend to zero. For generic non-periodic arrays <strong>of</strong> rods, we deduce equations describing the<br />
homogenized model <strong>of</strong> the system. It is shown that the homogenized equations correspond to
182 Section 8: Multiscales and homogenization<br />
a non-standard dynamics <strong>of</strong> an elastic medium. Namely, the homogenized stress tensor in the<br />
medium depends linearly not only on the strain tensor but also on the rotation tensor:<br />
σ[u] = A D e[u] + A R ω[u], (1)<br />
where the fourth-rank tensors A D and A R can be considered as the deformative and rotational<br />
parts <strong>of</strong> the elasticity tensor respectively. Moreover, those parts don’t possess the symmetry properties<br />
postulating in classical continuum mechanics.<br />
S8.3: Generalised continua Tue, 16:00–18:00<br />
Chair: Sergiy Nesenenko, Evgen Khruslov S1|01–A04<br />
On oscillation <strong>of</strong> elastic medium with small cavities filled by viscous incompressible<br />
liquid<br />
Evgen Khruslov (Verkin Institute for Low Temperature Physics, Kharkiv) Schedule<br />
We consider equations describing non-stationary oscillations <strong>of</strong> elastic medium with small cavities<br />
filled by viscous incompressible liquid. The asymptotic behaviour <strong>of</strong> the solution for the Cauchy<br />
problem for these equations is studied when the diameters <strong>of</strong> the cavities tend to zero and their<br />
density increases. We obtain the homogenized equation describing the first term <strong>of</strong> the asymptotics.<br />
Further, we study the long time behaviour <strong>of</strong> the solution for the homogenized equation. We<br />
prove that the solution decays exponentially.<br />
Parameteridentification in Discrete Element Methods via Comparison with Cosserat<br />
Theory<br />
Nicola Wessels, Klaus Hackl (<strong>Universität</strong> Bochum) Schedule<br />
One <strong>of</strong> the main challenges using the Discrete Element Method is that there is no direct compliance<br />
to the well known continuum parameters such as elastic moduli. In this presentation we<br />
show how homogenization procedures using representative volume elements composed <strong>of</strong> discrete<br />
particles lead to Cosserat continua.<br />
Simulating a shear test with discrete elements it becomes obvious, that the evolving microstructure<br />
is mainly composed <strong>of</strong> contact chains that form triangles and quadrilaterals. For these contact<br />
chains we set up contact energies in normal and shear directions and combine those to derive the<br />
effective energy <strong>of</strong> the material. By comparison <strong>of</strong> this energy to a Cosserat energy we can derive<br />
formulas for the Lamé and Cosserat parameters. They are now only dependent on the interaction<br />
energies and radii <strong>of</strong> the particles.<br />
To show the validity <strong>of</strong> our assumptions and derivations we present some discrete element simulations<br />
<strong>of</strong> shear tests.<br />
Complete asymptotic decomposition in the problem <strong>of</strong> elestic frameworks deformation<br />
A.G. Kolpakov (Siberian State University <strong>of</strong> Telecommunications and Informatics, Novosibirsk),<br />
S.I. Rakin (Siberian Transport University, Novosibirsk) Schedule<br />
Frameworks, considered as three dimensional elastic structure, consists <strong>of</strong> thin beams and joints,<br />
which assemble the beams in a unity. Thus, analysis <strong>of</strong> frameworks consists in both analysis <strong>of</strong><br />
beams and analysis <strong>of</strong> joints. The classical structural engineering approach does not ffeelßpecific<br />
properties <strong>of</strong> a joint: geometry, material characteristics, etc. We demonstrate that asymptotic analysis<br />
based approach allows integrated analysis <strong>of</strong> framework structure and joints. We demonstrate<br />
that the problem allows complete asymptotic decomposition: solution to the original problem can<br />
be separated into solution <strong>of</strong> a problem about deformation <strong>of</strong> a system <strong>of</strong> one dimensional beams
Section 8: Multiscales and homogenization 183<br />
and solution <strong>of</strong> the elasticity theory problems separately for any joint.<br />
We start our consideration with the case <strong>of</strong> two joined beams with one joint. The left beam<br />
places between x1 = −1 and x1 = 0, the right beam places between x1 = 0 and x1 = 1, the joint<br />
places around the origin <strong>of</strong> the coordinate system x = 0. We assume that the diameters <strong>of</strong> beams<br />
and dimensions <strong>of</strong> the joint in all directions are proportional to a small parameter ε.<br />
We use the method <strong>of</strong> local perturbation [1] and find solution in the form<br />
u ε (x) = εw1(x1)e1 + w2(x1)e2 − w ′ 2(x1)x2e1 + (1)<br />
+w3(x1)e3 − w ′ 3(x1)x2e1 + (x2e3 − x3e2)Θ(x1) + εv(x/ε)<br />
The leading six terms in the right-hand side <strong>of</strong> (1) correspond to structural mechanics hypothesis.<br />
The novelty is the last term in the right-hand side <strong>of</strong> (1). It is introduced to account the perturbation<br />
<strong>of</strong> solution associated with the joint. We assume that the function v(y) is perturbed near<br />
x = 0.<br />
The representation (1) is similar to the solution representation on the homogenization theory.<br />
The difference is that the perturbation v(y) is periodic in the homogenization theory, but v(y) is<br />
perturbed near x = 0 in our consideration. It leads to the significant differences in the final results.<br />
In particular, the joint is ignored in the limit problem. But local stress-strain state essentially<br />
depends on the specific properties (both geometrical and material) <strong>of</strong> the joint.<br />
We expand our method to beams with many joints and joint assembling several beams.<br />
The research was supported through Marie Curie actions FP7: project PIIF2-GA-2008-219690.<br />
[1] Gaudiello A., Kolpakov A.G.: Influence <strong>of</strong> nondegenerated joint on the global and local<br />
behaviour <strong>of</strong> joined rods. Int. J. Engng Sci. 2011, 49, 295-309.<br />
Periodic elliptic operators with preassigned spectral gaps<br />
Andrii Khrabustovskyi (B. Verkin Institute for Low Temperature Physics, Kharkiv) Schedule<br />
We deal with differential operators in R n (n ≥ 2) <strong>of</strong> the form<br />
A = − 1<br />
b(x)<br />
n�<br />
k,l=1<br />
∂<br />
∂xk<br />
�<br />
a kl (x) ∂<br />
where akl(x), b(x) are measurable functions satisfying the conditions<br />
a kl (x) = a lk (x), ∀ξ ∈ R n , |ξ| = 1 : 0 < a − ≤ a kl (x)ξkξl ≤ a + < ∞<br />
0 < b − ≤ b(x) ≤ b + < ∞<br />
∂xl<br />
∀i ∈ Z n , ∀x ∈ R n : a kl (x + i) = a kl (x), b(x + i) = b(x)<br />
It is known (E. Green (1997), A. Figotin and P. Kuchment (1997), R. Hempel and K. Lienau<br />
(2000), L. Friedlander (2002), O. Post (2003), V. Zhikov (2005)) that for an arbitrary m ∈ N one<br />
can construct an operator <strong>of</strong> the form (1) with at least m gaps in its spectrum.<br />
Our goal is to solve the following inverse problem: for an arbitrary set <strong>of</strong> m pairwise disjoint<br />
finite intervals on the positive semi-axis to construct an operator <strong>of</strong> the form (1) with (at least)<br />
m gaps that are close (in some sense) to these preassigned intervals.<br />
The precise statement <strong>of</strong> this problem and its solution are presented in [1], where the functions<br />
a kl (x) and b(x) are chosen in the form<br />
a kl (x) = g kl (x) � det G(x), b(x) = � det G(x)<br />
�<br />
(1)
184 Section 8: Multiscales and homogenization<br />
Here G(x) = {gkl(x)} n<br />
k,l=1 is some positively defined symmetric matrix, gkl (x) are the components<br />
<strong>of</strong> G −1 . Hence the operator A is the Laplace-Beltrami operator on the manifold M = R n equipped<br />
with the metrics G.<br />
We also discuss another method <strong>of</strong> constructing the appropriate functions a kl (x) and b(x)<br />
which has no geometrical interpretation.<br />
The ideas and methods are based on the previous results <strong>of</strong> the author related to homogenization<br />
theory for PDE’s.<br />
[1] A. Khrabustovskyi, Periodic Riemannian manifold with preassigned gaps in spectrum <strong>of</strong><br />
Laplace-Beltrami operator, J. Differ. Equ. 252 (<strong>2012</strong>), 2339 – 2369.<br />
Numerical assessment <strong>of</strong> disorder effects in metal foam core sandwich beams based<br />
on a local homogenization procedure<br />
Carla Beckmann, Jörg Hohe (Fraunh<strong>of</strong>er-Institut für Werkst<strong>of</strong>fmechanik) Schedule<br />
Solid foams are interesting materials for the core <strong>of</strong> sandwich constructions because <strong>of</strong> their<br />
low specific weight. However, the random microstructure is disadvantageous because disorder<br />
effects are the cause <strong>of</strong> spreading in the material behaviour <strong>of</strong> the whole device. To predict the<br />
uncertainties in the structural response <strong>of</strong> materials with random microstructure the numerical<br />
assessment gains more and more in importance because it is cost-efficient in contrast to extensive<br />
experimental analyses.<br />
In the present study, a numerical analysis <strong>of</strong> disorder effects in foam core sandwich beams is<br />
performed in order to assess the scatter due to the disordered foam microstructure. To determine<br />
the macroscopic effective material properties, a repeated numerical generation and analysis <strong>of</strong><br />
representative volume elements for the microstructure <strong>of</strong> the material is applied. Computational<br />
models for the foam microstructure are generated randomly using a Voronoï tessellation in<br />
Laguerre geometry. Using a large-scale volume element, a local homogenization procedure based<br />
on a moving window technique is applied which yields a sufficient large quantity <strong>of</strong> data in order<br />
to determine probability distributions and the spreading as well as the spatial correlation<br />
and the correlation between different material properties. In consideration <strong>of</strong> these statistical values,<br />
random fields are generated which make it possible not only to compute the mean effective<br />
properties in a numerical efficient way but also to determine the corresponding scatter. This is<br />
especially important in the assessment <strong>of</strong> the material strength because the local extreme values<br />
are responsible for the material failure.<br />
In order to illustrate the essential difference between computations where on the one hand the<br />
microstructure is replaced by a homogenous substitute medium and on the other hand by random<br />
fields, both methods are applied to a single edge clamped metal foam core sandwich beam which<br />
is loaded by a force at the free end.<br />
S8.4: Time-dependent and thermo-mechanical processes Wed, 13:30–15:30<br />
Chair: Daniel Juhre, Sandra Klinge S1|01–A01<br />
Viscoelastic effects and shrinkage as the accompanying phenomena <strong>of</strong> the curing <strong>of</strong><br />
polymers. Single- and multiscale effects<br />
Sandra Klinge, Alexander Bartels, Klaus Hackl (<strong>Universität</strong> Bochum), Paul Steinmann (<strong>Universität</strong><br />
Erlangen-Nürnberg) Schedule<br />
The presentation deals with the modeling <strong>of</strong> two phenomena that are characteristic for the curing<br />
<strong>of</strong> polymers, namely the increasing viscosity and the volume decrease known as autogeneous
Section 8: Multiscales and homogenization 185<br />
shrinkage. Both <strong>of</strong> these processes are caused by the cross-linking <strong>of</strong> polymer chains during polymerization.<br />
In order to model the viscoelastic effects the free energy consisting <strong>of</strong> an equilibrium<br />
and a non-equilibrium part is proposed. The former is related to the elastic processes and depends<br />
on total deformations. The latter is caused by the viscoelastic effects and depends only on the elastic<br />
part <strong>of</strong> deformations. It is assumed that the material parameters in the non-equilibrium part<br />
are constant while the evolution <strong>of</strong> the elastic deformations is controlled through the evolution <strong>of</strong><br />
the inelastic deformations and the inelastic material parameters. Different from the viscous process,<br />
the modeling <strong>of</strong> shrinkage effects does not require a new assumption for the free energy but a<br />
split <strong>of</strong> the total deformation gradient into a shrinkage and a mechanical part. The model suitable<br />
for simulating both <strong>of</strong> the mentioned phenomena is implemented in the single- and multiscale FE<br />
program. In the numerical examples, the focus is placed on the investigation <strong>of</strong> a combination <strong>of</strong><br />
a curing polymer with a standard elastic material <strong>of</strong> a high stiffness. This combination is used to<br />
represent the reinforced polymers, a group <strong>of</strong> nowadays widely applied materials.<br />
The maximal advance path constraint for the homogenization <strong>of</strong> materials with random<br />
network microstructures<br />
Mykola Tkachuk, Christian Linder (<strong>Universität</strong> Stuttgart) Schedule<br />
Many materials such as elastomers, biopolymer gels, s<strong>of</strong>t fibrous materials and open-cell foams<br />
possess a characteristic microstructure which is a random spatial network <strong>of</strong> long strands. Those<br />
undergo essentially non-affine microscopic deformation that consists in reorientation and axial<br />
stretch [1] when the macrodeformation is applied. A newly proposed statistical treatment based<br />
on the formalism <strong>of</strong> network paths allows to determine the non-affine deformation <strong>of</strong> the network<br />
and yields the homogenized elastic response <strong>of</strong> the material.<br />
Network paths with the maximal advance in a certain direction, called maximal advance paths,<br />
are used to formulate the constraints relating the macroscopic strain to the microscopic stretch<br />
<strong>of</strong> one-dimensional strands. These paths are defined in the initial undeformed configuration <strong>of</strong><br />
the network where all the strands have unit stretch and are oriented equally in all directions.<br />
The end-to-end vector <strong>of</strong> a path made by a large selection <strong>of</strong> strands from this assembly becomes<br />
a macroscopic object and deforms correspondingly. On the other hand, this deformed path is<br />
composed <strong>of</strong> the deformed strands and is defined by the average <strong>of</strong> the microstretch vectors over<br />
the path. The given macroscopic extension <strong>of</strong> such paths restricts the variation <strong>of</strong> the stretch in<br />
the network.<br />
The equilibrium state <strong>of</strong> the network at the given macroscopic strain should be characterized by<br />
the minimum <strong>of</strong> the free energy. This principle leads to a formulation <strong>of</strong> a constraint minimization<br />
problem from which the stretch distribution is derived. The homogenized response <strong>of</strong> the material<br />
is then computed by the averaging over the relaxed network. In the developed model the choice <strong>of</strong><br />
the free energy as a function <strong>of</strong> the microstretch distribution plays a crucial role. In particular, it<br />
should enforce the existence and uniqueness to the constrained minimization problem. Different<br />
generic energy terms are considered with respect to the fulfillment <strong>of</strong> this requirement. Furthermore<br />
the stability properties <strong>of</strong> the homogenized material with respect to the choice <strong>of</strong> network<br />
energy complement these studies. Finally, the numerical implementation <strong>of</strong> the developed model<br />
is proposed. This is based on the approximation <strong>of</strong> the variable microstretch on the microsphere<br />
<strong>of</strong> space orientations as in [2].<br />
[1] P. D. Wu, E. van der Giessen, On improved network models for rubber elasticity and their<br />
applications to orientation hardening in glassy polymers, Journal <strong>of</strong> the Mechanics and<br />
Physics <strong>of</strong> Solids, 41 (1993), 427-456.<br />
[2] C. Miehe, S. Göktepe, F. Lulei, A micro-macro approach to rubber-like materials – Part I: the
186 Section 8: Multiscales and homogenization<br />
non-affine micro-sphere model <strong>of</strong> rubber elasticity, Journal <strong>of</strong> the Mechanics and Physics <strong>of</strong><br />
Solids, 52 (2004), 2617–2660.<br />
Plane stress finite element analysis <strong>of</strong> filler reinforced polymers<br />
Deepanshu Sodhani, Stefanie Reese (RWTH Aachen) Schedule<br />
The characteristics <strong>of</strong> elastomers such as force-deformation behaviour, strength, fatigue and wear<br />
resistance, can be tailored by embedding it with filler particles. The influence <strong>of</strong> the fillers on the<br />
characteristic material behaviour significantly depends on the size and geometric form <strong>of</strong> the filler<br />
aggregates, which vary under mechanical loading.<br />
The polymer bulk can be divided into polymer matrix and primary aggregate. A new finite<br />
element-based simulation method proposed by Böl and Reese [1] has been used to represent the<br />
polymer matrix, which is characterized by chain like macro molecules linked together at certain<br />
points to form an irregular network.<br />
One <strong>of</strong> the classical reinforcing fillers are carbon blacks, which are produced in a variety<br />
<strong>of</strong> classes and types, depending on the required performance <strong>of</strong> the final product. In general,<br />
they consist <strong>of</strong> randomly ramified compositions <strong>of</strong> filler particles that are bonded together by<br />
strong sinter bridges. These compositions are referred to as primary aggregate. In this work, we<br />
investigate the polymer matrix being reinforced with primary aggregate.<br />
Suitable number <strong>of</strong> triangular elements are assembled to create a mesh unit referred to as<br />
filler element for each filler particle. Degrees <strong>of</strong> freedom <strong>of</strong> internal nodes in each filler element<br />
are eliminated using static condensation. The sinter bridges are modelled by adding another layer<br />
<strong>of</strong> elements around the filler element. Primary aggregate is now modelled using an assembly <strong>of</strong><br />
filler elements. This is now coupled with the polymer matrix to generate a finite element model<br />
<strong>of</strong> filler reinforced polymers.<br />
The proposed method provides the possibility to observe and understand how changes in size<br />
and geometry <strong>of</strong> filler particles (at microscopic level) affect the macroscopic behaviour <strong>of</strong> the filler<br />
reinforced polymers.<br />
[1] M. Böl and S. Reese, 2006, Finite element modelling <strong>of</strong> rubber like polymers based on chain<br />
statistics. International Journal <strong>of</strong> Solid and Structures 43, 2–26<br />
Keywords: filler element, primary aggregate, polymer matrix, sinter bridge<br />
Finite element simulation <strong>of</strong> the deformation behaviour <strong>of</strong> cellular rubber components<br />
Rathan Raghunath, Daniel Juhre (Deutsches Institut für Kautschuktechnologie) Schedule<br />
Cellular rubber is a heterogeneous material consisting <strong>of</strong> a filled elastomer matrix with embedded<br />
pores. It is characterized by a high compressibility with good resilience. Due to these properties<br />
cellular rubber is distinguished for a variety <strong>of</strong> sealing products. In practice cellular rubber gaskets<br />
are exposed to high mechanical loadings in which they have to combine a s<strong>of</strong>t closing behaviour<br />
and a sufficent reset for a guaranteed sealing. By varying the rubber mixture and the specific<br />
volume fraction <strong>of</strong> the pores, the behaviour <strong>of</strong> the cellular rubber can be adapted to its field <strong>of</strong><br />
application. To optimize this process a comprehensive characterization <strong>of</strong> the material concerning<br />
its mechanical properties is inevitable. However, in contrast to conventional materials, there are<br />
no suitable techniques for the material characterization <strong>of</strong> heterogeneous cellular rubber. Even<br />
both, the experimental testing as well as the finite element simulation <strong>of</strong> the material behaviour is<br />
not possible in the usual way. Indicative <strong>of</strong> this is that until today no reliable models for cellular<br />
rubber material are avaible in commercial FE programs. In this work a material model to describe
Section 8: Multiscales and homogenization 187<br />
the mechanical behaviour <strong>of</strong> cellular rubber is proposed. This model is intende to represent the<br />
highly complex material behaviour <strong>of</strong> cellular rubber under varying loading conditions. The model<br />
combines the material characteristics <strong>of</strong> the solid rubber with the explicit definition <strong>of</strong> the volume<br />
fraction <strong>of</strong> the embedded pores which facilitates the identification <strong>of</strong> the material parameter.<br />
Additionaly, it allows the distinct adjustment <strong>of</strong> the pore distribution within the gasket geometry<br />
which is induced by the production process and can be measured by micro-CT analyses.<br />
Microscopical investigation <strong>of</strong> wave propagation phenomena in residual saturated<br />
porous media<br />
Patrick Kurzeja, Holger Steeb (<strong>Universität</strong> Bochum), Marcel Frehner (ETH Zürich), Stefan<br />
Schmalholz (University <strong>of</strong> Lausanne) Schedule<br />
Wave propagation through partially saturated porous media can be <strong>of</strong> great interest, e. g. with<br />
respect to groundwater remediation and ganglia mobilization. Typical systems contain a solid<br />
skeleton and two non-miscible fluids, <strong>of</strong> which one is distributed discontinuously due to its low<br />
saturation. Therefore, a model <strong>of</strong> such a system requires to allow for two continuous phases (solid,<br />
non-wetting fluid) as well as for the fragmented wetting fluid. Models for continuous phases are<br />
well-established for two and three phases, e. g. [2]. The challenge is now to include the discontinuous<br />
fluid in a macroscopic description.<br />
First, we discuss wetting fluid patches and their dynamic behaviour on the microscale, i. e. 10 −5<br />
- 10 −3 m. The focus concentrates on the eigenfrequency and damping <strong>of</strong> their oscillations, which<br />
is influenced by the geometry, viscosity and surface tension. The weak formulation <strong>of</strong> this physical<br />
problem is solved and discussed against the background <strong>of</strong> other numerical and analytical<br />
solutions.<br />
These microscopic patches will be included in the macroscopic model as distinct damped oscillators<br />
after [1]. The homogenization between both scales conserves information about the microscopic<br />
density, eigenfrequency and damping to account for the discontinuity via probability density<br />
functions.<br />
The final model delivers insight into the behavior <strong>of</strong> propagating waves on the macroscale, influenced<br />
by different properties <strong>of</strong> the microscopic fluid clusters. Furthermore, the dispersion<br />
relations allow a comparison with continuous models and characteristic values, which might be<br />
helpful for experimental studies.<br />
[1] H. Steeb, M. Frehner and S.M. Schmalholz, Waves in residual-saturated porous media, in:<br />
G.A. Maugin and A.V. Metrikine, eds., Mechanics <strong>of</strong> generalized continua: One hundred<br />
years after the Cosserats, Springer, New York, USA, pp. 179-187, 2010.<br />
[2] H. Steeb, P. Kurzeja, M. Frehner and S.M. Schmalholz, Phase velocity dispersion and attenuation<br />
<strong>of</strong> seismic waves due to trapped fluids in residual-saturated porous media. submitted<br />
to: Vadose Zone Journal, 2011.<br />
A two scale model for coated hybrid forming tools under thermo-mechanical loading<br />
K.-H. Sauerland, R. Mahnken (<strong>Universität</strong> Paderborn) Schedule<br />
Hybrid forming processes with simultaneous mechanical and thermal loading conditions show a<br />
high potential for mass production <strong>of</strong> functionally graded structures and components [1]. In these<br />
processes the workpiece is loaded once with large deformations, high thermal gradients and phase<br />
transformations while the forming tool is loaded cyclically with small deformations and high<br />
thermal gradients. For protection <strong>of</strong> the forming tool from the high temperatures <strong>of</strong> the hybrid
188 Section 8: Multiscales and homogenization<br />
forming process in the process under consideration coated forming tools are applied, which should<br />
increase the tool lifetime.<br />
This work presents the finite element simulation <strong>of</strong> a coated hybrid forming tool subjected<br />
to thermo-mechanical loading conditions. The coating system consists <strong>of</strong> different coating layers<br />
which are considered on a meso level with particular constitutive equations and particular material<br />
parameters. On a macro level the complete coating system is discretized within one finite element<br />
over the thickness. For scale transitions between macro and meso level the Taylor assumption is<br />
applied for strains and temperatures and volume averaging procedures are applied for stresses<br />
and heat fluxes.<br />
[1] K. Steinh<strong>of</strong>f, H. J. Maier, D. Biermann, Functionally Graded Materials in Industrial Mass<br />
Production, Wissenschaftliche Scripten (2009).<br />
S8.5: Computational homogenization methods Wed, 16:00–18:00<br />
Chair: Holm Altenbach, Rainer Glüge S1|01–A01<br />
Multi-material simulation utilizing the Finite Cell Method<br />
Meysam Joulaian, Alexander Düster (TU Hamburg-Harburg) Schedule<br />
The finite element method (FEM) is a powerful and robust mathematical approach to deal with<br />
a wide variety <strong>of</strong> applications in engineering and science. Yet, fulfilling many prerequisites <strong>of</strong> this<br />
method, such as generating an appropriate mesh, in the case <strong>of</strong> complex geometries is computationally<br />
expensive. In addition, modeling problems with discontinuous or singular solutions is<br />
always a challenging task. Therefore, considerable effort has been devoted to circumvent these<br />
difficulties in an elegant way. Recently, new categories <strong>of</strong> this method, such as element free methods,<br />
partition <strong>of</strong> unity (PUM) based methods and the finite cell method (FCM), have been<br />
proposed to maintain the accuracy and increase the versatility <strong>of</strong> the FEM. The FCM is a new<br />
method, which uses the p-version FEM on Cartesian grids composed <strong>of</strong> rectangular cells that not<br />
necessarily coincide with the boundaries <strong>of</strong> the geometry. This method has an inherent capacity<br />
to easily handle linear and nonlinear problems with complicated geometries in 2D and 3D [1, 2].<br />
Furthermore, thanks to the use <strong>of</strong> high order shape functions in this method, a high rate <strong>of</strong> convergence<br />
is achievable. This method has successfully been applied in simulating various problems<br />
such as biomechanical applications, homogenization and topology optimization.<br />
Despite the accuracy and simplicity <strong>of</strong> the FCM, there is still an open area <strong>of</strong> research for<br />
modeling multi-material interfaces using this method. Considering heterogeneous problems including<br />
different materials, the solution features weak discontinuities introduced at the material<br />
interfaces which need to be resolved in order to obtain reliable results. For the purpose <strong>of</strong> our<br />
discussion, we thoroughly address this problem in the original version <strong>of</strong> the FCM and investigate<br />
possible remedies that fit effectively into the FCM framework. Different approaches including<br />
domain decomposition methods, the hp-d method, local enrichment, as well as their combinations<br />
are considered. The advantages and disadvantages <strong>of</strong> each method are investigated and an<br />
appropriate solution is suggested. Finally, some numerical examples are presented to investigate<br />
performance <strong>of</strong> the method.<br />
Keywords<br />
Finite cell method, discontinuity, local enrichment, hp-d method<br />
[1] J. Parvizian, A. Düster, and E. Rank. Finite cell method – h- and p-extension for embedded<br />
domain problems in solid mechanics.Computational Mechanics 41 (2007), 121–133.
Section 8: Multiscales and homogenization 189<br />
[2] A. Düster, J. Parvizian, Z. Yang, and E. Rank. The finite cell method for three-dimensional<br />
problems <strong>of</strong> solid mechanics.Computer Methods in Applied Mechanics and Engineering 197<br />
(2008) 3768–3782.<br />
Computational homogenization <strong>of</strong> materials with small deformation to determine<br />
configurational forces<br />
Md Khalaquzzaman, Ralf Müller (TU Kaiserslautern), Bai-Xiang Xu (TU <strong>Darmstadt</strong>) Schedule<br />
Computational homogenization has become increasingly important in determining the macroscopic<br />
material response <strong>of</strong> inhomogeneous materials, e.g. piezoelectric materials. In this work,<br />
two-scale classical (first-order) homogenization <strong>of</strong> materials for mechanical response using a FE 2 -<br />
approach is discussed. The literature shows that the strain tensor is <strong>of</strong>ten used for small deformation<br />
problem to determine the boundary conditions for the boundary value problem on the<br />
micro level. Use <strong>of</strong> this boundary condition gives consistent homogenized mechanical quantities,<br />
e.g. stress tensor as well as elasticity tensor, but it does not produce consistent results for configurational<br />
forces. Here, it is shown that the use <strong>of</strong> the displacement gradient for the determination<br />
<strong>of</strong> the boundary conditions <strong>of</strong> the micro problem is the appropriate one to determine homogenized<br />
configurational forces. The homogenized coefficients <strong>of</strong> the elastic tensor for small strain<br />
are explicitly formulated. Different representative volume elements (RVEs) are used to capture<br />
the inhomogeneities <strong>of</strong> the microstructure <strong>of</strong> the material. Based on the multiscale model and<br />
the homogenized configurational force, the mode-I crack problem <strong>of</strong> a microstructured material<br />
is simulated. The effect <strong>of</strong> the different microstructures on configurational forces at the crack tip<br />
is investigated.<br />
Comparison <strong>of</strong> different boundary conditions on spheric and cubic RVE<br />
Rainer Glüge, Martin Weber, Albrecht Bertram (<strong>Universität</strong> Magdeburg) Schedule<br />
The representative volume element (RVE) technique is routinely used to compute the macroscale<br />
material properties <strong>of</strong> a micro-structured material. In this talk, the influence <strong>of</strong> the shape <strong>of</strong><br />
the RVE on the quality <strong>of</strong> the results is investigated. Specifically, the performance <strong>of</strong> cubic and<br />
spherical RVEs is compared. Spherical RVEs have a better surface to volume ratio, allowing for<br />
a minimization <strong>of</strong> the influence <strong>of</strong> the choosen boundary conditions. Also, unlike a cubic RVE,<br />
no anisotropy is induced into a spherical RVE. The two latter issues are quantified, using an<br />
elasto-plastic matrix-inclusion material.<br />
Computational Homogenization for Linear and Nonlinear Heat Conduction in Concrete<br />
Tao Wu (<strong>Universität</strong> Hannover), İlker Temizer (Bilkent University), Peter Wriggers (<strong>Universität</strong><br />
Hannover) Schedule<br />
Concrete is an extremely complex heterogeneous material with a random microstructure at different<br />
length scales. It is critical to investigate heat conduction at different scales <strong>of</strong> concrete in<br />
engineering applications, such as fire resistance, deterioration due to high temperature exposure<br />
and so on. In this contribution, a three-scale framework <strong>of</strong> computational thermal homogenization<br />
for linear and nonlinear cases are carried out. First <strong>of</strong> all, the homogenization process is implemented<br />
at the microscale, and then the resulting effective quantity could be directly applied to<br />
thermal homogenization at the mesoscale, which specifically yields the multiscale framework <strong>of</strong><br />
thermal analysis in concrete.<br />
At the microscale <strong>of</strong> cement paste, computational thermal homogenizaiton with statistical tests<br />
are implemented in the mesh from 3D micro CT-scans with a resolution <strong>of</strong> 1 µm. The principle
190 Section 8: Multiscales and homogenization<br />
<strong>of</strong> partitioning is used to prove numerical results with different types <strong>of</strong> boundary conditions. On<br />
the other hand, aggregates with a random distribution embedded in a homogenized cement paste<br />
matrix is used for the mesoscale thermal homogenization. Each step simulation is strictly verified<br />
through available experimental data. Finally, nonlinear effects arising from various physical<br />
mechanisms such as pore radiation, dehydration, microcracking etc, will be considered within a<br />
thermodynamically consistent homogenization framework.<br />
Thermodynamically Consistent Thermo-Mechanical Micro-Macro-Structural FE 2<br />
Scheme for Thermo-Elasto-J2-Plastic Solids Exhibiting Solid-State Phase Transformations<br />
- Application to Ti6Al4V<br />
Benjamin Regener, Christian Krempaszky, Ewald Werner (TU München), Martin Stockinger<br />
(BOHLER Forging, Kapfenberg, Austria) Schedule<br />
Titanium alloys generally and the alloy Ti6Al4V in particular possess an exceptionally high<br />
strength to density ratio with superior durability at elevated temperatures. This predestines<br />
Ti6Al4V for applications in highly stressed jet engine rotating components such as fans, blades<br />
and disks within the low- and high-pressure compressor units <strong>of</strong> jet engines. These components<br />
typically originate from complex production routes involving multi-stage thermomechanical processing.<br />
Thus the macrosopic material performance is governed by the morphology, constitutive<br />
behaviour and deformation history <strong>of</strong> the microstructural constituents.<br />
To gain a physically based understanding <strong>of</strong> the evolution <strong>of</strong> microscale heterogeneities and residual<br />
stresses in aircraft components, a fully coupled thermomechanical multi-lengthscale finite<br />
element based model is introduced. Each integration point <strong>of</strong> the macro-scale model is coupled<br />
with a periodic micr<strong>of</strong>ield model providing temperature and displacement degrees <strong>of</strong> freedom on<br />
both lengthscales. Processing conditions are applied to the macroscale model representing the<br />
investigated component, whereas the attached microscale models provide the constitutive behaviour<br />
and display the microstructure evolution.<br />
The microstructure evolution <strong>of</strong> Ti6Al4V during thermomechanical processing is modelled morphologically<br />
by a differential Johnson-Mehl tessellation for the primary and secondary α-phase.<br />
The nucleation sites and times result from two heterogeneous Poisson point processes with<br />
temperature-dependent intensity. The microstructure evolution is tracked individually for each<br />
micro-constituent in an integral sense by means <strong>of</strong> the Minkowski functionals estimated at high<br />
accuracy using a spatial lattice.<br />
In order to maintain a fair ratio <strong>of</strong> computational costs to benefits, a thorough investigation <strong>of</strong> the<br />
micromodels with respect to numerical convergence and representativity is carried out. Furthermore,<br />
different meshing techniques and their influence on homogenised and local field quantities<br />
is quantified.<br />
Inelastic analysis <strong>of</strong> polycrystals based on Voronoi tessellation<br />
Oleksandr Prygorniev, Konstantin Naumenko, Holm Altenbach (<strong>Universität</strong> Magdeburg) Schedule<br />
In this work algorithms are presented to generate finite element polycrystal models based on<br />
Voronoi tessellation. They include a polycrystal unit cell, a uni-axial specimen and a circumferentially<br />
notched specimen. The behavior <strong>of</strong> a grain is governed by the anisotropic elasticity with<br />
the cubic symmetry. For the inelastic strain rate tensor the anisotropic power law type function <strong>of</strong><br />
the stress tensor is utilized. Benchmark problems are proposed to verify the developed numerical<br />
techniques including the quality <strong>of</strong> the mesh and accuracy <strong>of</strong> the implicit time step procedure.
Section 8: Multiscales and homogenization 191<br />
S8.6: Dislocation dynamics and polycrystals Thu, 13:30–15:30<br />
Chair: Malek Homayonifar, Thomas Hochrainer S1|01–A01<br />
Higher order alignment tensors in continuum dislocation dynamics<br />
Thomas Hochrainer (<strong>Universität</strong> Bremen), Michael Zaiser (University <strong>of</strong> Edinburgh), Stefan<br />
Sandfeld (KIT) Schedule<br />
Crystal plasticity is mainly mediated by the motion <strong>of</strong> line like crystal defects called dislocations.<br />
Continuum descriptions <strong>of</strong> dislocations reentered the focus <strong>of</strong> continuum mechanics after<br />
the partly known and partly newly discovered size-effects in crystal plasticity became relevant in<br />
micro- and nanotechnology. Because the dislocation density tensor is given by a suitable curl <strong>of</strong><br />
the plastic distortion tensor, its consideration in constitutive equations renders resulting theories<br />
size-dependent. That the dislocation density tensor can be obtained via a curl operation may<br />
have obstructed its nature as a statistical object which may be obtained from averaging actual<br />
dislocation configurations. In the current talk we derive the scalar total dislocation density and<br />
the dislocation density tensor from statistical averages and clarify theirs nature as the first two<br />
terms in a tensor expansion <strong>of</strong> dislocation density distributions. Theses tensors are known as<br />
alignment tensors in the theory <strong>of</strong> liquid crystals. From a higher dimensional dislocation density<br />
theory [1] we derive a hierarchy <strong>of</strong> evolution equations for the dislocation density tensors <strong>of</strong> all<br />
orders which are coupled to the evolution equations for a similar tensor expansion <strong>of</strong> the dislocation<br />
curvature. Assumptions for terminating the tensor expansions at low order are discussed<br />
and their implications are illustrated at numerical examples.<br />
[1] T. Hochrainer, M. Zaiser, P. Gumbsch, A three-dimensional continuum theory <strong>of</strong> dislocation<br />
systems: kinematics and mean-field formulation, Philos. Mag. 87, 8–9 (2007), 1261 – 1282.<br />
Data-driven estimation <strong>of</strong> atomistic support for continuum stress using the Gaussian<br />
mixture model<br />
Sean J. Moran (University <strong>of</strong> Edinburgh), Manfred H. Ulz (TU Graz) Schedule<br />
Recent developments in multiscale modelling include the treatment <strong>of</strong> atomistic scale interactions<br />
via molecular dynamics simulations. While existing methods in solid state physics and continuum<br />
mechanics model their fields very successfully albeit independently <strong>of</strong> each other, bridging those<br />
fields would lead to a fruitful synergy in material science and is therefore an area that is currently<br />
<strong>of</strong> significant interest. The notion <strong>of</strong> stress being an inherent continuum concept at macroscale has<br />
been a matter <strong>of</strong> discussion at microscale. The atomistic stress measure at a given spatial point<br />
contains a space averaging volume over nearby atoms to provide an averaged macroscopic stress<br />
measure. The atoms in this averaging volume are clearly correlated. Consequently the stress and<br />
position data <strong>of</strong> the atoms should implicitly contain this correlation information as well as the<br />
characteristic length <strong>of</strong> the space averaging volume. Previous work on atomistic stress measures<br />
introduce the characteristic length as an a priori given parameter and is therefore by no means<br />
directly determined from the physical problem at hand. In this contribution we motivate the<br />
Gaussian mixture model as a means to estimate the correlation between atoms in our lattice and<br />
therefore to derive the characteristic length <strong>of</strong> the space averaging volume in an entirely data<br />
driven manner. We fit a Gaussian mixture model to our data that captures the distribution <strong>of</strong><br />
subpopulations <strong>of</strong> atoms within the lattice. We learn the maximum likelihood model parameters<br />
using the Expectation Maximization (EM) algorithm. Rather than selecting the number <strong>of</strong> subpopulations<br />
a priori, we learn the optimal subpopulation configuration directly from the data<br />
by searching through the model space for the model which best describes our dataset. To form
192 Section 8: Multiscales and homogenization<br />
a parsimonious representation <strong>of</strong> the dataset we regularise our model search using the Bayesian<br />
Information Criterion (BIC) which maintains an optimal balance between too few and too many<br />
subpopulations <strong>of</strong> atoms through the penalization <strong>of</strong> overly complex (more parameters) models.<br />
The characteristic length is calculated directly from the subpopulations <strong>of</strong> atoms discovered by<br />
the Gaussian mixture model by averaging over the maximum extent <strong>of</strong> each subpopulation. Furthermore<br />
we demonstrate how our model is able to leverage the correlation <strong>of</strong> atoms in the lattice<br />
to calculate the value <strong>of</strong> unknown stress values at given macroscopic continuum positions. Thorough<br />
evaluation is conducted on a numerical example <strong>of</strong> an edge dislocation in a single crystal.<br />
We show that our model is able to derive estimates <strong>of</strong> the atomistic support that are within close<br />
agreement to the corresponding analytical solution.<br />
Towards a general multiscale framework based on Ritzs approximation: Application<br />
to atomistic and continuum models<br />
Malek Homayonifar (TU Dortmund), Jörn Mosler (TU Dortmund, Helmholtz-Zentrum Geesthacht)<br />
Schedule<br />
Material modeling using multiscale methods is in great demand because they allow achievement <strong>of</strong><br />
a higher physical resolution compared to classical continuum models by incorporating the effects<br />
<strong>of</strong> the underling micromechanical processes into the analysis <strong>of</strong> the macroscopic response. The core<br />
ingredients <strong>of</strong> these methods are the scale bridging schemes which can be realized by the relevant<br />
physical assumptions. For instance, a more frequently applied approach for atomistic-continuum<br />
multiscale simulations is the Cauchy-Born rule and the principle <strong>of</strong> energy equivalence. In the<br />
present contribution, a similar approach is proposed, however, with a more relaxed kinematic<br />
constraint and an emphasized numerical efficiency. Within the advocated model, the kinematics<br />
<strong>of</strong> the smaller scale is coupled to that <strong>of</strong> the larger scale in standard manner, i.e. by volume<br />
averaging. Moreover, the principle <strong>of</strong> energy equivalence is approximated by Ritzs method. Accordingly,<br />
the set <strong>of</strong> the larger scales material parameters is chosen which fits the average energy<br />
<strong>of</strong> the lower scale best. The applicability and the efficiency <strong>of</strong> the resulting homogenization approach<br />
are demonstrated by selected numerical examples ranging from the atomistic scale to the<br />
macroscopic scale.<br />
Invariance <strong>of</strong> Parrinello-Rahman molecular dynamics and its relation to continuum<br />
mechanics<br />
Manfred H. Ulz (TU Graz) Schedule<br />
Parrinello-Rahman molecular dynamics [1] has proved to be a reliable technique for the investigation<br />
<strong>of</strong> phase transitions in solids. This type <strong>of</strong> molecular dynamics may lead to a proper<br />
description <strong>of</strong> the atomistic scale in multi-scale analysis <strong>of</strong> engineering problems. However, the<br />
employed Lagrangian in [1] is proposed without a derivation and lacks invariance under modular<br />
transformations.<br />
A reinterpretation <strong>of</strong> the Lagrangian in [1] in terms <strong>of</strong> continuum mechanics can be found in<br />
[2]. The new formulation is derived in a consistent physical manner and only quantities native<br />
to continuum mechanics are incorporated into this Lagrangian. However, numerical examples<br />
demonstrating the performance <strong>of</strong> the proposed model are not provided in [2].<br />
Based on this recent continuum-related derivation, the invariance <strong>of</strong> the new Lagrangian under<br />
modular transformations is investigated. The implication that the obtained dynamics is invariant<br />
to the chosen unit cell agrees with results in solid state physics and is a mandatory requirement<br />
for the suitability <strong>of</strong> multi-scale analysis. We conduct a numerical simulation <strong>of</strong> a phase transition<br />
in nickel which scrutinises the validity <strong>of</strong> the Lagrangian in [2] and its invariance under modular<br />
transformations.
Section 8: Multiscales and homogenization 193<br />
[1] M. Parrinello, A. Rahman, Polymorphic transitions in single crystals: A new molecular dynamics<br />
method, J. Appl. Phys. 52 (1981), 7182–7190.<br />
[2] P. Podio-Guidugli, On (Andersen-)Parrinello-Rahman molecular dynamics, the related metadynamics,<br />
and the use <strong>of</strong> the Cauchy-Born rule, J. Elasticity 100 (2010), 145–153.<br />
S8.7: Damage processes and contact problems Thu, 13:30–15:30<br />
Chair: Julia Orlik, Dorothee Knees S1|01–A02<br />
Derivation <strong>of</strong> an effective damage evolution model using two-scale convergence techniques<br />
Hauke Hanke, Dr. Dorothee Knees (WIAS Berlin) Schedule<br />
This lecture is addressed to the question <strong>of</strong> deriving an effective damage evolution model by investigating<br />
the limit process <strong>of</strong> damage models with a “simple” micro-structure.<br />
Thereto, microscopic damage models are introduced, where there are only two phases <strong>of</strong> material<br />
- damaged and undamaged. This microscopic structure is non-periodic and a regularization for<br />
piecewise constant functions correlated to this microstructure is introduced. Then, classical twoscale<br />
convergence techniques are used to identify an effective damage model, wherein the damage<br />
is described by a damage variable z : [0, T ] × Ω → [0, 1] reflecting the micro-structure induced<br />
by the micro-models. Here, z(t, x) = 1 means that no damage occurs in point x at the time t<br />
and z(t, x) = 0 means the material cannot take any more damage but is still allowed to perform<br />
elastic deformations (i.e. no complete damage).<br />
This approach suggests in which way phenomenological damage models could depend on the damage<br />
variable. Furthermore, anisotropy is allowed in the microscopic damage models, which leads<br />
to an anisotropic limit damage model.<br />
A toy model for dynamic debonding<br />
Giuliano Lazzaroni (<strong>Universität</strong> Würzburg), Renaud Bargellini (EDF RD, Laboratoire de Mécanique<br />
des Structures Industrielles Durables), Pierre-Emmanuel Dumouchel (Peugeot-Citroen<br />
Automobile), Jean-Jacques Marigo (École Polytechnique) Schedule<br />
We study the dynamic debonding <strong>of</strong> a one-dimensional inextensible film, subject to a monotonic<br />
loading and under the hypothesis that the toughness <strong>of</strong> the glue can take only two values. We<br />
first consider the case <strong>of</strong> a single defect <strong>of</strong> small length in the glue where the toughness is lower<br />
than in the remaining part. The dynamic solution is obtained in a closed form and we prove<br />
that it does not converge to the expected quasi-static one when the loading speed tends to zero.<br />
The gap is due to a kinetic energy which appears when the debonding propagates across the<br />
defect at a velocity which is <strong>of</strong> the same order as the sound velocity. The kinetic energy becomes<br />
negligible again only when the debonding has reached a critical distance beyond the defect. The<br />
case <strong>of</strong> many defects is then considered and solved using an exact numerical solution <strong>of</strong> the wave<br />
equation and the Griffith law <strong>of</strong> propagation. The numerical results highlight the effects <strong>of</strong> the<br />
time evolution <strong>of</strong> the kinetic energy which induce alternate phases <strong>of</strong> rapid and slow debonding,<br />
these oscillations depending essentially on the volume fraction <strong>of</strong> the highest toughness.<br />
Multiscale modelling for the simulation <strong>of</strong> damage processes at refractory materials<br />
under thermal shock<br />
Dimitri Henneberg, Andreas Ricoeur (<strong>Universität</strong> Kassel) Schedule
194 Section 8: Multiscales and homogenization<br />
Refractory materials, for example ceramic materials, initially contain a multitude <strong>of</strong> defects such<br />
as voids, microcracks, grain boundaries etc. Particularly for refractory ceramics being exposed<br />
to high temperatures above 1200 C and loaded by thermal shocks, the macroscopic properties<br />
such as effective compliance, strength and lifetime are essentially determined by these microscopic<br />
features <strong>of</strong> the material. The deformation process and failure mechanisms are going along with<br />
the creation <strong>of</strong> new microdefects as well as the growth and coalescence <strong>of</strong> cracks. A brittle damage<br />
model based on multiscale considerations and homogenisation procedures is presented. Cell<br />
models are developed as representative volume elements (RVE) including different microstructural<br />
features. The material laws themselves are formulated on the continuum level. Local failure<br />
occurs if the damage variable reaches a critical value. In order to properly model the thermomechanical<br />
coupling, the temperature-dependence <strong>of</strong> material constants is taken into account.<br />
Moreover, fracture and damage mechanical approaches are combined using different techniques.<br />
Thus, interactions <strong>of</strong> macroscopic crack tips and microstructural features can be taken into account.<br />
Crack face contact within a 3d XFEM multiscale framework<br />
D.S. Mueller-Hoeppe, P. Wriggers, S. Loehnert (<strong>Universität</strong> Hannover) Schedule<br />
Many materials, like e.g. ceramics, exhibit micro cracking in the vicinity <strong>of</strong> a macro crack front.<br />
These micro cracks have a significant influence on the macro crack propagation behavior.<br />
As the micro cracks are in general arbitrarily arranged, crack closure occurs in many cases. The<br />
eXtended Finite Element Method (XFEM), which is a popular method for numerical fracture mechanics,<br />
does not prevent unphysical crack face penetration. As a remedy, [1] develop a contact<br />
formulation which accounts for crack closure in hexahedral XFEM elements. Due to a projection<br />
<strong>of</strong> the contact contribution on the hexahedral element nodes, the introduction <strong>of</strong> additional degrees<br />
<strong>of</strong> freeedom is avoided.<br />
This contact formulation is applied to the XFEM multiscale projection method introduced by [2]<br />
and extended to the three-dimensional case by [3] in order to account for micro crack closure.<br />
[1] D.S. Mueller-Hoeppe, P. Wriggers and S. Loehnert. Crack face contact for a hexahedral-based<br />
XFEM formulation. Submitted to Comput. Mech.<br />
[2] S. Loehnert and T. Belytschko. A multiscale projection method for macro/microcrack simulations.<br />
Int. J. Numer. Meth. Eng., Vol. 71, 1466 -1482, 2007<br />
[3] S. Loehnert and D.S. Mueller-Hoeppe. Multiscale methods for fracturing solids. IUTAM<br />
Symposium on Theoretical, Computational and Modelling Aspects <strong>of</strong> Inelastic Media, 79–<br />
87, 2008<br />
Homogenization via unfolding in periodic elasticity with contact on oscillating interface<br />
J. Orlik (Fraunh<strong>of</strong>er ITWM) Schedule<br />
In this paper, we consider the elasticity problem in a heterogeneous domain with ε−periodic<br />
micro-structure, ε
Section 8: Multiscales and homogenization 195<br />
interface, implying their two-scale convergence. Furthermore, this implies the weak convergence<br />
<strong>of</strong> the nonlinear continuous convex functions applied to these interface jumps.<br />
The limiting problem describes elasto-plasticity, where the micro-sliding on the oscillating<br />
interface reasons plastic deformations, determined by solving a local contact elasticity problems on<br />
the standard periodicity cell. The multiscale algorithm provides an effort for numerical solution <strong>of</strong><br />
periodic multiphase problems containing multiple contact in their microstructure. It is illustrated<br />
by simulation <strong>of</strong> the effective properties <strong>of</strong> two fabric materials.<br />
[1] D. Cioranescu, A. Damlamian and G. Griso: Periodic unfolding and homogenization, C. R.<br />
Acad. Sci. Paris, Ser. I, 335 (2002), 99-104.<br />
[2] Damlamian, A.: An elementary introduction to periodic unfolding, Multi Scale Problems and<br />
Asymptotic Analysis 24 (2005), 119-136.<br />
Asymptotics for thin elastic fibers in contact<br />
Zoufine Bare, Julia Orlik (Fraunh<strong>of</strong>er-ITWM) Schedule<br />
In this work a 3-D uni-lateral contact elasticity problem for a thin fiber with a rigid foundation<br />
is studied. We approximate the contact condition by a linear Robin-boundary-condition (by<br />
meaning <strong>of</strong> the penalized and linearized non-penetration and friction conditions, [1]). The Robin<br />
parameters are scaled differently in the longitudinal and cross-sectional directions. The dimension<br />
<strong>of</strong> the problem is reduced by a standard ([2], [3]) formal asymptotic approach with an additional<br />
expansion suggested to fulfill the contact conditions. The 3-D contact conditions result into<br />
1-D Robin-boundary-conditions for corresponding 1-D PDEs. The Robin-coefficients <strong>of</strong> the 1-D<br />
problem depend on the ones from the 3-D statement, on the cross-section <strong>of</strong> the fiber and on the<br />
solution <strong>of</strong> auxiliary problems in the boundary layer. The error is estimated and the theoretical<br />
results are illustrated by a numerical comparison <strong>of</strong> the solutions to the contact problems for 3-D<br />
and 1-D beams for validation.<br />
[1] Kikuchi, N and Oden, J.T.:Contact problems in elasticity: A study <strong>of</strong> variational inequalities<br />
and finite elements methods, SIAM, USA, 1988.<br />
[2] Panasenko, G.: Multi-scale modelling for structures and composites, Springer, 2005.<br />
[3] Trabucho, L. and Viano, J.M.: Mathematical modelling <strong>of</strong> rods, Handbook <strong>of</strong> Numerical<br />
Analysis, Vol. IV, 1996.<br />
S8.8: Composites and fiber-reinforced structures Thu, 16:00–18:00<br />
Chair: Udo Nackenhorst, Robert Fleischhauer S1|01–A01<br />
FE 2 Modelling <strong>of</strong> laminated plates<br />
Cécile Helfen, Stefan Diebels (<strong>Universität</strong> des Saarlandes) Schedule<br />
Laminated plates are nowadays widely used, especially in transport and automobile industry.<br />
However, their mechanical behaviour is complex and a multi-scale consideration proved to be<br />
useful. In the scope <strong>of</strong> this work, the modelling <strong>of</strong> the mechanical behaviour <strong>of</strong> a hybrid sandwich<br />
laminate under bending is made with a numerical homogenisation.<br />
The principle <strong>of</strong> a numerical homogenisation (or so-called FE 2 ) for plates is based on the<br />
separation <strong>of</strong> the investigated problem into different scales. Whereas the macroscale is defined
196 Section 8: Multiscales and homogenization<br />
as a plate, the mesoscale is computed as a three dimensional problem discretizing the different<br />
layers stacking order. A first Finite Element computation is made on the macroscale, which<br />
is following the plate kinematics and resolving the balance equation <strong>of</strong> the plate. From each<br />
integration point, the deformations are projected to the mesoscale, where an other Finite Element<br />
computation is made. On this level, a Representative Volume Element (RVE) is defined, resolving<br />
the different layers <strong>of</strong> the laminate and a local boundary value problem is solved. Then, the<br />
macroscopic forces, moments and hyperstresses are computed as stress resultants and higherorder<br />
stress resultants from the mesoscopic stresses and transferred back in the macroscale. At<br />
this stage, the macroscale is following a plate theory with thickness change enabling better results<br />
as the classical theories <strong>of</strong> Reissner-Mindlin or Love-Kirchh<strong>of</strong>f, especially towards the shear forces.<br />
Concerning the mesoscale, it resolves a three dimensional boundary value problem incorporating<br />
non-linear material behaviour.<br />
Further improvements has to be made concerning the contact interface between the different<br />
layers.<br />
Numerical aspects on computational homogenization <strong>of</strong> epoxy/glass composites<br />
Robert Fleischhauer, Hüsnü Dal, Michael Kaliske (TU Dresden) Schedule<br />
Numerical aspects <strong>of</strong> two-scale modeling <strong>of</strong> epoxy/glass composites are presented. Special focus<br />
is given to the use <strong>of</strong> a computational homogenization scheme and the micromechanical modeling<br />
<strong>of</strong> interphases and interfaces. The homogenization process is carried out under consideration <strong>of</strong><br />
periodic boundary constraints <strong>of</strong> the representative volume element (RVE) due to the periodic<br />
structure <strong>of</strong> glassfiber reinforced epoxy systems. Generally, the homogenization process employed<br />
is based on an internal variable formulation for the constitutive model <strong>of</strong> inelastic materials.<br />
An objective energy storage function is needed to derive micro-stresses and micro-moduli. The<br />
numerical treatment <strong>of</strong> the micro-scale requires the incremental stress potential function, that is<br />
the result <strong>of</strong> the solution <strong>of</strong> the minimization problem <strong>of</strong> the constitutive response <strong>of</strong> standard<br />
dissipative materials. Therein, the stored and dissipated energy is minimized within a finite increment<br />
<strong>of</strong> time, with respect to the internal state <strong>of</strong> the material. It provides the potential for the<br />
micro-stresses at the end <strong>of</strong> the current time step. The deformation <strong>of</strong> the microstructure is assumed<br />
to be driven by a prescribed macro-deformation and a superimposed micro-scale fluctuation<br />
field. The fluctuation field has to vanish in an averaged sense over the surface <strong>of</strong> the RVE. This<br />
constraint is fulfilled demanding e.g. periodic deformations on the boundary <strong>of</strong> the microstructure.<br />
Therewith, it is possible to achieve the linking <strong>of</strong> the periodicity constraint to the energy<br />
minimization problem by using a Lagrange multiplier method. Numerical aspects <strong>of</strong> solving this<br />
minimization problem are presented. Due to protective coating <strong>of</strong> fibers and chemical reactions<br />
during the manufacturing process, interphases between bulk- and fiber material build up. In order<br />
to simulate the overall macroscopic mechanical response <strong>of</strong> an epoxy/glass composite, we present<br />
a constitutive model to couple the newly developed mechanical material model for epoxy with the<br />
hyperelastic Neo-Hookean glass fiber material under consideration <strong>of</strong> the designated failure layer.<br />
Two-scale simulations are carried out for RVEs with and without interface/interphase interaction<br />
and the comparison <strong>of</strong> the results will be presented.<br />
A stochastic procedure for the homogenization <strong>of</strong> damaging composites<br />
André Hürkamp, Udo Nackenhorst (<strong>Universität</strong> Hannover) Schedule<br />
The mechanical properties <strong>of</strong> materials are mainly influenced by the microstructure. In particular,<br />
the global phenomena like fatigue and fracture start at the microscale. Randomly distributed<br />
initial microcracks or other defects are the source <strong>of</strong> fatigue. Regarding composite materials also<br />
the combination <strong>of</strong> different materials obeys uncertainties. The arrangement <strong>of</strong> all <strong>of</strong> these inho-
Section 8: Multiscales and homogenization 197<br />
mogeneities is a random process. In order to give precise information about the global mechanical<br />
properties, a possible degradation or the risk <strong>of</strong> failure, the microstructure has to be described<br />
with the aid <strong>of</strong> related statistical methods.<br />
Exemplarily, investigations on short fibre reinforced concrete are made. Its microstructure can be<br />
described by a matrix material <strong>of</strong> concrete which includes randomly distributed microcracks and<br />
short fibres <strong>of</strong> steel. Additionally, the material parameters itself are assumed to be random, so that<br />
a multidimensional stochastic problem is obtained. Classical analytical homogenization schemes<br />
like the Mori-Tanaka-Method or the self-consistent scheme are extended with statistical methods.<br />
In that way, we are able to compute effective material properties with respect to their statistics.<br />
The statistics for the homogenization are captured by advanced Monte-Carlo simulations using a<br />
Latin Hypercube sampling.<br />
For the further processing <strong>of</strong> the homogenized material model a spatial random field is generated<br />
using the Karhunen-Loève expansion.<br />
Tolerance modeling <strong>of</strong> heat conduction in bidirectional gradedthin walled cellular<br />
structures.<br />
Eugeniusz Baron, Sylwia Czarnecka (Silesian University <strong>of</strong> Technology) Schedule<br />
The aim <strong>of</strong> this contribution is to formulate a certain new mathematical model for the analysis <strong>of</strong><br />
heat conduction In functionally graded plane lattice composite structure. The composite consists<br />
<strong>of</strong> two isotropic components, with very different thermo mechanical properties, constituting a thin<br />
walled skeleton and a matrix. The structure is homogeneous in direction normal to its mid-plane.<br />
The proposed model describes the behavior <strong>of</strong> the composite on the macroscopic level i.e.<br />
by means <strong>of</strong> partial differential equation with smooth coefficients. The model <strong>of</strong> equation has<br />
a simple analytical form obtained under certain simplified heuristic assumptions. Obviously, for<br />
the composite under consideration there are partial differential equations with highly oscillating<br />
functional coefficients.<br />
The modeling method is based on the tolerance averaging procedure. This procedure was<br />
investigated and discussed in a series <strong>of</strong> papers and summarized in [1]. This contribution introduces<br />
a certain revisited tolerance averaging technique foundation <strong>of</strong> which will be exposed <strong>of</strong> the<br />
83 <strong>GAMM</strong> conference in a separate presentation [2]. The modeling procedure applied in this<br />
contribution also takes into account the new concept <strong>of</strong> a virtual cell and a local shape functions.<br />
They are concepts which make it possible to describe functionally graded (non periodic) structure<br />
<strong>of</strong> the skeleton lattice.<br />
The proposed tolerance modeling procedure is based on new heuristic assumption. It states<br />
that heat flux along every family <strong>of</strong> parallel lattice walls can be treated as independent <strong>of</strong> the<br />
thickness <strong>of</strong> these walls. This is a good approximation, provided that the walls are sufficiently<br />
thin.<br />
In the contribution there are obtained two model equations for the averaged temperature field<br />
and that is called the fluctuation amplitude <strong>of</strong> temperature field. These equations have smooth<br />
functional coefficients and stand for the basis <strong>of</strong> analysis for specific engineering problems.<br />
[1] Woźniak Cz., [ed.], 2008, Termomechanics <strong>of</strong> Micro heterogeneous Solids and Structures,<br />
Łódź, Wydawnictwo Politechniki Łódzkiej.<br />
[2] Nagórko W., Woźniak Cz., <strong>2012</strong>, On a certain model <strong>of</strong> heat conduction in laminated media<br />
with interlaminar defects, 83 <strong>GAMM</strong> Conference.
198 Section 8: Multiscales and homogenization<br />
A model <strong>of</strong> the heat conduction in functionally graded laminates with interlaminar<br />
defects<br />
Czesław Woźniak (Technical University <strong>of</strong> Lodz), Monika Wągrowska (Warsaw University <strong>of</strong> Life<br />
Sciences) Schedule<br />
Modelling and analysis <strong>of</strong> laminates with non ideal contact between adjacent laminae are not<br />
new problems in thermomechanics. So far, one can mention here a list <strong>of</strong> contributions by A.<br />
Kaczyński, S.J. Matysiak, V.J. Pauk, [1] and many others in which a single interlaminar defect<br />
as well as systems <strong>of</strong> these effects were discussed. Term defect stands here for a crack and/or a<br />
thin inclusion. Alternative modelling approaches, which also take into account the delamination<br />
problem, were proposed by Z. Naniewicz, Cz. Woźniak, [2]. At the same time the unilateral contact<br />
between adjacent laminae was studied by M. Woźniak, [3].<br />
In this contribution the object <strong>of</strong> analysis will be restricted to the heat conduction in two<br />
component functionally graded laminates. The non ideal contact between adjacent laminas is<br />
modelled by sufficiently thin interlaminar inclusion. Term sufficiently thin suggests the applicability<br />
<strong>of</strong> a specific tolerance asymptotic modelling. This approach was recently investigated by Cz.<br />
Woźniak and M. Wągrowska, [4].<br />
The aim <strong>of</strong> this presentation is to propose a certain refined version <strong>of</strong> a tolerance asymptotic<br />
modelling procedure.<br />
[1] Kaczyński A., Matysiak S. J., Pauk V. J., 1995: Stress intensity factors for an interface<br />
penny-shope crack in laminated elastic layer, J. Theor. Appl. Mech., 33, 361-373.<br />
[2] Naniewicz Z., Woźniak Cz., 1988: On the quasi-stationary models <strong>of</strong> debonding processes in<br />
layered composites, Ing. Arch., 58, 403-412.<br />
[3] Woźniak M., 1995: On the dynamic behaviour <strong>of</strong> micro- demaged stratified media, Int. J.<br />
Fract., 73, 223-232.<br />
[4] Cz. Woźniak, M.Wągrowska, Asymptotic modelling <strong>of</strong> some functionally graded materials,<br />
PAMM Proc. Appl. Math. Mech., 10, 349-350, 2010.<br />
Multiscale failure modeling <strong>of</strong> composites using generalized finite element method<br />
Mahendra Kumar Pal, Amirtham Rajagopal (Indian Institute <strong>of</strong> Technology Hyderabad) Schedule<br />
In this work multiscale Generalized Finite Element Method (GFEM) is used for failure modeling<br />
<strong>of</strong> laminated composites. The GFEM [1] is used to construct higher order function spaces for the<br />
solution <strong>of</strong> partial differential equations. The enrichment functions for the GFEM approximation<br />
are computed using a Proper Orthogonal Decomposition (POD) technique [2]. Higher accuracy is<br />
achieved through addition <strong>of</strong> enrichment functions to the classical finite element basis functions.<br />
The approximation is then used in a Galerkin scheme for multiscale failure analysis <strong>of</strong> composites.<br />
Numerical examples are presented to demonstrate the multiscale failure modeling <strong>of</strong> composites.<br />
[1] J. M. Melnek, I. Babuska, The partition <strong>of</strong> unity finite element method, Computer Methods<br />
in Applied Mechanics and Engineering, 139, pp. 289-314, 1996.<br />
[2] W. Aquino, J. B. Brigham, C. J. Earls, N. Sukumar, Generalized finite element method<br />
using proper orthogonal decomposition, International Journal for Numerical Methods in<br />
Engineering, 79(7), pp. 887-906, 2008.
Section 9: Laminar flows and transition 199<br />
Section 9: Laminar flows and transition<br />
Organizers: Suad Jakirlic (TU <strong>Darmstadt</strong>), Ulrich Rist (<strong>Universität</strong> Stuttgart)<br />
S9.1: Laminar flows and transition I Tue, 13:30–15:30<br />
Chair: Suad Jakirlic, Ulrich Rist S1|01–A2<br />
Transition Prediction and Modeling in External Flows Using RANS-based CFD Codes<br />
Andreas Krumbein, Normann Krimmelbein, Cornelia Seyfert (DLR Göttingen) Schedule<br />
Besides wind tunnel testing and flight tests, CFD simulation based on RANS solvers has become<br />
a standard design approach in industry for the design <strong>of</strong> aircraft. For the design point <strong>of</strong> aircraft<br />
a positive assessment <strong>of</strong> the numerical results was achieved for many validation and application<br />
tests and the prediction capabilities <strong>of</strong> the s<strong>of</strong>tware tools could be positively evaluated. As<br />
a consequence, high confidence in numerical simulations could be achieved in industry and will<br />
eventually allow more simulation and less physical testing. However, and despite <strong>of</strong> the progress<br />
that has been made in the development and application <strong>of</strong> RANS-based CFD codes, there is still<br />
the need for improvement, for example, with regard to the capability <strong>of</strong> a proper capturing <strong>of</strong> all<br />
relevant physical phenomena. This can only be achieved if capable and accurate physical models<br />
are available in the codes. On the one hand, the combined use <strong>of</strong> turbulence and transition models<br />
is indispensable for flows exhibiting separation, because otherwise the close interaction between<br />
the laminar-turbulent transition and its impact on flow separation is not reproduced. On the other<br />
hand, it is not possible to fully exploit the high potential <strong>of</strong> todays advanced turbulence models<br />
if transition is not taken into account. Thus, in modern high-fidelity CFD codes a robust transition<br />
prediction and modeling must be established together with reliable and effective turbulence<br />
models.<br />
At DLR, the RANS codes for external flows, [1]-[2], have been provided with transition prediction<br />
and modeling functionalities which can be applied to three-dimensional aircraft configurations.<br />
Two different basic approaches are currently at hand: the streamline based and the transport<br />
equation approach.<br />
The streamline based approach uses information from the current flow solution along defined<br />
integration paths in order to compute the laminar boundary layers, either using a laminar<br />
boundary-layer method or by direct extraction from the RANS solution. A fully automated, local<br />
linear stability code analyses the laminar boundary layers and detects transition due to Tollmien-<br />
Schlichting or cross flow instabilities. The stability code, which applies the e N -method, [3]-[4], and<br />
the two N factor approach, [5], for the determination <strong>of</strong> the transition points, uses a frequency estimator<br />
for the detection <strong>of</strong> the relevant regions <strong>of</strong> amplified disturbances for Tollmien-Schlichting<br />
instabilities and a wave length estimator for cross flow instabilities. Also separation induced transition<br />
is covered. Alternatively, different empirical transition criteria for streamwise and crossflow<br />
transition are available and, in addition, criteria for attachment-line and by-pass transition. Using<br />
this approach transition is predicted either along spanwise line-in-flight cuts through a wing or<br />
along the boundary-layer edge streamline. The latter is the only possible way in the case <strong>of</strong> fully<br />
three-dimensional flow about fuselages or nacelles. The streamline approach has been validated<br />
by numerous test cases and is the standard transition prediction approach currently used in production<br />
simulation. Here, it is usually applied in parallel mode on large compute cluster systems,<br />
[6].<br />
The transport equation approach, [7], is relatively new and based exclusively on local variables<br />
so that it is inherently parallelizable and, thus, very well suited for unstructured CFD codes and
200 Section 9: Laminar flows and transition<br />
large applications which can only be tackled by massively parallel computations. The boundarylayer<br />
quantities are resolved by the RANS computational grid and approximated by the modeling<br />
approach reflected by two transport equations. The prediction <strong>of</strong> the locations <strong>of</strong> transition onset<br />
is based on empirical criteria which can and must be evaluated locally. While the original model<br />
formulation was restricted to the prediction <strong>of</strong> streamwise transition mechanisms the model is<br />
currently extended in order to predict crossflow transition, [8].<br />
The two different approaches and methods will be presented and explained, their applicability<br />
ranges are discussed and numerical results are compared to a number <strong>of</strong> validation test cases demonstrating<br />
the prediction accuracy <strong>of</strong> the different methods. The results from the application <strong>of</strong><br />
the methods to large and partially very complex, industrial configurations are presented and discussed.<br />
Eventually, an outlook is given to the challenges placed by complex aircraft configurations<br />
and to the way forward to tackle the still open issues.<br />
[1] Krumbein, A., Automatic Transition Prediction and Application to Three-Dimensional Wing<br />
Configurations, Journal <strong>of</strong> Aircraft, Vol. 44, No. 1, 2007, pp. 119-133; also: AIAA Paper<br />
2006-914, January 2006.<br />
[2] Krimmelbein, N., Radespiel, R., Transition prediction for three-dimensional flows using parallel<br />
computation, Computers Fluids, No. 38, Elsevier, 2009, pp. 121-136, doi:10.1016/j.compfluid.2008.<br />
01.004.<br />
[3] Smith, A.M.O., Gamberoni, N., Transition, Pressure Gradient and Stability Theory, Douglas<br />
Aircraft Company, Long Beach, Calif. Rep. ES 26388, 1956.<br />
[4] van Ingen, J.L., A suggested Semi-Empirical Method for the Calculation <strong>of</strong> the Boundary<br />
Layer Transition Region, University <strong>of</strong> Delft, Dept. <strong>of</strong> Aerospace Engineering, Delft, The<br />
Netherlands, Rep. VTH-74, 1956.<br />
[5] Rozendaal, R. A., Natural Laminar Flow Flight Experiments on a Swept Wing Business<br />
Jet-Boundary-Layer Stability Analysis, NASA CP 3975, March 1986.<br />
[6] Krimmelbein, N., Krumbein, A., Automatic Transition Prediction for Three-Dimensional<br />
Configurations with Focus on Industrial Application, AIAA-2010-4292, 40th AIAA Fluid<br />
Dynamics Conference and Exhibit, June 28 July 1, 2010, Chicago, Illinois, USA.<br />
[7] Langtry, R.B., Menter, F.R., Correlation-Based Transition Modeling for Unstructured Parallelized<br />
Computational Fluid Dynamics Codes, AIAA Journal, Vol. 47, No.12, 2009, pp.<br />
2894-2906, DOI: 10.2514/1.42362.<br />
[8] Seyfert, C., Krumbein, A., Correlation-Based Transition Transport Modeling for Three-<br />
Dimensional Aerodynamic Configurations, to be presented as AIAA paper at the 50th<br />
Aerospace Sciences Meeting, 9-12 January <strong>2012</strong>, Nashville, Tennessee, USA.<br />
Preliminary results <strong>of</strong> the conditional analysis <strong>of</strong> wall friction during laminarturbulent<br />
transition <strong>of</strong> a rough wall boundary layer<br />
Pavel Jonás, Ondřej Hladík, Oton Mazur, Václav Uruba (Czech Academy <strong>of</strong> Sciences Praha)<br />
Schedule<br />
The transitional intermittency is investigated in the zero pressure gradient boundary layer developing<br />
on the surface covered with sand paper (grits 60). The free stream mean velocity is 5 m/s
Section 9: Laminar flows and transition 201<br />
and the turbulence level is either 0.3 percent or risen by means <strong>of</strong> the square mesh plane grid to<br />
3 percent and the dissipation length parameter 3.8 mm.<br />
Records (25 kHz, 750000 samples, 16 bit) <strong>of</strong> the instantaneous wall friction in various locations<br />
are evaluated from the records <strong>of</strong> the single wall wire CTA output signal. The procedure <strong>of</strong> the<br />
constant temperature anemometer signal transformation to the wall friction has been developed<br />
formerly and presented in [1, 2]. The adjustment <strong>of</strong> this procedure to rough surface conditions<br />
is based on the mean wall friction distribution which has been determined in advance. This<br />
procedure is described in the paper.<br />
Then the transitional intermittency factor distribution is derived by means <strong>of</strong> the TERA<br />
method [3]. Next the conditional analysis <strong>of</strong> the wall friction records is done which sorts the wall<br />
friction records in passages with the non-turbulent structure (intermittency factor g = 0) and<br />
those with the full turbulent structure (g = 1).<br />
Evaluated are the probability density function and the conditioned probability density functions<br />
<strong>of</strong> the wall friction, relevant moments and the mean residence time <strong>of</strong> the wall friction in<br />
laminar and turbulent state. Results are compared with analogous characteristics received during<br />
investigations <strong>of</strong> smooth wall boundary layers.<br />
[1] Jonás, P. - Mazur, O. - Uruba, V. (1999) Statistical characteristics <strong>of</strong> the wall friction in a<br />
flat plate boundary layer through by-pass transition. ZAMM 79, S3, S691-S692.<br />
[2] Jonás, P. - Mazur, O. - Uruba, V. (2002) Problem <strong>of</strong> the intermittency distributions in<br />
transitional boundary layers under flows with various scales <strong>of</strong> turbulence. PAMM, Proc.<br />
Appl. Math. Mech. 1, Section 10.5, 298-299.<br />
[3] Zhang, D.H. - Chew, Y.T. - Winoto, S.H.: (1996) Investigation <strong>of</strong> intermittency measurement<br />
methods for transitional boundary, Exp. Thermal and Fluid Sci. 12, 433-443.<br />
Velocity and shear stress distributions in laminar-turbulent transition <strong>of</strong> unsteady<br />
boundary layer on aer<strong>of</strong>oil in high accelerating and decelerating fluid flow<br />
Decan J. Ivanovic, Vladan M. Ivanović (University <strong>of</strong> Montenegro, Podgorica) Schedule<br />
The corresponding equations <strong>of</strong> unsteady boundary layer, by introducing the appropriate variable<br />
transformations, momentum and energy equations and similarity parameters set, being transformed<br />
into generalized form. These parameters are expressing the influence <strong>of</strong> the outer flow velocity<br />
and the flow history in boundary layer, on the boundary layer characteristics. Since the generalized<br />
equation contain summ <strong>of</strong> terms equal to the number <strong>of</strong> parameters, it is necessary to limit<br />
the number <strong>of</strong> parameters for numerical integration. The numerical integration <strong>of</strong> the generalized<br />
equation with boundary conditions has been performed by means <strong>of</strong> the difference schemes and<br />
by using Tridiagonal Algorithm Method with iterations in the two once localized approximation,<br />
where the first unsteady and dynamic parameter will remaine, while all others will be let to be<br />
equal to zero, and where the derivatives with respect to the first unsteady parameter will be<br />
considered equal to zero. So obtained generalized solutions are used to calculate the distributions<br />
<strong>of</strong> velocity and shear stress in laminar-turbulent transition <strong>of</strong> unsteady incompressible boundary<br />
layer on aer<strong>of</strong>oil, whose center velocity changes in time as a degree function. It’s found that for<br />
both in confuser and in diffuser aer<strong>of</strong>oil regions the decelerating flow reduces the shear stress and<br />
favours the separation <strong>of</strong> flow, which occurring for lower contour values. The accelerating fluid<br />
flow postpones the boundary layer separation, i.e. laminar-turbulent transition, and vice versa
202 Section 9: Laminar flows and transition<br />
the separation is occurring for greater contour values <strong>of</strong> aer<strong>of</strong>oil. Boundary layer characteristics<br />
are found directly, no further numerical integration <strong>of</strong> momentum equation.<br />
Unsteady convective diffusion <strong>of</strong> a solute in a Hagen-Poiseuille flow through a tube<br />
with permeable wall<br />
Alexandru Dumitrache, Florin Frunzulica (POLITEHNICA University <strong>of</strong> Bucharest and Institute<br />
<strong>of</strong> Mathematical Statistics and Applied Mathematics) Schedule<br />
Effects <strong>of</strong> Interphase Mass Transfer (IMT) on the unsteady convective diffusion in a fluid flow<br />
through a tube surrounded by a porous medium is examined against the background <strong>of</strong> no IMT.<br />
The three coefficients namely exchange coefficient, convection coefficient, and dispersion coefficient<br />
are evaluated asymptotically at large-time using Gill Sankarasubramanian model [1]. The<br />
exchange coefficient exists due to IMT.<br />
The convective diffusion equation and the corresponding initial and boundary conditions are<br />
used for the beginning<br />
∂C<br />
∂t<br />
+ u(r)∂C<br />
∂x<br />
� 2 ∂ C 1<br />
= D +<br />
∂x2 r<br />
�<br />
∂<br />
r<br />
∂r<br />
∂C<br />
��<br />
∂r<br />
(1)<br />
C(0, x, r) = F (x, r) (2)<br />
C(t, ∞, r) = 0 = ∂C<br />
(t, ∞, r) (3)<br />
∂r<br />
−D ∂C<br />
∂r (t, x, r) = KsC at r = ±R. (4)<br />
where D is the molecular diffusivity and Ks is the rate <strong>of</strong> mass transfer <strong>of</strong> solute at the walls <strong>of</strong><br />
the cylinder. The condition (3) means that solute does not reach distances far down stream. The<br />
condition (4) implies that the flux <strong>of</strong> concentration at the walls is due to a first order chemical<br />
reaction.<br />
Then the dimesionless parameters will be used to transform equation.<br />
The convection and dispersion coefficient <strong>of</strong> solute are studied as a function <strong>of</strong> slip parameter,<br />
IMT parameter and porous parameter. All-time analysis is made analytically when there is no<br />
IMT. The mean concentration distribution is measured at a point inside and outside the slug.<br />
The peak <strong>of</strong> mean concentration is higher than that <strong>of</strong> pure convection and it is further enhanced<br />
with increase <strong>of</strong> porous parameter (or decrease <strong>of</strong> particle size).<br />
The results have applications in heat exchangers, petroleum and chemical engineering problems,<br />
chromatography and biomechanical problems.<br />
[1] R. Sankarasubramanian and W. N. Gill, Unsteady convective diffusion with interphase<br />
mass transfer, Proc. Roy. Soc. London A, 333 pp. 115–132, 1973.<br />
On the Optimum Efficiency <strong>of</strong> a Flapping Foil And Its Application to Valveless Pumps<br />
Markus Müllner (TU Wien) Schedule<br />
Several different working principles exist to drive a valveless pump. An efficient pump may be<br />
constructed by placing a flapping foil into a channel. For the case <strong>of</strong> inviscid flow, the pressure
Section 9: Laminar flows and transition 203<br />
difference along the channel is equivalent to the thrust force acting on the propulsor. The effect<br />
<strong>of</strong> the channel walls on the forces is briefly discussed. The focus in this talk is on the determination<br />
<strong>of</strong> movements <strong>of</strong> highest propulsive efficiency for a given thrust. In order to treat the<br />
optimization problem analytically, the case <strong>of</strong> a slender foil placed in a free stream, flapping in<br />
time-harmonic motion with small deflections, is investigated. Novel results for the heaving- and<br />
pitching amplitude and for the pivot point <strong>of</strong> the pitching motion are presented as a function<br />
<strong>of</strong> the reduced frequency σ. A surprising outcome is that for a certain range <strong>of</strong> the thrust force,<br />
the reduced frequency needs to be infinitely large to obtain maximum efficiency. Unfortunately,<br />
the optimum movements are accompanied by some drawbacks. An important issue is to reduce<br />
the lateral forces acting on the structure. Therefore, foil movements with zero lateral force are<br />
investigated and the deficit in efficiency is compared to the optimum foil motion. Furthermore,<br />
instead <strong>of</strong> the foil, an undulating wave motion is considered. The analytic result for different wave<br />
numbers k is presented and the efficiency is compared to the optimum solution <strong>of</strong> the foil.<br />
S9.2: Laminar flows and transition II Tue, 16:00–18:00<br />
Chair: Ulrich Rist, Suad Jakirlic S1|01–A2<br />
Global flow instabilities in plane sudden expansions<br />
Hendrik Christoph Kuhlmann , Daniel Lanzerstorfer (TU Wien) Schedule<br />
The three-dimensional linear stability <strong>of</strong> the two-dimensional, incompressible flow in a plane symmetric<br />
sudden expansion is considered. The geometry is varied systematically, covering expansion<br />
ratios (steps to outlet height) from 0.25 to 0.95. The stability analysis reveals that the primary<br />
symmetry-breaking bifurcation is two-dimensional. The asymmetric flow solution, however, becomes<br />
unstable to different secondary three-dimensional instabilities. The critical modes depend on<br />
the expansion ratio. An energy-transfer analysis is used to understand the nature <strong>of</strong> the instabilities.<br />
In the limit <strong>of</strong> vanishing step height, the critical mode is stationary and the amplification<br />
process is caused by a shear instability. For high expansion ratios, the basic jet-like flow and<br />
becomes unstable due to centrifugal forces leading to an oscillatory mode. For intermediate expansion<br />
ratios, an elliptic instability mechanism is identified and the instability characteristics<br />
change continuously with the expansion ratio. For an asymmetric geometry the disconnected<br />
primary solution branches are readily shifted to very high Reynolds numbers. The connected twodimensional<br />
solution branch is found to be very similar to the asymmetric flow <strong>of</strong> the symmetric<br />
channel thus showing the same type <strong>of</strong> secondary instability.<br />
Connecting the dots: Symmetry Analysis in Linear Stability Theory <strong>of</strong> a Linear Shear<br />
Flow<br />
Andreas Nold, Martin Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
A novel self-similar base solution for linear stability analysis <strong>of</strong> an unbounded linear shear flow<br />
employing symmetry methods is presented. Symmetry analysis is used to derive a full classification<br />
<strong>of</strong> symmetries <strong>of</strong> the linearized Navier-Stokes-Equations for two-dimensional perturbations<br />
<strong>of</strong> a linear shear flow. It is shown that the normal mode approach leading to the Orr-Sommerfeld<br />
equation and the Kelvin mode approach are both special classes <strong>of</strong> self-similar ansatz functions<br />
systematically derived in the framework <strong>of</strong> symmetry analysis. A third novel class <strong>of</strong> ansatz<br />
functions is presented. In the viscous case, known solutions <strong>of</strong> the initial value problem can be<br />
recovered by superposition <strong>of</strong> the novel self-similar modes. In the inviscid case, a new closed-form<br />
solution <strong>of</strong> traveling, energy-conserving modes localized in spanwise direction is presented.
204 Section 9: Laminar flows and transition<br />
An Exact Navier-Stokes Solution for Three-Dimensional, Spanwise-Homogeneous<br />
Boundary Layers<br />
M. O. John, D. Obrist, L. Kleiser (ETH Zürich) Schedule<br />
In some boundary layer flows the incompressible Navier-Stokes equations are amenable to exact<br />
similarity solutions. Two such cases are the plane stagnation flow onto a wall (Hiemenz boundary<br />
layer, HBL) and the asymptotic suction boundary layer flow (ASBL) over a flat wall. The Hiemenz<br />
solution has been extended to the swept Hiemenz configuration by superposition <strong>of</strong> a third,<br />
spanwise-homogeneous sweep velocity. This solution, however, becomes singular as the chordwise,<br />
tangential base flow component vanishes. Similarly, the ASBL does not contain any chordwise<br />
velocity.<br />
This work presents a generalized three-dimensional similarity solution, using a novel similarity<br />
coordinate. The HBL and ASBL are shown to be two limits <strong>of</strong> this solution which describes threedimensional<br />
spanwise-homogeneous impinging boundary layers at arbitrary wall-normal suction<br />
velocities.<br />
Further extensions may consist <strong>of</strong> oblique impingement, or different boundary suction directions,<br />
such as slip walls or stretching walls.<br />
Near critical laminar flow past an expansion ramp<br />
A. Kluwick, S. Braun, R. Szeywerth (TU Wien) Schedule<br />
Steady two-dimensional laminar flows past an expansion ramp are known to exist up to a critical<br />
ramp angle αc in the limit as the Reynolds number tends to infinity. The theory <strong>of</strong> viscousinviscid<br />
interaction combined with a local bifurcation analysis is used to study the evolution <strong>of</strong><br />
three-dimensional unsteady perturbations if |α − αc| ≪ 1 for both sub- and supercritical conditions.<br />
Special emphasis is placed on the effects <strong>of</strong> controlling devices and the phenomenon <strong>of</strong><br />
bubble bursting.<br />
Asymptotic description <strong>of</strong> incipient separation bubble bursting<br />
Stefan Braun, Stefan Scheichl, Alfred Kluwick (TU Wien) Schedule<br />
The appearance <strong>of</strong> short laminar separation bubbles in high Reynolds number wall bounded flows<br />
due to appropriate adverse pressure gradient conditions is usually associated with minor effects on<br />
global flow properties (e.g. lift force). However, localized reverse flow regions are known to react<br />
very sensitively to perturbations and in further consequence may trigger the laminar-turbulent<br />
transition process or even cause global separation. The present investigation <strong>of</strong> marginally separated<br />
boundary layer flows is based on a high Reynolds number asymptotic approach. Special<br />
emphasis is placed on solutions <strong>of</strong> the corresponding model equations which blow up within finite<br />
time indicating the ejection <strong>of</strong> a vortical structure and the emergence <strong>of</strong> shorter spatio-temporal<br />
scales reminiscent <strong>of</strong> the early transition scenario (‘bubble bursting’). Among others, an adjoint<br />
operator method is used to formulate the consequential evolution equations <strong>of</strong> the viscous-inviscid<br />
interaction process beyond blow up. Recent analytical and numerical findings regarding this new<br />
stage will be presented.<br />
Cauchy Problems and Breakdown in the Theory <strong>of</strong> Marginally Separated Flows<br />
Mario Aigner, Stefan Braun (TU Wien) Schedule<br />
Flow separation can be viewed as one <strong>of</strong> the trigger events <strong>of</strong> laminar-turbulent boundary layer<br />
transition. Thus, intensive investigations have been carried out as to when and how laminar boundary<br />
layers break down. In the special case <strong>of</strong> marginal separation, i.e. the formation <strong>of</strong> short<br />
laminar separation bubbles, high Reynolds number asymptotic theory yields integro-differential<br />
equations governing the essential flow behavior. Since transition, which can be associated with
Section 9: Laminar flows and transition 205<br />
”bubble bursting”, is an inherent time dependent phenomenon, initial value problems (IVPs) were<br />
formulated, using appropriate time scales within the according asymptotic setting. We will present<br />
further considerations <strong>of</strong> these problems in planar and three-dimensional flow cases regarding<br />
the general ill-posedness, using analytical and numerical techniques to depict the spatio-temporal<br />
manifestation <strong>of</strong> short-scale instabilities. To regularize such disturbances, higher order asymptotic<br />
terms comprising the streamline curvature in the boundary layer region are taken into account.<br />
Evidence for well-posedness <strong>of</strong> this modified problem will be given in terms <strong>of</strong> a dispersion relation<br />
and numerical solutions <strong>of</strong> the full problem, especially by performing backward in time<br />
calculations. Even though the regularized IVPs admit limiting steady states in their time evolution,<br />
the phenomenon <strong>of</strong> finite time blow-up, which can be interpreted as ”bubble bursting”, is<br />
still present. As a consequence, the inevitable breakdown <strong>of</strong> the according flow description leads<br />
to the emergence <strong>of</strong> a new asymptotic structure <strong>of</strong> shorter spatio-temporal scales (yielding a so<br />
called nonlinear triple deck stage). Deeper insight into this next stage <strong>of</strong> the bursting process is<br />
still to be gained and we will conclude by presenting some first attempts in solving this problem.<br />
S9.3: Laminar flows and transition III Wed, 13:30–15:30<br />
Chair: Andreas Krumbein, Suad Jakirlic S1|01–A2<br />
Transition Modelling for Aerodynamic Flow Simulations with a Near-Wall Reynolds-<br />
Stress Model<br />
Axel Probst (DLR Göttingen), Ulrich Rist (<strong>Universität</strong> Stuttgart), René-Daniel Cécora, Rolf Radespiel<br />
(TU Braunschweig) Schedule<br />
Transition from laminar to turbulent flow plays a significant role in modern aircraft designs. Numerical<br />
simulations <strong>of</strong> flows around flying aircrafts still mostly rely on RANS (Reynolds-averaged<br />
Navier-Stokes) approaches which use semi-empirical closures to model turbulent flow. The most<br />
general level <strong>of</strong> RANS closures is achieved by modelling the six individual transport equations<br />
<strong>of</strong> the Reynolds-stress tensor (Reynolds-stress model, RSM). To account for near-wall turbulence<br />
effects additional low-Reynolds number damping functions can be applied which locally alter the<br />
model calibration.<br />
Our present approach uses the ε h -based near-wall RSM [1] in an extended formulation which<br />
is combined with an e N -transition-prediction method within the finite-volume flow solver DLR-<br />
TAU. Due to its DNS-based calibration the model is able to accurately predict the anisotropic<br />
Reynolds-stress and dissipation-rate pr<strong>of</strong>iles down to the wall. However, the damping terms were<br />
found to delay or even suppress transition in the low-disturbance environments <strong>of</strong> flying aircrafts.<br />
The simulation method is therefore extended by a novel approach to incorporate the usually neglected<br />
Reynolds-stress contributions by the unstable transitional modes into the RANS solution<br />
[2]. To derive realistic input quantities at turbulence onset a linear-stability eigenfunction analysis<br />
<strong>of</strong> the incoming laminar boundary layer is performed. It provides the wall-normal shapes <strong>of</strong> the<br />
transitional Reynolds stresses which are derived from the amplitudes and phase shifts <strong>of</strong> the most<br />
amplified Tollmien-Schlichting or crossflow wave at the end <strong>of</strong> linear amplification. Closure <strong>of</strong><br />
the yet missing magnitudes is obtained by an additional calibration based on DNS results <strong>of</strong> an<br />
adverse-pressure-gradient flow.<br />
The talk provides a detailed overview on both the near-wall Reynolds-stress closure and the<br />
linear-stability-based transition model. To demonstrate the validity <strong>of</strong> the approach, computations<br />
<strong>of</strong> different 2D and 3D flow cases are presented, such as generic boundary layers, airfoil<br />
flows and a flow-through nacelle near stall. Moreover, a recent extension for combined Tollmien-<br />
Schlichting/crossflow transition scenarios is addressed.
206 Section 9: Laminar flows and transition<br />
[1] Jakirlić, S., Hanjalić, K., A new approach to modelling near-wall turbulence energy and stress<br />
dissipation, J. Fluid Mechanics, 459 (2002), 139 – 166.<br />
[2] Probst, A., Radespiel, R., Rist, U., Linear-Stability-Based Transition Modeling for Aerodynamic<br />
Flow Simulations with a Near-Wall Reynolds-Stress Model, to appear in: AIAA Journal<br />
(<strong>2012</strong>).<br />
An investigation <strong>of</strong> the separate flow and stall delay for horizontal-axis wind tubine<br />
Florin Frunzulica (POLITEHNICA University <strong>of</strong> Bucharest), Razvan Mahu (TENSOR SRL,<br />
Bucharest), Horia Dumitrescu (Institute <strong>of</strong> Mathematical Statistics and Applied Mathematics<br />
Bucharest) Schedule<br />
The flow characteristics and stall delay phenomenon <strong>of</strong> a stall regulated wind turbine rotor due to<br />
blade rotation in steady state non-yawed conditions are investigated. An incompressible Reynoldsaveraged<br />
Navier-Stokes solver is applied to carry out the separate flow cases at high wind speeds<br />
from 11 m/s to 25 m/s with an interval <strong>of</strong> 2 m/s. The objective <strong>of</strong> the present research effort is<br />
to validate a first-principles based approach for modeling horizontal-axis wind turbines (HAWT)<br />
under stalled flow conditions using NREL/ Phase VI rotor data. The computational results are<br />
compared with the predicted values derived by a new stall-delay model and blade element momentum<br />
(BEM) method.<br />
An insight into the rotational stall delay<br />
Horia Dumitrescu, Vladimir Cardos (Institute <strong>of</strong> Statistical Mathematics and Applied Mathematics<br />
Bucharest) Schedule<br />
Blade element and momentum methods (BEM) are the traditional design approach to calculate<br />
drag and lift forces <strong>of</strong> wind turbine rotor blades. The major disadvantage <strong>of</strong> these theories is<br />
that the airflow is reduced to axial and circumferential flow components. Disregarding radial flow<br />
components leads to underestimation <strong>of</strong> lift and thrus. Therefore, correction models for rotational<br />
effects are <strong>of</strong>ten used in the case <strong>of</strong> the stall controlled rotors at a constant rotation speed. At<br />
inboard locations, there is a strong interaction between the fast rotating flow <strong>of</strong> wake and the 3-D<br />
boundary layer close to the blade surface rotating with an angular velocity smaller than that <strong>of</strong><br />
the fluid. This behaviour is visible from the streamlines over the blade surface during operation in<br />
deep stall. The knowledge extracted from the physical mechanism <strong>of</strong> 3-D rotational effects can be<br />
then used to develop an improved BEM model for the design <strong>of</strong> stall control-wind turbine rotor<br />
blades. In this study the pressure fields generated by the wake and blade are superimposed and<br />
the main contributions for the rise <strong>of</strong> the three-dimensional and rotational effects are described.<br />
Analytical and Numerical Modelling <strong>of</strong> the Safe Turn Manoeuvres <strong>of</strong> Agricultural<br />
Aircraft<br />
Bosko Rasuo (University <strong>of</strong> Belgrade) Schedule<br />
In this paper, a theoretical study <strong>of</strong> the turn manoeuvre <strong>of</strong> an agricultural aircraft is presented.<br />
The manoeuvre with changeable altitude is analyzed, together with the, effect <strong>of</strong> the load factors<br />
on the turn manoeuvre characteristics during the field-treating flights. The mathematical model<br />
used describes the procedure for the correct climb and descent turn manoeuvre. For a typical<br />
agricultural aircraft, the numerical results and limitations <strong>of</strong> the climb, horizontal and descending<br />
turn manoeuvre are given. The problem <strong>of</strong> turning flight with changeable altitude is described<br />
by the system <strong>of</strong> differential equations which describe the influence <strong>of</strong> the normal and tangential<br />
load factors on velocity, the path angle in the vertical plane and the rate <strong>of</strong> turn, as a function <strong>of</strong><br />
the bank angle during turning flight. The system <strong>of</strong> differential equations <strong>of</strong> motion was solved
Section 9: Laminar flows and transition 207<br />
on a personal computer with the Runge-Kutta-Merson numerical method. Some analytical and<br />
numerical results <strong>of</strong> this calculation are presented in this paper.<br />
Ariel treating has become an integral part <strong>of</strong> modern agriculture. However, agricultural flying<br />
has been plagued by a great number <strong>of</strong> accidents. The manoeuvres <strong>of</strong> an agricultural aircraft<br />
are divided into those carried out while entering or leaving the spraying line. Despite low height<br />
<strong>of</strong> the aeroplane while spraying, this part <strong>of</strong> the flight is considered to be the safest because<br />
<strong>of</strong> an appreciable flight velocity. Upon completing a spraying run, the aircraft enters the turn<br />
manoeuvre procedure.<br />
The low altitude <strong>of</strong> the turn manoeuvre procedure and the vicinity <strong>of</strong> terrain are main causes<br />
<strong>of</strong> numerous accidents. The pilots assert that the procedure is the most dangerous manoeuvre<br />
and most <strong>of</strong> the accidents occur when these manoeuvres are performed, due to low altitude and<br />
the possibility <strong>of</strong> stall during the manoeuvres. There are many secondary factors that influence<br />
the safety <strong>of</strong> agricultural flying and some <strong>of</strong> them will be treated in this paper.<br />
In this paper a criterion has been established for determining the margin <strong>of</strong> the speed over the<br />
stalling speed (safety speed) after the agricultural aeroplane increases its height above the ground<br />
by a given amount. The required altitude may be different for different types <strong>of</strong> aeroplanes and<br />
will depend on their capability to perform rolling and turning manoeuvres. The minimum margin<br />
<strong>of</strong> velocity allowed is determined from the requirements <strong>of</strong> the rolling manoeuvre.<br />
A numerical study <strong>of</strong> vortex structures behind an harbor seal vibrissa<br />
Daniel Matz, Albert Baars (Bionik Innovations Centrum) Schedule<br />
Harbor seals (Phoca vitulina) use whiskers (vibrissa) to detect prey by their trailing wake. These<br />
whiskers are not circular cylinders, but show wavy elliptical structures in spanwise direction.<br />
This geometry is found to substantially reduce vortex shedding in the wake <strong>of</strong> the vibrissa in<br />
comparison to circular cylinders and elliptical structures. In this work we want to contribute to<br />
the question, to what extent wave length and amplitude <strong>of</strong> the shape are optimized for reduction<br />
<strong>of</strong> self induced oscillations. Therefore, numerical flow simulations at Re = 230 are performed to<br />
investigate the influence <strong>of</strong> amplitude and wavelength on vortex structures, drag and lift coefficient,<br />
as well as the Strouhal number. The 3D calculations are carried out with a finite volume<br />
code with discretization <strong>of</strong> second order in space and time. The block structured grids consists <strong>of</strong><br />
around 1 · 10 7 volumes. For the basic geometry the amplitude <strong>of</strong> the lift coefficient range lower by<br />
a factor <strong>of</strong> 120 in comparison to a cylinder and a factor <strong>of</strong> 30 in comparison to an ellipse. This is in<br />
accordance with literature. The separated shear layer in the wake <strong>of</strong> the vibrissa forms complex<br />
3D flow pattern, which show a periodical structure in spanwise direction. For overflow length<br />
greater than 800 this structure gets unstable and deforms in spanwise direction. This influences<br />
the temporal progression <strong>of</strong> drag and lift coefficient.<br />
S9.4: Laminar flows and transition IV Wed, 16:00–18:00<br />
Chair: Martin Oberlack / Florian Kummer, Stefan Braun S1|01–A2<br />
A discontinuous Galerkin solver for steady incompressible flows based on the SIM-<br />
PLE algorithm<br />
Benedikt Klein, Florian Kummer (TU <strong>Darmstadt</strong>) Schedule<br />
For the numerical simulation <strong>of</strong> incompressible flows the finite volume method (FVM) and the<br />
continuous finite element method (FEM) are widely used. Besides, a newer method, the discontinuous<br />
Galerkin method (DGM), which has got favorable properties <strong>of</strong> both the FVM and the<br />
FEM, is becoming more popular. The DGM provides a convergence order <strong>of</strong> O(∆x k+1 ), where k<br />
is the order <strong>of</strong> the approximating polynomials.
208 Section 9: Laminar flows and transition<br />
When simulating incompressible flows one has to deal with certain difficulties, like the nonlinearity<br />
in the momentum equation, a strong coupling between velocity and pressure and the lack<br />
<strong>of</strong> an explicit equation for the pressure. The well-known SIMPLE algorithm, which was originally<br />
proposed by Patankar and Spalding [1], has shown to be very efficient in the context <strong>of</strong> the FVM<br />
and the FEM [2]. For the SIMPLE algorithm, by introducing an iterative process the discrete<br />
equations are linearized and decoupled. An equation for the pressure, more precisely speaking,<br />
for the pressure correction is derived on the discrete level.<br />
Using a discontinuous Galerkin discretization <strong>of</strong> the momentum and continuity equation [3],<br />
we present how the SIMPLE algorithm can be adapted to the DGM. Various test cases are carried<br />
out, which show the expected convergence rate <strong>of</strong> k + 1.<br />
[1] S.V. Patankar and D.B Spalding, A calculation procedure for heat, mass and momentum<br />
transfer in three-dimensional parabolic flows, Int. J. Heat Mass Transfer 15 (1972), 1787 –<br />
1806.<br />
[2] V. Haroutunian, M.S. Engelman and I. Hasbani, Segregated finite element algorithms for the<br />
numerical solution <strong>of</strong> large-scale incompressible flow problems, Int. J. Numer. Meth. Fl. 17<br />
(1993), 323 – 348.<br />
[3] K. Shahbazi, P.F. Fischer and C.R. Ethier, A high-order discontinuous Galerkin method for<br />
the unsteady incompressible Navier-Stokes equations, J. Comput. Phys. 222 (2007), 391 –<br />
407.<br />
Energy conserving incompressible flows on collocated and distorted grids<br />
Julius Reiss (TU Berlin) Schedule<br />
An energy preserving finite difference scheme for incompressible, constant density flows is presented.<br />
It is based on the idea <strong>of</strong> the skew-symmetric formulation <strong>of</strong> the non–linear transport term<br />
<strong>of</strong> the Navier–Stokes Equation<br />
∂tuα + 1<br />
2 (div (uuα) + u · grad (uα)) + (gradp)α = 0<br />
div(u) = 0<br />
with u = (u1, u2, u3), and α = 1, 2, 3. In contrast to established schemes collocated Euclidean grids<br />
can be used while exactly preserving the energy and momentum conservation, yet avoiding the<br />
odd–even decoupling <strong>of</strong> the Laplacian <strong>of</strong> the pressure Poisson equation. The essential idea is to use<br />
different discretizations for the different derivatives in the above equations. High order derivatives<br />
in space and time can be used. The generalization to transformed grids is discussed and full<br />
conservation for arbitrary transformations in two dimensions and for restricted transformations<br />
in three dimensions is found.<br />
On a reduced mixed s-v least-squares finite element formulation for the incompressible<br />
Navier-Stokes equations<br />
Alexander Schwarz, Jörg Schröder (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
In the present work a mixed finite element based on a least-squares approach is proposed. Here,<br />
we consider a formulation for Newtonian fluid flow, which is described by the incompressible<br />
Navier-Stokes equations. First, a div-grad first-order system is derived resulting in a three-field<br />
approach with stresses, velocities, and pressure as unknowns. Following the idea in [1], this threefield<br />
formulation can be transformed into a reduced stress-velocity (s-v) two-field approach. The
Section 9: Laminar flows and transition 209<br />
L2-norms <strong>of</strong> the residuals <strong>of</strong> the derived equations yield then the least-squares functional, which is<br />
the basis for the associated minimization problem. Besides some numerical advantages, as e.g. an<br />
inherent symmetric structure <strong>of</strong> the system <strong>of</strong> equations and an error estimator, it is known that<br />
least-squares methods have also a drawback concerning accuracy, especially when lower-order<br />
elements are used, see e.g. [2,3]. Therefore, the main focus <strong>of</strong> the presentation is on performance<br />
and implementation aspects <strong>of</strong> triangular mixed finite elements with different interpolation order.<br />
In order to approximate the stresses, shape functions related to the edges are chosen. These<br />
vector-valued functions are used for the interpolation <strong>of</strong> the rows <strong>of</strong> the stress tensor and belong<br />
to a Raviart-Thomas space, which guarantees a conforming discretization <strong>of</strong> the Sobolev space<br />
H(div). Furthermore, standard polynomials associated to the vertices <strong>of</strong> the triangle are used for<br />
the continuous approximation <strong>of</strong> the velocities. The talk closes with some numerical examples,<br />
which focus on well-known benchmark problems for incompressible Newtonian fluid flow and<br />
demonstrate the performance <strong>of</strong> the mixed finite element formulation.<br />
[1] Z. Cai, B. Lee, P. Wang, Least-squares methods for incompressible Newtonian fluid flow:<br />
linear stationary problems, SIAM J. Numer. Anal. 42 (2004), 843–859.<br />
[2] O. Kayser-Herold, Least-squares methods for the solution <strong>of</strong> fluid-structure interaction problems,<br />
PhD Thesis, <strong>Technische</strong> <strong>Universität</strong> Braunschweig (2006).<br />
[3] A. Schwarz, J. Schröder, A mixed least-squares formulation <strong>of</strong> the Navier-Stokes equations<br />
for incompressible Newtonian fluid flow, Proc. Appl. Math. Mech. 11 (2011), submitted.<br />
Allocation <strong>of</strong> the particle concentration for the SPH-method depending on the gradients<br />
<strong>of</strong> flow parameters<br />
Anika Stein, Olaf Wünsch (<strong>Universität</strong> Kassel), Markus Rütten (DLR Göttingen), Jens Kuenemund,<br />
Stefan Saalfeld (<strong>Universität</strong> Göttingen) Schedule<br />
The Smoothed Particle Hydrodynamics method (SPH) is a Lagrangian, mesh free method to<br />
discretize partial differential equations like the Navier-Stokes-Equation by interpolating flow properties<br />
directly at a set <strong>of</strong> particles. It was first developed 1977 by [1] and [2] for astrophysical<br />
Problems. Today it is applied more and more for mechanical problems. It is comfortable to use<br />
for fluid and multiphase flow problems, large deformation problems and free surface flows because<br />
it is possible to allocate different properties to each particle. Moreover the differential set <strong>of</strong> the<br />
Momentum-Equation is particularly suitable for complex rheological problems like polymer melts,<br />
[3]. All the information about the flow like velocity, temperature, viscosity and so on are recorded<br />
at each particle for a optional number <strong>of</strong> departed time steps. It brings a lot <strong>of</strong> advantages as<br />
described above, but another outcome <strong>of</strong> that are costs in memory and a rising need <strong>of</strong> calculation<br />
power, the more particles are inside a domain. Taking in account that in some areas <strong>of</strong> a flow field<br />
nearly nothing happens and in some areas the gradients <strong>of</strong> flow parameters are very high, it is<br />
not the best choice to use the same particle concentration at those different regions. In this paper<br />
a method is presented to optimise this number <strong>of</strong> particles according to the gradients <strong>of</strong> the flow<br />
parameters. The functional principle <strong>of</strong> this operation is to generate particles at domains with<br />
highly alternate flow properties and to turn them out where they are not needed. This algorithm<br />
is able to generate more accurate solutions, which is shown by different examples like a leaked<br />
tank or a breaking dam. Finally the influence <strong>of</strong> the procedure is discussed.<br />
[1] R. A. Ginglod and J. J. Monaghan, Smoothed particle hydrodynamics theory and application<br />
to non-spherical stars, Mon. Not. R. Astron. Soc. 181, 375 (1977)
210 Section 9: Laminar flows and transition<br />
[2] L. B. Lucy, A numerical approach to the testing <strong>of</strong> the fission hypothesis, Astron. J. 83, 1013<br />
(1977)<br />
[3] M. Ellero, Smoothed Particle Dynamics Methods for the Simulation <strong>of</strong> Viscoelastic Fluids,<br />
Dissertation, <strong>Universität</strong> Berlin,(2004), urn:nbn:de:kobv:83-opus-7658<br />
Internal flow analysis for slow moving small droplets in contact with rough surfaces<br />
Raheel Rasool, Roger A. Sauer, Muhammad Osman (RWTH Aachen) Schedule<br />
Motivated by the self-cleaning phenomena, internal fluid flow behavior for slow moving small<br />
droplets in contact with rough surfaces is analyzed. The shape <strong>of</strong> the droplet is first computed<br />
using the Young-Laplace equation. For this purpose a Finite Element (FE) model [1], in which<br />
contact constraints are enforced through Penalty and Augmented Lagrange Multiplier methods,<br />
is used. The flow field within the droplet is then analyzed through the Stokes flow model, constituting<br />
a decoupled approach. Similar to the membrane deformation model, the formulation for<br />
the flow analysis is also expressed in the framework <strong>of</strong> FE analysis. Both, stabilized (Pressure<br />
Stabilizing/Petrov-Galerkin PSPG) and Galerkin FE formulations are considered. The motion<br />
<strong>of</strong> the fluid inside the droplet is governed by the slip condition enforced on the membrane <strong>of</strong><br />
the droplet. Numerical examples for droplets rolling steadily on smooth and rough surfaces are<br />
presented.<br />
[1] M. Osman and R.A. Sauer, A two-dimensional computational droplet contact model, Proc.<br />
Appl. Math. Mech., 11 (2011), 103-104.<br />
Pattern formation and mixing in three-dimensional film flow<br />
Thilo Pollak, Christian Heining, Nuri Aksel (<strong>Universität</strong> Bayreuth) Schedule<br />
The effect <strong>of</strong> inertia on gravity-driven free surface flow over different three-dimensional periodic<br />
corrugations is considered analytically, numerically and experimentally. In the case <strong>of</strong> high bottom<br />
undulations the results predict complex free surface structures especially in cases where the<br />
topography is not fully flooded by the liquid film. The investigation <strong>of</strong> the flow field shows a rich<br />
variety <strong>of</strong> pattern formation phenomena depending on the interplay between the geometry <strong>of</strong> the<br />
topography and the inertia <strong>of</strong> the film. Finally, we show how the complex topographical structure<br />
enhances the laminar mixing within the film.<br />
S9.5: Laminar flows and transition V Thu, 13:30–15:30<br />
Chair: Ulrich Rist S1|01–A2<br />
Modelling study <strong>of</strong> turbulent-to-laminar transitional features <strong>of</strong> a strongly heated<br />
pipe flow<br />
S. Jakirlic (TU <strong>Darmstadt</strong>), R. Jester-Zuerker (Voith Hydro Holding GmbH Co. KG-tts, Heidenheim)<br />
Schedule<br />
A flow in a circular pipe subjected to increasingly enhanced wall heating is computationally investigated<br />
by means <strong>of</strong> a differential, near-wall second-moment closure model based on the solution<br />
<strong>of</strong> transport equations for second moments <strong>of</strong> the fluctuating velocities and temperature, � u ′′<br />
i u′′<br />
j and<br />
�u ′′<br />
i<br />
θ respectively. Both Reynolds stress model and heat flux model represent wall-topography free<br />
formulations with quadratic pressure-strain term and pressure-temperature-gradient correlation.
Section 9: Laminar flows and transition 211<br />
The transport equations for the turbulent stress tensor and the turbulent heat flux are solved in<br />
conjunction with the equation governing a novel length-scale determining variable, the so-called<br />
homogeneous dissipation rate, Jakirlic and Hanjalic (2002, J. Fluid Mech., 539:139-166). Such an<br />
approach <strong>of</strong>fers a number <strong>of</strong> important advantages: proper near-wall shape <strong>of</strong> the dissipation rate<br />
pr<strong>of</strong>ile was obtained without introducing any additional term and the correct asymptotic behaviour<br />
<strong>of</strong> the stress dissipation components by approaching the solid wall is fulfilled automatically<br />
without necessity for any wall geometry-related parameter. In order to account for the influence<br />
<strong>of</strong> the temperature field and associated fluid property variation on the velocity field, the Favreaveraged<br />
equations for mass, momentum and energy are solved. The temperature dependence on<br />
viscosity and heat conductivity is defined via a power-law formulations, while Prandtl number<br />
P r and specific heat at constant pressure Cp were kept constant. Density is evaluated from the<br />
equation for ideal gas.<br />
The flow configuration considered presently, representing a vertical circular tube with air flowing<br />
in upward direction, was experimentally investigated by Shehata and McEligot (1998, Int. J.<br />
Heat and Mass Transfer, 41:4297-4313) and by means <strong>of</strong> DNS by Satake et al. (2000, Int. J. Heat<br />
and Fluid Flow, 21:526-534) and Bae et al. (2006, Physics <strong>of</strong> Fluids, 18(075102)). After a portion<br />
<strong>of</strong> a fully-developed pipe flow (length = 4D, with D being the pipe diameter) with constant wall<br />
temperature Θw the air enters a 30D-long pipe subjected to intensive heating (with negligible<br />
buoyancy effects). The thermal boundary conditions correspond to a constant heat flux. Three<br />
different heating rates were considered q +<br />
i = 0.0018, 0.0035 and 0.0045. According to the reference<br />
data originators, these values relate to the turbulent, sub-turbulent and laminarizing regimes. In<br />
the latter case some laminarization phenomena have been observed. The influence <strong>of</strong> strong heating<br />
<strong>of</strong> a gas flow (as, e.g., encountered in gas combustors and similar high-temperature reactors) is<br />
primarily manifested through a severe variation <strong>of</strong> the fluid properties (density, viscosity) leading<br />
consequently to important structural changes. The most important changes are concentrated in<br />
the immediate wall vicinity. The strongest modification <strong>of</strong> flow structure, deviating substantially<br />
from the equilibrium conditions, occurs in the inner part <strong>of</strong> the temperature layer. Accordingly,<br />
the density decrease and viscosity increase led to the thermal boundary layer growth and<br />
viscous sublayer thickening (relative to the boundary layer thickness reduction) causing the flow<br />
acceleration, which, if sufficiently strong, can suppress turbulence resulting in flow laminarization.<br />
The model results obtained follow closely the experimental and DNS findings manifested especially<br />
through the laminar-like pr<strong>of</strong>iles <strong>of</strong> the velocity and temperature fields. The behaviour <strong>of</strong><br />
Reynolds stress components is in accordance with a severe suppression <strong>of</strong> the turbulence intensity<br />
due to local acceleration caused by a strong viscosity increase.<br />
Numerical and experimental investigations <strong>of</strong> thermal convection in an inclined narrow<br />
gap<br />
O. Sommer (TU Chemnitz), H. G. Heiland (SUVIS GmbH, Chemnitz), G. Wozniak (TU Chemnitz)<br />
Schedule<br />
The knowledge <strong>of</strong> the fluid behaviour in inclined cavities is <strong>of</strong> fundamental importance as far as<br />
heat and mass transfer are concerned. The interest in this subject is particulary increasing due<br />
to the rapid process in microtechnologies. We therefore studied the flow- and temperature field <strong>of</strong><br />
such flows numerically as well as experimentally using CFD and PIV/ T, respectively. We present<br />
and discuss the numerical and experimental results <strong>of</strong> our investigations and explain the applied<br />
techniques.<br />
Gas exchange <strong>of</strong> almost leak-tight display cases<br />
Johannes Strecha, Herbert Steinrück (TU Wien) Schedule
212 Section 9: Laminar flows and transition<br />
A requirement for display cases for art objects is to be leak tight. However, due to design constraints<br />
there a are tiny gaps resulting in a gas exchange between the interior <strong>of</strong> the show case and<br />
its environment. Usually the leak-tightness is being quantified by the so-called air exchange rate,<br />
the ratio <strong>of</strong> the gas volume exchanged between display-case and environment per unit time and<br />
the volume <strong>of</strong> the display-case. Commonly the concentration <strong>of</strong> a tracer-gas in the display-case is<br />
monitored to calculate the air exchange rate. For this purpose a certain tracer-gas exchange-law is<br />
assumed, usually a linear exchange-law. We present experimental results that disqualify a linear<br />
exchange law and find that it is a special case, not applicable in general.<br />
We review the gas exchange mechanism through the gaps Taking hydro static pressure differences<br />
due to temperature and concentration differences <strong>of</strong> the tracer gas and diffusion into<br />
account a non linear exchange model is derived and validated experimentally.<br />
We conclude that in general the tracer-gas concentration has a significant influence on the gas<br />
exchange and therefore the assumption <strong>of</strong> a linear exchange-law is discouraged. Instead we suggest<br />
the introduction <strong>of</strong> two parameters: one that characterizes the air-exchange in the diffusion-driven<br />
limit and one that takes the influence <strong>of</strong> hydrostatic pressure into account. Strategies to identify<br />
these parameters will be presented and demonstrated.<br />
Non isothermal simulation <strong>of</strong> non-Newtonian flow in the shot sleeve <strong>of</strong> semi- solid<br />
die casting processes<br />
Roudouane Laouar, Olaf Wünsch (<strong>Universität</strong> Kassel) Schedule<br />
This work deals with a numerical study <strong>of</strong> the flow <strong>of</strong> metal in the semi-solid state in the shot sleeve<br />
<strong>of</strong> horizontal die casting machine during the injection process. With the discovery <strong>of</strong> shear thinning<br />
and the thixotropic behavior <strong>of</strong> partially solidified alloys under vigorous agitation, a new era in<br />
forming technology was started, namely semi-solid metal (SSM) processing. The new technology<br />
promises several important advantages in comparison with the traditional die casting processes.<br />
In the semi-solid state, metallic alloys consists <strong>of</strong> solid particles suspended in a liquid Newtonian<br />
matrix and consequently modeling approaches known from classical suspension rheology can be<br />
applied. In the equilibrium state, semi-solid alloys are shear-thinning and different descriptions in<br />
form <strong>of</strong> material equation are used in literature. In the present work, the Herschel-Bulkley model,<br />
which contains a yield stress and a shear-thinning viscosity, was used in order to demonstrate<br />
the effect <strong>of</strong> the nonlinear viscosity to the flow pattern in the shot sleeve. The used numerical<br />
model, which considers the problem as two-dimensional, is based on the conservation equations<br />
<strong>of</strong> mass and momentum, and describes the free surface using the volume-<strong>of</strong>-fluid method. The<br />
motion <strong>of</strong> plunger is simulated by using a layering dynamic mesh method. The numerical results<br />
are obtained by using a CFD code that is based in the finite volume method. The influence <strong>of</strong><br />
different parameters as yield stress, the power law index and the temperature in the flow dynamics<br />
is to be discussed. A comparison between a Herschel-Bulkley fluid and a shear-thinning fluid with<br />
no yield stress limit is presented.<br />
Simulating <strong>of</strong> a pressing process <strong>of</strong> a viscoelastic polymer melt<br />
Ammar Al-Baldawi, Olaf Wünsch (<strong>Universität</strong> Kassel) Schedule<br />
A well known and <strong>of</strong>ten used method to obtain anisotropic polymer films is the so-called pressing<br />
process. Here, films are squeezed under high temperatures, pressure and deformation rates. To<br />
simulate such a process, the polymeric matrix is treated as a non-Newtonian, viscoelastic melt.<br />
Experimental investigations <strong>of</strong> it predict a shear thinning and elongational hardening/s<strong>of</strong>tening<br />
behavior. The modeling <strong>of</strong> this behavior is done with a generalized Maxwell Model. Where the<br />
generalization is obtained using a Phan-Thien and Tanner anisotropic molecule movement tensor<br />
for high deformation rates [1,2].
Section 9: Laminar flows and transition 213<br />
Simulating this process leads to a hyperbolic equation set <strong>of</strong> mass conservation, momentum<br />
balance and material model. Therefore, the simulation needs to be stabilized; here the DEVSS<br />
method is used. Furthermore, the ALE method is used to interpolate between the Euler and<br />
Lagrange description method in connection with a cell-layering method to obtain big changes in<br />
the calculation domain.<br />
In this work we present some simulations to show the difference between the classical approaches<br />
using a generalized Newtonian viscosity to model the polymeric matrix and the viscoelastic<br />
model. Here, the major difference is shown to be the pressure field and its influence on the velocity<br />
field and the extra stress tensor. For this end we use a flow type parameter to show the elongation<br />
types in the regions and the differences [1].<br />
[1] A. Al-Baldawi, O. Wünsch, Some new aspects <strong>of</strong> the invariants <strong>of</strong> the rate <strong>of</strong> deformation<br />
tensor and their application on viscoelastic polymer melts, Accepted for publication in<br />
<strong>Technische</strong> Mechanik (2011)<br />
[2] O. Wünsch, Laminar Fluid Flow with Complex Material Behavior in Devices <strong>of</strong> Mechanical<br />
Engineering, Int. Journal <strong>of</strong> Emerging Multidisciplinary Fluid Sciences, 1-4, 255-267 (2009)<br />
S9.6: Laminar flows and transition VI Thu, 16:00–18:00<br />
Chair: Suad Jakirlic S1|01–A2<br />
Direct numerical simulation <strong>of</strong> MHD duct flow at high Reynolds number<br />
Dmitry Krasnov (TU Ilmenau), Oleg Zikanov (University <strong>of</strong> Michigan), Thomas Boeck (TU Ilmenau)<br />
Schedule<br />
Evolution <strong>of</strong> turbulent flow <strong>of</strong> an incompressible, electrically conducting fluid is studied numerically<br />
in a square duct subjected to a uniform magnetic field B. The magnetic field is applied in<br />
the vertical (wall-normal) direction, the walls are perfectly insulating. The governing equations<br />
are the Navier-Stokes system with the additional Lorentz force term j × B, where j is the electric<br />
current. There are two governing parameters, the Reynolds number Re = UqL/ν and the Hartmann<br />
number Ha = BL � σ/ρν, which characterizes the strength <strong>of</strong> the applied magnetic field B.<br />
Here Uq are the mean flux velocity, L is the duct half-width and σ is the electrical conductivity.<br />
The Joule dissipation selectively damps out fluctuations <strong>of</strong> velocity perpendicular to the magnetic<br />
field that can result into anisotropy <strong>of</strong> turbulent eddies. For strong magnetic fields the<br />
anisotropy can evolve into 2D structures stretched along the direction <strong>of</strong> the magnetic field. Two<br />
major ingredients are necessary to achieve the 2D states: (i) the Reynolds number Re should<br />
be large, that amounts to intensive turbulent fluctuations and (ii) the interaction parameter<br />
N = Ha 2 /Re should exceed 1, which also means strong magnetic fields.<br />
In our simulations Re = 100000 and Ha = 0 ... 400. For the present study a series <strong>of</strong> DNS was<br />
performed at the grid resolution <strong>of</strong> 2048 × 769 × 769 points that amounts to more than 1 billion<br />
points as a problem size. The numerical method is based on highly conservative finite-difference<br />
discretization <strong>of</strong> the second order, the flow solver is hybrid-parallel (both MPI and Open MP<br />
interfaces).<br />
As Ha increases the flow transforms from nearly isotropic turbulence at Ha = 0 to a spatial<br />
anisotropy at Ha > 200. At Ha = 300 the core flow becomes essentially laminar, the turbulence<br />
remains small-scale near the side walls, but becomes large-scale, weak, and strongly anisotropic<br />
towards the core flow. Finally, at Ha = 400 the fluctuations die out and the flow becomes laminar.<br />
The quasi-2D structures have been identified in a clear-cut way by applying the so-called
214 Section 9: Laminar flows and transition<br />
lambda-2 criterion. The results <strong>of</strong> the lambda-2 visualization at Ha = 300 and 350 show a region<br />
with clearly expressed 2D structures stretched along the magnetic field. We have also found<br />
transformation <strong>of</strong> the mean velocity similar to our previous study on channel flow under spanwise<br />
magnetic field. This behavior is observed in the cross-section perpendicular to the magnetic field<br />
for a range Ha ≈ 100 ... 200. During this transformation the classical log-layer almost disappears<br />
and is replaced by a linear dependence.<br />
Visualisation <strong>of</strong> the Ludford column<br />
André Thess (TU Ilmenau), Oleg Andreev (Forschungszentrum Dresden-Rossendorf) Schedule<br />
The formation <strong>of</strong> TTaylor columnsïn rotating flows is well known: When a liquid flows over a<br />
truncated cylinder in a rotating systems, a stagnant region forms above the cylinder. It has been<br />
known for quite some time that an analogous phenomenon, the LLudford columnëxists when a<br />
liquid metal flows across a truncated cylinder under the influence <strong>of</strong> a magnetic field parallel<br />
to the axis <strong>of</strong> the cylinder. Since liquid metals are opaque, it is impossible to visualise Ludford<br />
columns. Using an electrolyte instead <strong>of</strong> a liquid metal and a high magnetic field created by<br />
a superconducting magnet we visualise for the first time the Ludford column and discuss their<br />
properties. We discuss further ways in which optical flow measurement can be applied to better<br />
understand magnetohydrodynamic flows.<br />
Separation <strong>of</strong> magnetic particles in channel flows by BEM<br />
J. Ravnik, M. Hriberek (University <strong>of</strong> Maribor), F.Vogel, P. Steinmann (<strong>Universität</strong> Erlangen-<br />
Nürnberg) Schedule<br />
In-line separation <strong>of</strong> suspensions can become difficult in in case <strong>of</strong> particles with comparable values<br />
<strong>of</strong> densities. For flows in micro devices in such cases gravitational settling is inefficient, and other<br />
separation techniques must be applied. In case <strong>of</strong> magneto active particles, the action <strong>of</strong> Kelvin<br />
magnetic force in a non-uniform magnetic field could be used in order to achieve a higher degree <strong>of</strong><br />
particles separation. The contribution therefoe deals with Euler-Lagrangian formulation <strong>of</strong> dilute<br />
two-phase flows. The Boundary element based computational algorithm solves the incompressible<br />
Navier-Stokes equations written in velocity-vorticity formulation. The nonuniform magnetic field<br />
was defined analytically for the case <strong>of</strong> a set <strong>of</strong> long thin wires. The particle trajectories were<br />
computed by applying the 4th order Runge-Kutta method. The computed test case consisted <strong>of</strong><br />
a narrow channel with laminar flow <strong>of</strong> suspension under Re=1-10. Particle trajectories under the<br />
influence <strong>of</strong> a nonuniform magnetic field were computed for the case <strong>of</strong> magnetite and aluminium<br />
particles suspended in water. The efficiency <strong>of</strong> separation on basis <strong>of</strong> particle trajectories for different<br />
values <strong>of</strong> Re number and magnetic field strength was performed, clearly indicating superior<br />
separation <strong>of</strong> magneto active particles.<br />
Experimental investigation <strong>of</strong> the electrokinetic flow in microchannels with internal<br />
electrodes<br />
Carsten Gizewski, Peter Ehrhard (TU Dortmund) Schedule<br />
In micr<strong>of</strong>luidic devices, electrokinetic phenomena can be engaged to manipulate liquids, particles,<br />
or cells. In general, electrokinetic phenomena are related to the existence <strong>of</strong> electrical double<br />
layers (EDL), which are present e.g. where solid walls are in contact with electrolytes. Due to<br />
surface charges <strong>of</strong> the solid, ions <strong>of</strong> opposite charge are attracted and lead to a thin electrically<br />
non-neutral zone the EDL. The application <strong>of</strong> an electrical field, consequently, leads to forces<br />
onto the fluid inside the EDL, capable <strong>of</strong> driving a flow within the microchannel. This particular<br />
flow is termed electroosmotic. If further, the electrodes are placed inside the microchannel, due
Section 9: Laminar flows and transition 215<br />
to small distances, strong inhomogeneous electrical fields can be induced, which in turn cause<br />
complex flow fields. This is true despite low applied electrode potentials <strong>of</strong> a few Volts. Numerical<br />
simulations <strong>of</strong> various authors have shown the potential for pumping and mixing <strong>of</strong> such complex<br />
flows in microchannels with internal electrodes.<br />
We focus on the electroosmotic flow within rectangular microchannels <strong>of</strong> 100 x 200 µm cross<br />
section. In each microchannel eight pairs <strong>of</strong> electrodes are placed onto the top and bottom glass<br />
covers, whereas the <strong>of</strong>fset <strong>of</strong> the electrodes is chosen differently in each <strong>of</strong> the microchannels. Due<br />
to the limited optical access through the glass covers, only the two velocity components which<br />
are tangential to the glass cover are accessible by means <strong>of</strong> the micro-particle-image velocimetry<br />
(µPIV). The expected electroosmotic flow, however, features vortices which cannot be recognized<br />
within this velocity plane. Therefore, a number <strong>of</strong> two-dimensional, two-component velocity<br />
fields are measured at different heights <strong>of</strong> the microchannel. From an integration <strong>of</strong> the continuity<br />
equation, subsequently, the third velocity component, which is normal to the glass cover, can<br />
be determined at reasonable accuracy. A further difficulty arises from the fact that the microparticles,<br />
used for µPIV, are not electrically neutral. Hence, in addition to drag forces from the<br />
electroosmotic flow, they experience electrophoretic forces. Hence, the particle movement appears<br />
to be a superposition <strong>of</strong> electroosmotic and electrophoretic effects.<br />
Flow characterization in a bioaffinity enrichment system for detection <strong>of</strong> relevant<br />
microorganisms in food<br />
A. Osorio Nesme, R. Benning, A. Delgado, (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
In food industry the quality assurance and consumer protection represent essential requirements<br />
for preserving high product ratings and competitiveness. Decreases in food quality or risks to<br />
consumers health must be properly detected in time to avoid image damage to the companies<br />
or risks from the product liability. In particular, the detection <strong>of</strong> microorganisms is <strong>of</strong> great<br />
importance. In general, this can be carried out by the routine microbiological diagnostic, whose<br />
negative results can be obtained only after 24 (Staphylococcus aureus) or 48 hours (Bacillus<br />
cereus). Furthermore, the confirmation <strong>of</strong> positive samples can take up to 144 hours. From the<br />
perspective <strong>of</strong> the current state <strong>of</strong> art, this analysis time could be for the microorganisms S.<br />
aureus and B. cereus significantly reduced by means <strong>of</strong> the development and combination <strong>of</strong> new<br />
analytical techniques. In the present study, a new system for direct detection <strong>of</strong> S. aureus and<br />
B. cereus (spores) through bioaffinity enrichment is introduced by means <strong>of</strong> a fully automated<br />
selective-microarray device (microporous columns) for milk and whey. The system consists <strong>of</strong><br />
a monolithic column with a microporous structure, in which biological receptors (monoclonal<br />
antibodies or aptamers) are immobilized on the surface. These receptors have a specific interaction<br />
with the microorganisms (bioaffinity). The matrix (milk) flows through the monolithic column,<br />
allowing the microorganisms to come in contact with the receptors and get bound to the column<br />
surface. It has been found that the amount <strong>of</strong> microorganisms captured during the process depends<br />
not only on the binding kinetics but also on the flow characteristics. High flow rates signify<br />
less residence time <strong>of</strong> the microorganism in the column and therefore less probability <strong>of</strong> getting<br />
captured. The flow velocity and flow distribution along the column have a direct impact on the<br />
binding process (microorganism enrichment). An important part <strong>of</strong> the present work consists <strong>of</strong><br />
the optimization <strong>of</strong> the column geometry by means <strong>of</strong> numerical simulations. The influence <strong>of</strong> the<br />
inlet form <strong>of</strong> the monolithic column on both flow and pressure distribution is investigated.
216 Section 10: Turbulence and reactive flows<br />
Section 10: Turbulence and reactive flows<br />
Organizers: Stefan Braun (TU Wien), Reinhard Farwig (TU <strong>Darmstadt</strong>)<br />
S10.1: Reactive flows and turbulent heat transfer Tue, 13:30–15:30<br />
Chair: S. Braun, R. Farwig S1|01–A02<br />
Free energy budgets in viscoelastic natural convection<br />
Elisabetta De Angelis (University <strong>of</strong> Bologna) Schedule<br />
It has been known for over fifty years that the introduction <strong>of</strong> a small amount <strong>of</strong> polymer additives<br />
could significantly reduce friction drag in wall-bounded turbulent flows. However, in the last years<br />
also the effect <strong>of</strong> polymers on turbulent thermal convection has drawn attention with controversial<br />
results. In fact, a recent experiment has been conducted in an Rayleigh-Bénard convection cell<br />
with and without polymers and a monotonic decrease <strong>of</strong> the Nusselt number (Nu, the ratio <strong>of</strong><br />
actual heat flux over that if there were only conduction) with increasing polymer concentration<br />
was found. Whereas, a direct numerical simulation (DNS) study, where top and bottom walls<br />
have been replaced by periodic boundary conditions, has shown an increase in Nu. Since it is not<br />
easy to remove walls in the experiments, in order to assess the presumed role <strong>of</strong> the boundary<br />
layers in the physics <strong>of</strong> the convection with polymers, new simulations are proposed. Namely, a<br />
Direct Numerical Simulation <strong>of</strong> natural convection between parallel walls have been performed<br />
at a modest but turbulent Rayleigh Number Ra, for varying polymers parameters. The present<br />
results confirm an increase <strong>of</strong> the Nusselt number i.e. heat transfer for all the cases studied when<br />
the polymer are highly stretched. Related to the enhancement <strong>of</strong> the heat transfer a deep modification<br />
<strong>of</strong> the structure <strong>of</strong> the convection cells is observed. A detailed description <strong>of</strong> the polymer<br />
free energy redistribution in such flows will be the subject <strong>of</strong> the present contribution.<br />
Ahlers, G. and Nikolaenko, A., “Effect <strong>of</strong> a polymer additive on heat transport in turbulent<br />
Rayleigh-Bénard convection,” Physical Review Letters, 104, 34503 (2010).<br />
Benzi, R., Ching, E.S.C. and De Angelis, E., “Effect <strong>of</strong> Polymer Additives on Heat Transport in<br />
Turbulent Thermal Convection,” Physical Review Letters, 104, 24502 (2010).<br />
Numerical investigation <strong>of</strong> lean-premixed turbulent flame using combustion LES including<br />
thickened flame model<br />
A. Hosseinzadeh, A. Sadiki, J. Janicka (TU <strong>Darmstadt</strong>) Schedule<br />
Lean premixed combustion is recently a theme <strong>of</strong> interest in gas turbines and other industrial<br />
applications in an effort towards Nox emission reduction, which is a result <strong>of</strong> lower flame temperature<br />
comparing to non-premixed flames. However, instabilities occurring in a combustion chamber<br />
under lean premixed combustion, may lead to the operation efficiency and life cycle degradation.<br />
Thus, LES as an adequate tool can be used to investigate the addressed unsteady phenomena.<br />
In the present work a lean premixed turbulent Bunsen Type flame [1] is numerically investigated<br />
using incompressible LES including the dynamic smagorinsky model for the flow filed, the eddy<br />
diffusivity model for the scalar flux and thickened flame model coupled with tabulated chemistry<br />
for the combustion [2]. The burner is equipped with a square matrix turbulence generator consisting<br />
<strong>of</strong> 32 boreholes, which induce a turbulent intensity <strong>of</strong> Tu= 8% in the reaction zone.<br />
The well known in house code FASTEST 3D, has been used for this investigation. The preliminary<br />
results <strong>of</strong> flow characteristics, Temperature and combustion quantities <strong>of</strong> the investigated<br />
configuration show a very good agreement to the experimental data.<br />
[1] Zajadatz, M., Hettel, M., Leuckel, W. Burning velocity <strong>of</strong> high-turbulence natural gas flames
Section 10: Turbulence and reactive flows 217<br />
for gas turbine application. In: International Gas Research conference. pp. 793-803.<br />
[2] Künne, G. , Ketelheun, A. , Janicka, J. : LES modeling <strong>of</strong> premixed combustion using a<br />
thickened flame approach coupled with FGM tabulated chemistry. In: Combustion and<br />
Flame 158. pp. 1750-1767.<br />
Large Eddy Simulation <strong>of</strong> Scalar Field in a High-Pressure Combustor fuelled with<br />
Pre-Vaporized Kerosene<br />
A.Hosseinzadeh, P. Pantangi, A. Sadiki, J.Janicka (TU <strong>Darmstadt</strong>) Schedule<br />
Turbulent mixing is one <strong>of</strong> the important phenomena which govern the chemical reactions in both<br />
chemical and combustion processes. In recent times the interest for developing comprehensive<br />
numerical models, which are able to predict more precisely the mixing phenomenon <strong>of</strong> scalars in<br />
complex systems, is increasing. In both cases <strong>of</strong> gaseous and liquid flows with chemical reactions,<br />
scalar transport and mixing can be a rate determining step, so that there is a need <strong>of</strong> scalar flux<br />
models that are accurate and efficient in both environments simultaneously.<br />
In the present work the capability <strong>of</strong> an existing and a newly developed sub grid-scale (SGS)<br />
model for the filtered scalar flux vector in the scalar transport equations <strong>of</strong> reactive scalars,<br />
namely the dynamic eddy diffusivity model (EDM) and the dynamic anisotropic eddy diffusivity<br />
model (AEDM), will be assessed for large eddy simulations (LES) <strong>of</strong> complex configurations. For<br />
this purpose, the EKT high pressure kerosene combustion chamber operated with pre-vaporized<br />
kerosene along swirled air as oxidant under non-premixed conditions is simulated using the in<br />
house FASTEST-3D CFD code. The code includes additionally dynamic Smagorinsky SGS model<br />
for the flow field and a flamelet generated manifold (FGM)-tabulated chemistry based approach<br />
for the combustion.<br />
Since comprehensive validation experimental data are available, the simulation results with<br />
both SGS scalar flux models are compared with experimental data, respectively. Besides the model<br />
sensitivity a grid sensitivity studies with coarse and fine meshes have been carried out to<br />
highlight any parameter and grid dependency. The simulation in both grid levels showed that<br />
the AEDM, that obviously involves more physical features, could provide better results than the<br />
EDM. In particular, the investigations have proved that using advanced models for SGS scalar<br />
uxes leads to a less mesh dependent simulation in complex configurations and to a reliable scalar<br />
field prediction without additional computational costs.<br />
A Tensorial Eddy Diffusivity based Subgrid Scale Model for Scalar Flux and its<br />
Validation in Turbulent Reactive Flows<br />
P. Pantangi (TU <strong>Darmstadt</strong>), H. Ying (Chinese Academy <strong>of</strong> Sciences Dalian), A. Sadiki (TU<br />
<strong>Darmstadt</strong>) Schedule<br />
In both diffusion and premixed combustion modes and in partially premixed combustion chemical<br />
reactions that occur are promoted by mixing processes. While in a premixed flame, a thin reaction<br />
layer propagates in the fuel/air mixture where the propagation speed is governed by chemical<br />
reactions and diffusion <strong>of</strong> species between the reaction zone and the preheat zone, chemical reactions<br />
in diffusion flames also occur in very thin layers where the combustion process is governed<br />
by the diffusion <strong>of</strong> fuel and air to the reaction zones. In both cases turbulence length scales are<br />
mainly larger than the thickness <strong>of</strong> reaction layers, so that one <strong>of</strong> the main effects <strong>of</strong> turbulence is<br />
to wrinkle the reaction layers and to increase the surface area <strong>of</strong> the reaction layers and the fuel<br />
conversion rate. Deeper understanding and reliable modelling <strong>of</strong> the turbulence/flame interaction<br />
together with the mixing control are challenging for designers <strong>of</strong> spark-ignition engines (premixed
218 Section 10: Turbulence and reactive flows<br />
flames), diesel engines (diffusion flames) and modern aircraft combustors (lean premixed flames or<br />
partially premixed spray flames). To meet the need for a reliable predictive method, it is essential<br />
that turbulent SGS models for scalar in CFD should be able to address accurately major mixing<br />
transport effects at low computational cost.<br />
This paper presents a newly developed Sub-Grid-Scale (SGS) scalar flux model and its validation<br />
on diffusion and premixed configurations. The model that results from a general tensorial representation<br />
theory is especially constrained by the second law <strong>of</strong> thermodynamic via the entropy<br />
inequality to yield a practical model. This emerges in form <strong>of</strong> an explicit and algebraic expression<br />
including a tensorial eddy diffusivity that is quadratic in terms <strong>of</strong> scalar gradients that can, in<br />
turn, be linked to scalar dissipation rate. The model parameters are prescribed by the so-called<br />
projection method allowing a dynamic evaluation.<br />
The combustion LES tool includes additionally a dynamic Smagorinsky SGS model for the flow<br />
field and a tabulated detailed chemistry based on a flamelet generated manifold (FGM) approach,<br />
in which a variable local equivalence ratio due to a possible entrainment <strong>of</strong> the environment air<br />
is included through a mixture fraction variable. A presumed pdf approach has been considered to<br />
account for the turbulence-combustion interaction process. All these models are integrated into<br />
the in house finite volume FASTEST3D code. To assess the prediction capability, LES results are<br />
compared against experimental data and results achieved by using some existing SGS models. An<br />
overall satisfactory agreement for the flow field quantities, species concentrations and SGS scalar<br />
fluxes is accomplished with the new model.<br />
Quasi-DNS <strong>of</strong> a Turbulent Premixed Flame treated as a Gasdynamic Discontinuity<br />
S. Strein, C. Bruzzese, A. G. Class (KIT) Schedule<br />
For a description <strong>of</strong> a premixed turbulent flame based on first principles, it is necessary to solve<br />
a highly coupled system <strong>of</strong> equations including complex chemistry. The required spatial and temporal<br />
resolution <strong>of</strong> a premixed turbulent flame leads to high computational costs. An attractive<br />
approach reducing the effort is to describe a flame front as a gasdynamic discontinuity [1]. Governing<br />
equations become the conservation equations for mass and momentum coupled to a level<br />
set equation describing the kinematics <strong>of</strong> the flame front.<br />
We present an implementation employing the level set approach using the open source C++<br />
library OPENFOAM R○. A quasi-DNS (direct numerical simulation) <strong>of</strong> a turbulent premixed flame<br />
in a two-dimensional box is realized to show the high efficiency <strong>of</strong> the method. Suitable deterministic<br />
boundary conditions representing the unsteady nature <strong>of</strong> the turbulent flow field with a given<br />
integral length scale are generated by a diffusion operator acting on a random field [2]. Statistic<br />
values for the turbulent flame velocity are extracted and compared to previous investigations.<br />
This work is supported by DFG grant SFB 606.<br />
[1] A.G. Class, B.J. Matkowksy, A.Y. Klimenko, A Unified Model <strong>of</strong> Flames as Gasdynamic<br />
Discontinuities, J. Fluid Mech 491 (2003), 11 – 49.<br />
[2] A. Kempf, M. Klein, J. Janicka, Efficient Generation <strong>of</strong> Initial- and Inflow-Conditions for<br />
Transient Turbulent Flows in Arbitrary Geometries, Flow, Turbulence and Combustions 74<br />
(2005), 67 – 84.<br />
Compressible Large-Eddy Simulation <strong>of</strong> Boundary-Layer Heat Transfer in a Turbulent<br />
Convective Flow<br />
Rodion Groll, Claudia Zimmermann, Hans J. Rath (<strong>Universität</strong> Bremen) Schedule
Section 10: Turbulence and reactive flows 219<br />
Computing the heat transfer through the fluid between two heat controlled plates the compressible<br />
fluid is accelerated by local density differences. Investigating the convective heat transfer <strong>of</strong> this<br />
Rayleigh-Benard convection. The temperature distribution shows increasing temperature gradients<br />
directly close to the wall. In the center region the heat transfer is defined by the convective<br />
mass exchange.<br />
The described convective mass transfer generates turbulent shear layers parallel to the gravity<br />
direction. Because <strong>of</strong> the transient turbulence and the high local density gradients the simlation<br />
works with a coupled model for the compressible Large-Eddy simulation.<br />
The investigated Rayleigh numbers are in the region between 6 · 10 7 and 4 · 10 8 . Therefore<br />
a direct correlation between Rayleigh number and Nusselt number is detected. Discussing the<br />
results the asymmetric temperature pr<strong>of</strong>iles are explainable according to the density weighted<br />
velocity pr<strong>of</strong>ile. The simulation results are compared with experimental data [1] and analytical<br />
model results [2].<br />
[1] A. Ebert, C. Resagk, A. Thess, Experimental study <strong>of</strong> temperature distribution and local<br />
heat flux for turbulent Rayleigh-Bénard convection <strong>of</strong> air in a long rectangular enclosure,<br />
Int. J. <strong>of</strong> Heat and Mass Transfer, 51 (2008), 4238-4248.<br />
[2] M. Hoelling, H. Herwig, Asymptotic analysis <strong>of</strong> heat transfer in turbulent Rayleigh-Benard<br />
convection, Int. J. <strong>of</strong> Heat and Mass Transfer, 49 (2006), 1129-1136.<br />
S10.2: Fundamental aspects <strong>of</strong> turbulent flows Tue, 16:00–18:00<br />
Chair: R. Farwig, S. Braun S1|01–A02<br />
Generating turbulent scaling laws from the multi-point equations using Lie theory<br />
Andreas Rosteck, Martin Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
The main aim is to give an analytic description <strong>of</strong> statistical turbulence behaviour and, in particular,<br />
to determine turbulent scaling laws. The governing equations shall be analysed using the<br />
Lie theory and the related Lie symmetries.<br />
The starting point <strong>of</strong> the entire analysis is the infinite set <strong>of</strong> multi-point correlation (MPC)<br />
equations, which are direct statistical consequences <strong>of</strong> the Navier-Stokes equations. In order to<br />
gain differential equations for the multi-point correlations denoted by Ri {n+1} = Ri (0)i (1)...i (n) =<br />
ui (0) (x(0)) · . . . · ui (n) (x(n)) , where the correlation <strong>of</strong> n + 1 turbulent velocity components is consi-<br />
dered, the infinite set <strong>of</strong> correlation equations<br />
Ti = {n+1} ∂Ri n�<br />
�<br />
∂<br />
{n+1}<br />
+ + Ri ∂t<br />
{n+1}[i (l)↦→k (l)]<br />
Ūi (x<br />
(l) (l))<br />
+ ∂xk (l)<br />
∂Pi {n}<br />
[l]<br />
∂xi (l)<br />
l=0<br />
Ūk (l) (x(l)) ∂Ri {n+1}<br />
∂xk (l)<br />
−ν ∂2Ri ∂ui uk (x<br />
{n+1}<br />
(l) (l) (l))<br />
−Ri ∂xk ∂xk {n}[i (l)↦→∅]<br />
+ ∂xk (l) (l)<br />
(l)<br />
∂Ri {n+2}<br />
[i<br />
(n+1)<br />
↦→k<br />
(l) ][x (n+1)↦→x (l)]<br />
∂xk (l)<br />
�<br />
=0 ,<br />
for n = 1, 2, 3, . . . is introduced, which also has to be extended by additional continuity equations.<br />
First we determine the Lie symmetries <strong>of</strong> the multi-point equations. It is clear that all Lie<br />
symmetries <strong>of</strong> the Navier-Stokes equations can be transferred to the multi-point equations. However,<br />
these are not the only symmetries holding for the MPC-equations. Additional symmetries,<br />
which we call stastistical symmetries, can be found. At this point we have found an additional<br />
scaling symmmetry and also translation symmetries <strong>of</strong> the MPC have been identified.<br />
These new statistical groups have important consequences on our understanding <strong>of</strong> turbulent<br />
scaling laws to be exemplarily revealed by two examples. Firstly, one <strong>of</strong> the key foundations <strong>of</strong>
220 Section 10: Turbulence and reactive flows<br />
statistical turbulence theory is the universal law <strong>of</strong> the wall with its essential ingredient, the logarithmic<br />
law. We demonstrate that the log-law fundamentally relies on one <strong>of</strong> the new translational<br />
groups. Furthermore, we consider a rotating channel flow, whose scaling behaviour can only be<br />
described using the new statistical symmetries. It can be seen that the direction <strong>of</strong> rotation axes<br />
plays an important role, because different axes result in different scaling laws.<br />
DNS <strong>of</strong> a Turbulent Poiseuille Flow with Uniform Wall Transpiration<br />
V.S. Avsarkisov, M. Oberlack (TU <strong>Darmstadt</strong>), I. Vigdorovich (Institute <strong>of</strong> Mechanics, Moscow<br />
State University), G. Khujadze (TU <strong>Darmstadt</strong>) Schedule<br />
A fully developed, plane constant-mass-flux turbulent Poiseuille flow with wall transpiration<br />
i.e. uniform blowing and suction on the walls is investigated by the direct numerical simulation<br />
(DNS) <strong>of</strong> the three-dimensional, incompressible Navier-Stokes equations. The DNS is conducted<br />
at Reτ = 250, 480 for different relative transpiration velocities by means <strong>of</strong> the numerical code<br />
developed by School <strong>of</strong> Aeronautics, Technical University <strong>of</strong> Madrid [1]. Existance <strong>of</strong> the uniform<br />
transpiration implies asymmetry <strong>of</strong> the mean velocity pr<strong>of</strong>ile and the Reynolds shear stresses [2].<br />
The flow on the blowing side is highly populated with small scale vortical structures, while on the<br />
suction side vortical structures appear rarely and in larger scales. Thus, transverse velocity not<br />
only redistributes, but also produces Reynolds stresses on the blowing side. As a result, viscous<br />
sublayer becomes thiner on the blowing side and log-law region wider.<br />
The DNS data are used to validate a new turbulent logarithmic scaling law derived from Lie<br />
symmetry theory <strong>of</strong> the infinite dimensional multi-point correlation equation and is principally<br />
different from the classical near-wall log-law [3,4]. It is shown that the DNS data agrees with the<br />
new turbulent scaling law over practically the whole cross-section <strong>of</strong> the channel.<br />
[1] S. Hoyas, J. Jiménez, Scaling <strong>of</strong> velocity fluctuations in turbulent channels up to Reτ = 2000,<br />
Phys. <strong>of</strong> Fluids 18 (2006), 011702-1-3.<br />
[2] Y. Sumitani, N. Kasagi, Direct numerical simulations <strong>of</strong> turbulent transport with uniform<br />
wall injection and suction, AIAA Journal 33(7) (1995), 1220-1228.<br />
[3] M. Oberlack, Symmetrie, Invarianz und Selbstähnlichkeit in der Turbulenz, Habilitation thesis<br />
(2000), RTWH Aachen.<br />
[4] M. Oberlack, A. Rosteck, New statistical symmetries <strong>of</strong> the multi-point equations and its<br />
importance for turbulent scaling laws, Discrete Contin. Dyn. Syst., Ser. S 3 (2010), 451-<br />
471.<br />
Application <strong>of</strong> the extended group analysis to the functional formulation <strong>of</strong> the Burgers<br />
equation<br />
Wacławczyk Marta, Oberlack Martin (TU <strong>Darmstadt</strong>) Schedule<br />
Description in terms <strong>of</strong> the characteristic functional is a one <strong>of</strong> the possible approaches to specify<br />
statistical properties <strong>of</strong> random fields fluctuating in time or space. The functional calculus has<br />
been introduced in the seminal work <strong>of</strong> E. Hopf [1] for the phenomenon <strong>of</strong> turbulence. In statistical<br />
mechanics the system <strong>of</strong> N particles with positions x1, . . . , xN and velocities u1, . . . , uN can<br />
be described by the probability density function P (x1, . . . , xN, v1, . . . , vN, t). We consider now<br />
the continuum limit (e.g. hydrodynamics) where the number <strong>of</strong> particles go to infinity and the<br />
elements <strong>of</strong> the phase space <strong>of</strong> velocity v1, . . . , vN become a continuous function v(x). In this case<br />
the system is described by the probability density functional P ([v(x)], t). Its Fourier transform in
Section 10: Turbulence and reactive flows 221<br />
the functional space is called the characteristic functional and will be denoted by Φ([y(x)], t). Multipoint<br />
statistics <strong>of</strong> any order are computed by taking successive functional derivatives δ/δyα(x)<br />
<strong>of</strong> Φ evaluated at y = 0<br />
δk �<br />
Φ([y(x)], t)<br />
�<br />
�<br />
� = i<br />
δyα(x1)δyβ(x2) . . . δyγ(xk) �<br />
y=0<br />
k uα(x1, t)uβ(x2, t) . . . uγ(xk, t) (1)<br />
Hence, the characteristic functional fully characterises the random field. The time evolution <strong>of</strong><br />
Φ is described by a functional differential equation with functional derivatives. Such general<br />
description is, however, hardly tractable due to missing analytical methods. We believe that the<br />
Lie group analysis extended towards functional differential equations in Oberlack & Wacławczyk<br />
[2] is a step towards development <strong>of</strong> such methods and may give a chance to treat such type <strong>of</strong><br />
functional equations. The analysis is applied to the functional formulation <strong>of</strong> the Burgers equation<br />
which is <strong>of</strong>ten treated as a ”toy model” <strong>of</strong> the Navier-Stokes equations. We have shown that the<br />
considered functional equation has an infinite set <strong>of</strong> symmetry transformations. After solving<br />
a hyperbolic equation with the derived infinitesimals invariant solutions for the characteristic<br />
functional <strong>of</strong> the Burgers equation equations are found. Next, by successive differentiation, cf.<br />
Eq. (1) the multipoint statistics are derived and their physical meaning is discussed.<br />
[1] E. Hopf, Statistical hydromechanics and functional calculus, J. Rational Mech. Anal. 1 (1952),<br />
87 – 123.<br />
[2] M. Oberlack, M. Wacławczyk, On the extension <strong>of</strong> Lie group analysis to functional differential<br />
equations, Arch. Mech. 58 (2006), 597 – 618.<br />
Length scale analysis in turbulent Poiseuille flow<br />
Fettah Aldudak, Martin Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
Geometrical structures in wall-bounded turbulent flow are investigated by means <strong>of</strong> dissipation<br />
element (DE) and streamline segment (SLS) analysis. The scalar fields obtained by Direct Numerical<br />
Simulations (DNS) for the turbulent channel flow are decomposed into numerous finite<br />
size regions using the DE method proposed by [1]. Therefore, local pairs <strong>of</strong> minimal and maximal<br />
points in the scalar field φ(x, y, z, t) are detected where ∇φ = 0. Gradient trajectories <strong>of</strong> finite<br />
length starting from every point in the scalar field in the directions <strong>of</strong> ascending and descending<br />
scalar gradients will reach a minimum and a maximum point with ∇φ = 0. All points belonging<br />
to the same pair <strong>of</strong> extremal points defines a DE. Hence, the decomposition <strong>of</strong> the domain into<br />
DEs follows from the structures <strong>of</strong> the flow itself and is completely space filling the turbulent<br />
field.<br />
The linear distance ℓD between the extremal points and the absolute value <strong>of</strong> the scalar<br />
difference ∆φ at these two points mark the key parameters to parameterize the geometry and the<br />
field variable structure <strong>of</strong> the DE. We find that the mean DE length is in the order <strong>of</strong> the Taylor<br />
scale supporting the results in [1] for the case <strong>of</strong> homogeneous shear turbulence. In addition, DE<br />
length scale reveals a clear dependency on wall-normal distance y.<br />
Streamline segment analysis is another way to classify spatial structures in turbulent fields.<br />
Here, extremal points <strong>of</strong> the velocity magnitude along streamlines are identified marking the<br />
beginning and ending points <strong>of</strong> the respective segment. Dependent on the gradient <strong>of</strong> the velocity<br />
magnitude, SLS are classified as positive or negative segments. We, again, investigate the length<br />
ℓS <strong>of</strong> these structures in a turbulent channel flow as a function <strong>of</strong> distance from the wall y. In
222 Section 10: Turbulence and reactive flows<br />
this context, a strong wall-normal dependency is found. Positive segments appear to be larger in<br />
average.<br />
Furthermore, we examine the probability density function (pdf ) P <strong>of</strong> both length scales in<br />
different wall-normal regions. Large differences between the curves are observed. However, after<br />
normalizing the pdf with the corresponding mean length, the curves coincide with each other<br />
except for the near-wall layer. This behavior is a strong indication toward a Lie scaling group and<br />
its corresponding similarity -revealing a self-similar behavior with respect to the wall distance.<br />
[1] N. Peters, L. Wang, Dissipation element analysis <strong>of</strong> scalar fields in turbulence, C. R. Mech.<br />
334 (2006), 433-506.<br />
S10.3: Turbulent flows: measurements and simulations Wed, 13:30–15:30<br />
Chair: R. Farwig, S. Braun S1|01–A02<br />
Investigation <strong>of</strong> structure and non-gradient turbulent transfer in swirling flows<br />
Ðorđe Čantrak (University <strong>of</strong> Belgrade), Martin Gabi (KIT), Novica Janković, Svetislav Čantrak<br />
(University <strong>of</strong> Belgrade) Schedule<br />
Non-gradient turbulent diffusion and non-local turbulent transfer are significant characteristics<br />
<strong>of</strong> turbulent swirling flows. Turbulence structure is being investigated in this paper, on the basis<br />
<strong>of</strong> experimental and theoretical numerical results. Investigation <strong>of</strong> the structure and mechanics<br />
<strong>of</strong> turbulent transport processes is difficult because the turbulent swirling flows are threedimensional,<br />
inhomogeneous and anisotropic flows with shear. Contemporary optical measuring<br />
techniques laser Doppler anemometry (LDA) and stereo particle image velocimetry (PIV) are<br />
applied. Analysis proves that the presence <strong>of</strong> swirl has, as a consequence, non-local turbulent<br />
transfer, what should be modeled adequately. Experimentally determined distributions <strong>of</strong> correlation<br />
and statistical moments <strong>of</strong> the second and higher order give closer insight into physics <strong>of</strong><br />
turbulence, which results in better modeling <strong>of</strong> very complex transport processes in turbulent<br />
swirling flow in a pipe. Investigation <strong>of</strong> the structure and statistical properties in the vortex core<br />
and shear layer in turbulent swirling flow is <strong>of</strong> special significance. This gives closer insight into<br />
the physics <strong>of</strong> turbulent transfer processes in internal swirling flows.<br />
Flow over back-facing step in a narrow channel<br />
Václav Uruba, Ondřej Hladík, Pavel Joná (Czech Academy <strong>of</strong> Sciences) Schedule<br />
Flow structure behind the back-facing step in a narrow channel will be studied in details. The<br />
step height will be about 15 percent <strong>of</strong> the channel width. The contra-rotating secondary vortices<br />
in corners <strong>of</strong> the input channel detach on the step edge and interact together forming impinging<br />
structure on the channel floor behind the step. The vortices behavior will be observed using stereo<br />
PIV technique. Time-mean 3D structures behind the step are to be evaluated and shown in the<br />
paper.<br />
Hot-wire measurement in turbulent flow behind a parallel-line heat source<br />
Pavel Antos, Vaclav Uruba (Czech Academy <strong>of</strong> Sciences) Schedule<br />
A paper describes used HWA method <strong>of</strong> measurement in non-isothermal flow. A dual hot-wire<br />
probe was employed. Velocity and temperature calibration including static and dynamic part are<br />
described were done. Procedure <strong>of</strong> evaluation observed quantities is described in detail. An interaction<br />
<strong>of</strong> the free turbulent flow and the temperature field generated by parallel line heat sources<br />
was investigated. The velocity and the temperature distributions behind the heat generator are
Section 10: Turbulence and reactive flows 223<br />
presented in the paper.<br />
Crude estimate <strong>of</strong> velocity distributions from Truckenbrodt’s energy and momentum<br />
coefficients<br />
Herbert Niessner (NiMa Baden-Rütih<strong>of</strong>/Switzerland) Schedule<br />
One <strong>of</strong> the simplest models for the velocity distribution in a pipe cross-section dependent on two<br />
parameters consists <strong>of</strong> two layers <strong>of</strong> different thickness and velocity. Unfortunately relative thickness<br />
and velocity <strong>of</strong> the wall layer cannot be expressed analytically in terms <strong>of</strong> Truckenbrodt’s<br />
energy and momentum coefficents. But relative thicknesses <strong>of</strong> a three layer model with wall and<br />
intermediate layer having opposite core and zero velocity can be. Reasonable in case <strong>of</strong> strong<br />
reverse wall flow only they allow a crude estimate <strong>of</strong> the parameters <strong>of</strong> the two layer model, which<br />
may serve as initial values in computing them iteratively.<br />
Coarse-Grid-CFD (CGCFD) using a Porous-Media formulation<br />
A. G. Class, M. Viellieber (KIT) Schedule<br />
Computational fluid dynamics (CFD) simulations for large complex geometries like the complete<br />
reactor core <strong>of</strong> a nuclear power plant requires exceedingly huge computational resources. State<br />
<strong>of</strong> the art computational power and CFD s<strong>of</strong>tware is restricted to simulations <strong>of</strong> representative<br />
sections <strong>of</strong> these geometries.<br />
The conventional approach to simulate such complex geometries is 1D subchannel analysis<br />
employing experimental correlations in the transport models. The development <strong>of</strong> the CGCFD<br />
(1,2) provides an alternative method to the traditional 1D subchannel analysis and does not rely<br />
on experimental data.<br />
The CGCFD is based on strongly under-resolved CFD and inviscid Euler equations. Although<br />
the use <strong>of</strong> the Euler equations and coarse grids does not capture the subgrid physics, i.e. viscous<br />
dissipation or turbulence, the subgrid physical information is taken into account by volumetric<br />
source terms derived from fully resolved representative CFD simulations. Non-resolved geometrical<br />
information in the very coarse meshes is taken into account by appropriate volume and surface<br />
porosities in the finite volume scheme. Such a porous media approach was originally used in the<br />
COMMIX (3) code which was designed to compute complex flow applications in a time when<br />
computational resources where limited.<br />
The benefits and limitations <strong>of</strong> our technique are explored by simulating a section <strong>of</strong> a water<br />
rod bundle containing a spacer. General recommendations for the proper application <strong>of</strong> our<br />
technique are presented in this work.<br />
[1] A. G. Class, M. O. Viellieber, A. Batta: Coarse-Grid-CFD for pressure loss evaluations in rod<br />
bundles, International Congress <strong>of</strong> Advances in Nuclear Power Plants(ICAPP) 2011, Nizza<br />
[2] S. R. Himmel: Modellierung des Strömungsverhaltens in einem HPLWR-Brennelement mit<br />
Drahtwendelabstandshaltern, Dissertation Forschungszentrum Karlsruhe 2009<br />
[3] T. H. Chien, H. M. Domanus, W. T. Sha: A Three-Dimensional Transient Multicomponent<br />
Computer Program for Analyzing Performance <strong>of</strong> Power Plant Condensers Volume I: Equations<br />
and Numerics, Argonne National Laboratory 1993<br />
S10.4: Methodical aspects <strong>of</strong> turbulent flow computations Wed, 16:00–18:00<br />
Chair: S. Braun, R. Farwig S1|01–A02
224 Section 10: Turbulence and reactive flows<br />
Simulation <strong>of</strong> bubbly flow in a vertical turbulent channel<br />
Claudio Santarelli, Jochen Fröhlich (TU Dresden) Schedule<br />
Direct numerical simulations are performed to investigate the influence <strong>of</strong> bubble size and void<br />
fraction on turbulent channel flow. An immersed boundary method is employed to simulate the<br />
dispersed phase in an in-house finite-volume-based code, where each bubble is represented by Lagrangian<br />
marker points on its surface connected to the Eulerian description <strong>of</strong> the fluid via suitable<br />
interpolation algorithms and continuous direct forcing. The turbulent flow between two parallel<br />
walls at distance H is directed upwards and three different bubble loadings have been simulated:<br />
Sim.1: few small bubbles (Dp/H = 0.52, Np = 384, ɛ = 0.28%; being Dp the bubble diameter and<br />
Np the number <strong>of</strong> bubbles); Sim.2: many small bubbles (Dp/H = 0.52, Np = 2880, ɛ = 2.2%);<br />
Sim.3: many large bubbles (Dp/H = 0.75, Np = 913, ɛ = 2.2%). As expected, small bubbles are<br />
more likely to be found near the wall and show almost no influence on the mean velocity <strong>of</strong> the<br />
fluid. Large bubbles, with higher bubble Reynolds number, tend to accumulate in the center <strong>of</strong> the<br />
channel, strongly modifying the mean velocity <strong>of</strong> the fluid, with the lateral migration <strong>of</strong> bubbles<br />
apparently related to the bubble wake. Two-point correlations and flow visualizations show the<br />
formation <strong>of</strong> flow structures and the influence <strong>of</strong> the bubbles on the generation <strong>of</strong> turbulence.<br />
Statistical data for both, the liquid and the dispersed phase will be provided, including mean<br />
velocity pr<strong>of</strong>iles, turbulent fluctuations and void fraction distributions.<br />
Simulation <strong>of</strong> bed load transport in turbulent open channel flow<br />
Bernhard Vowinckel, Jochen Fröhlich (TU Dresden) Schedule<br />
In the present work direct numerical simulations <strong>of</strong> a particle laden open channel flow were carried<br />
out to investigate the interaction between the dispersed and the continuous phase. The dispersed<br />
phase is represented by an immersed boundary method. The particle-particle collisions are<br />
accounted for by a physically based collision model that guarantees a fully resolved four-way<br />
coupling <strong>of</strong> the flow [1]. Applying theses models, the fully turbulent open channel flow laden<br />
with spherical particles over a rough bed is simulated choosing different particle densities. Two<br />
cases, one with shear stress below the threshold <strong>of</strong> mobilization and the other with shear stress<br />
above the threshold are compared (Dp/H = 1/10, Np = 2000, ɛ = 0.12, Dp being the particle<br />
diameter, Np number <strong>of</strong> particles, H the depth <strong>of</strong> the fluid layer, and ɛ the volume fraction). The<br />
different density ratios lead to different types <strong>of</strong> modification <strong>of</strong> the flow field by the formation <strong>of</strong><br />
density-specific patterns <strong>of</strong> the particle. Light particles do not come to resting positions saltating<br />
evenly distributed in span-wise direction. Heavy particles tend to form stream-wise clusters <strong>of</strong><br />
inactive particles, that generate large scale flow structures. As a result different mechanisms <strong>of</strong><br />
transport occur. These mechanisms will be analyzed by means <strong>of</strong> particle statistics <strong>of</strong> both, rotation<br />
and translation, that have not appeared in literature so far. Two-point correlations suggest<br />
an alteration <strong>of</strong> the coherent structures.<br />
[1] T. Kempe and J. Fröhlich. On Euler-Lagrange coupling and collision modelling for spherical<br />
particles. ETMM8, p. 806-811, Marseille, France, 2010.<br />
Numerical simulation separation in the hydrocyclones <strong>of</strong> nonspherical particles<br />
Matvienko Oleg, Andropova Antonina (Tomsk State University <strong>of</strong> Architecture and Building)<br />
Schedule<br />
Hydrocyclones are used extensively for particle separation and classification in mineral, powderprocessing,<br />
environmental and chemical engineering.<br />
This paper presents the results <strong>of</strong> the mathematical modelling separation in the hydrocyclone<br />
<strong>of</strong> the nonspherical particles. The turbulent Reynolds equations were used for description <strong>of</strong> the
Section 10: Turbulence and reactive flows 225<br />
flow fields. The turbulence characteristics were calculated on the basis <strong>of</strong> two-equation k - ɛ model<br />
with a Richardson number Ri correction to the dissipation equation. The parameters <strong>of</strong> the flow<br />
depends on the solid concentration and the density and viscosity <strong>of</strong> the slurry. It is assumed that<br />
concentrated suspension influence fluid velocities via density and viscosity. In order to account<br />
the influence <strong>of</strong> particle concentration on the viscosity the Thomas expression was used. When<br />
calculating trajectories <strong>of</strong> nonspherical particles, both translational and rotational motions should<br />
be simultaneously considered, since these motions are coupled. The orientation distribution <strong>of</strong><br />
nonspherical particles in flows is an important factor affecting the cumulative transport properties<br />
<strong>of</strong> the fluidparticle system. Spheroidal particles are chosen for the investigation <strong>of</strong> the effect <strong>of</strong><br />
nonsphericity on particle hydrodynamic interactions and trajectories, since the force and torque<br />
acting on a stationary spheroid in creeping flows are well known for uniform flow, simple shear flow<br />
and for an arbitrary oriented spheroid adjacent to a planar wall. A typical hydrocyclone consists<br />
<strong>of</strong> a cylindrical section with a central tube connected to a conical section with a discharge tube.<br />
An inlet tube is attached to the top section <strong>of</strong> the cylinder. The fluid being injected tangentially<br />
into hydrocyclone causes swirling and thus generates centrifugal force within the device. This<br />
centrifugal force field brings about a rapid classification <strong>of</strong> particulate material from the medium in<br />
which it is suspended. Separation takes place in the radial direction, with coarse particles moving<br />
towards the wall and fines towards the axis. Coarse particles leave through the underflow, and<br />
fines through the overflow. The calculations <strong>of</strong> the cut size in several hydrocyclone geometries and<br />
also particles trajectories are calculated for both inertial and inertialess particles, the orientation<br />
<strong>of</strong> which is fixed or free. Lateral drift was found to occur for inertial particles with both fixed and<br />
free orientations. The results demonstrate that separation characteristics <strong>of</strong> the hydrocyclone are<br />
strongly depends on the flow shear rate, particle size, and particle shape. For a particle with a<br />
fixed orientation the transverse motion also strongly depends on the particle orientation.<br />
This research has been supported by the Alexander von Humboldt<br />
Dynamic Mode Decomposition (DMD) for Swirling Jet Flows<br />
Tobias Luginsland, Leonhard Kleiser (ETH Zürich) Schedule<br />
Swirling jets undergoing vortex breakdown occur in many technical applications, e.g. vortex burners,<br />
turbines and jet engines. At the stage <strong>of</strong> vortex breakdown the flow is dominated by a conical<br />
shear layer and a large recirculation zone around the jet axis.<br />
We performed Large-Eddy Simulations (LES) <strong>of</strong> compressible swirling jet flows at Re=5000,<br />
Ma=0.6 in the moderate to high swirl number regime (S=0.5 and 1.0). A nozzle is included in<br />
our computational setup to account for more realistic inflow conditions.<br />
The obtained velocity fields are analyzed by means <strong>of</strong> temporal and spatial dynamic mode decomposition<br />
(DMD) to get further insight into the characteristic structures dominating the flow.<br />
We present eigenvalue spectra for the different cases and discuss the stability behaviour in time<br />
and space. While the flows are temporarily stable, which is expected for quasi-steady flows after<br />
transition, unstable structures are found in the spatial investigation. For both moderate and high<br />
swirl numbers helical structures dominate the flow together with shear-layer instabilities.<br />
Implementation <strong>of</strong> low-Reynolds turbulence models in boundary element fluid dynamics<br />
algorithm<br />
Janez Lupse, Leopold Skerget, Jure Ravnik (University <strong>of</strong> Maribor) Schedule<br />
The article presents an implementation and testing <strong>of</strong> low-Reynolds RANS type turbulence models<br />
in boundary element fluid dynamics code. The governing equations are cast in velocity-vorticity<br />
form and are used to solve incompressible viscid fluid flow. In this form governing equations are<br />
given for kinematic and kinetic aspect <strong>of</strong> flow instead <strong>of</strong> mass and momentum conservation equa-
226 Section 10: Turbulence and reactive flows<br />
tions. Kinematics equations represent compatibility and restriction conditions between velocity<br />
and vorticity field functions and local expansion fields while kinetics equations represent transport<br />
<strong>of</strong> vorticity. For application <strong>of</strong> turbulence model, stress tensor has to be rewritten in such a way<br />
that an appropriate form for application <strong>of</strong> boundary elements is obtained. For weighting functions<br />
<strong>of</strong> governing equations integral representation Laplace and convective-diffusive fundamental<br />
solutions were used.<br />
Solution algorithm solves kinematics equation for unknown boundary vorticity values first,<br />
using single domain boundary element numerical method. In all <strong>of</strong> the steps following sub-domain<br />
technique is used to solve equations for unknown domain variables, e.g. velocity, vorticity, temperature...<br />
Sub-domain technique in our case yields overdetermined system <strong>of</strong> equations which is<br />
solved by LSQR type solver. When unknown boundary vorticity values are known calculation <strong>of</strong><br />
intermediate velocity field is possible. Next values <strong>of</strong> velocity field and boundary values <strong>of</strong> vorticity<br />
are used to solve vorticity transport equation. For turbulent flows last step is calculation <strong>of</strong><br />
unknown turbulence variables from intermediate velocity and vorticity fields. Two representative<br />
benchmark problems (channel flow and backward facing step) are used to assess the performance<br />
<strong>of</strong> presented algorythm.
Section 11: Interfacial flows 227<br />
Section 11: Interfacial flows<br />
Organizers: Dieter Bothe (TU <strong>Darmstadt</strong>), Bernhard Weigand (<strong>Universität</strong> Stuttgart)<br />
S11.1: Nucleation and Phase Transfer Tue, 13:30–15:30<br />
Chair: Claus-Dieter Munz S1|03–123<br />
Numerical Investigations on Nucleation Processes in Supercooled Droplets<br />
K. Eisenschmidt (<strong>Universität</strong> Stuttgart), T. Němec (Czech Academy <strong>of</strong> Sciences Prague), P. Rauschenberger,<br />
B. Weigand (<strong>Universität</strong> Stuttgart) Schedule<br />
We intend to numerically investigate the behaviour <strong>of</strong> droplets in supercooled clouds regarding<br />
freezing. These processes are <strong>of</strong> critical relevance for clouding.<br />
The numerical code for the simulations is the in-house code Free Surface 3D (FS3D), which is a<br />
solver for Direct Numerical Simulations (DNS) <strong>of</strong> incompressible multiphase flows. As a prerequisite<br />
for the numerical investigations on freezing the treatment <strong>of</strong> three phases as ice, liquid water<br />
and air has already been implemented.<br />
In the present paper we focus on the simulation <strong>of</strong> nucleation and growth <strong>of</strong> the nuclei.<br />
Nucleation in an undercooled droplet starts if water molecules form a cluster <strong>of</strong> critical size. The<br />
nuclei that are formed in that way will grow and the whole droplet begins to freeze. The freezing<br />
<strong>of</strong> the droplet is described on a macroscopic scale while the nucleation starts with few hundreds <strong>of</strong><br />
molecules and therefore takes place at a microscopic scale. The nucleation model that is currently<br />
implemented in FS3D works as a subscale model and links the microscopic view to the macroscopic<br />
description. The results will be shown in the presentation.<br />
The nucleation model is based on the Classical Nucleation Theory (CNT) approach. It predicts<br />
the ice nucleation rate J in supercooled water as a function <strong>of</strong> temperature. The nucleation rate<br />
J can be evaluated in each cell <strong>of</strong> the computational domain that is placed inside the undercooled<br />
droplet. From these nucleation rates J the number N <strong>of</strong> nuclei can be calculated as an integral<br />
value from the whole volume <strong>of</strong> the droplet V<br />
∆N<br />
∆t =<br />
�<br />
JdV . (1)<br />
The nuclei will grow and the macroscopic freezing starts. The microscopic growth is first calculated<br />
from a subscale model by evaluating the energy equation in the ice and in the water. Once the<br />
ice particle is large enough it could be tracked by the solver.<br />
Parametrization <strong>of</strong> the homogeneous ice nucleation rate for the numerical simulation<br />
<strong>of</strong> multiphase flow<br />
Tomáš Němec (Czech Academy <strong>of</strong> Sciences Prague), Kathrin Eisenschmidt, Philipp Rauschenberger,<br />
Bernhard Weigand (<strong>Universität</strong> Stuttgart) Schedule<br />
The numerical modelling <strong>of</strong> the freezing process <strong>of</strong> supercooled water droplets in the atmosphere<br />
requires a description <strong>of</strong> the nucleation <strong>of</strong> ice particles. The thermophysical property <strong>of</strong> interest<br />
is the nucleation rate J [m −3 s −1 ] describing the number <strong>of</strong> newly formed particles in the system<br />
per unit volume and unit time.<br />
There are several parametrizations <strong>of</strong> the experimentally measured ice nucleation rates available<br />
in the literature [1] for the temperatures 230 – 240 K relevant to homogeneous ice nucleation.<br />
There is however an uncertainty <strong>of</strong> 2 K in the estimation <strong>of</strong> the temperature in these experiments<br />
which is unsufficient for a precise simulation <strong>of</strong> atmospheric processes.
228 Section 11: Interfacial flows<br />
In this work, we employed the Classical Nucleation Theory (CNT) approach [2] for the prediction<br />
<strong>of</strong> the homogeneous ice nucleation rate. The evaluation <strong>of</strong> the CNT formulas requires<br />
accurate thermophysical data <strong>of</strong> both supercooled water and ice, i.e. density, vapor-equilibrium<br />
pressure, specific heat capacity, latent heat <strong>of</strong> melting, and the ice-water interfacial tension. As a<br />
result, the CNT predicts the nucleation rate J, the initial (critical) size <strong>of</strong> the ice particle r ⋆ , and<br />
the nucleation work W ⋆ needed to create the critical ice particle.<br />
The predicted ice nucleation rates show a good agreement with the experimental data from<br />
several authors. Some other experimental nucleation rates show a slight deviation from the CNT<br />
which might hint that the nucleation process during the experiment was influenced by heterogeneities<br />
or by surface effects. The temperature dependence <strong>of</strong> the theoretical homogeneous<br />
nucleation rate was fitted to a simple formula applicable to numerical CFD calculations <strong>of</strong> the<br />
freezing behavior <strong>of</strong> supercooled water droplets.<br />
[1] B. J. Murray, S. L. Broadley, T. W. Wilson, S. J. Bull, R. H. Wills, H. K. Christenson, and<br />
E. J. Murray. Kinetics <strong>of</strong> the homogeneous freezing <strong>of</strong> water. Physical Chemistry Chemical<br />
Physics, 12 (35):10380–10387, 2010.<br />
[2] Dimo Kashchiev. Nucleation - Basic Theory with Applications. Butterworth-Heinemann,<br />
2000.<br />
Volume <strong>of</strong> fluid based direct numerical simulation <strong>of</strong> ice growth<br />
P. Rauschenberger, K. Eisenschmidt, B. Weigand (<strong>Universität</strong> Stuttgart) Schedule<br />
In atmospheric clouds, water droplets may remain liquid down to a temperature <strong>of</strong> about −40 ◦ C.<br />
When nucleation starts, the initial particle grows and starts to form dendrites when reaching<br />
a certain critical radius. The freezing process <strong>of</strong> supercooled liquid water droplets in clouds is<br />
<strong>of</strong> great interest for weather forecast and is still not well understood today. We intend to do<br />
numerical investigations on this subject.<br />
Our in-house code Free Surface 3D (FS3D) is applied for the Direct Numerical Simulation<br />
(DNS) <strong>of</strong> incompressible multiphase flows and is based on the Volume <strong>of</strong> Fluid (VOF) method.<br />
The Navier-Stokes equations are spatially discretized on a fixed Eulerian grid. One prerequisite<br />
to perform the abovementioned simulations is the possibility to treat solid particles. This has<br />
already been implemented and validated. The rigid particles are treated as Eulerian ones and<br />
may move freely within the fluid phase. Furthermore, the code is currently extended to treat<br />
more than two phases, since the two phases <strong>of</strong> water (ice and liquid) and the surrounding gas<br />
phase appear simultaneously.<br />
The energy equation is solved in temperature form. For the phase change problem, we use a<br />
two-scalar representation <strong>of</strong> the temperature. This approach has already been applied for simulations<br />
<strong>of</strong> droplet evaporation. Temperature advection and heat conduction are done separately for<br />
the solid and the liquid temperature field (Ts and Tl), but they are coupled at the phase interface<br />
by the energy jump condition<br />
˙m ′′ ∆hs = λs∇T |s · nγ + λl∇T |l · nγ. (1)<br />
This means that in interface cells, three temperatures are present: Ts, Tl and the interface temperature<br />
Tγ, that can be determined with the Gibbs-Thomson relation.<br />
The particle growth and temperature distribution will be validated against known solutions.<br />
The growth <strong>of</strong> dendrites is subject for further research.
Section 11: Interfacial flows 229<br />
Curvature Driven Liquid-Vapour Flow in Compressible Fluids<br />
Christoph Zeiler (<strong>Universität</strong> Stuttgart) Schedule<br />
We consider a mathematical model that describes the dynamics <strong>of</strong> compressible fluids which can<br />
occur in a liquid and a vapour phase. Therein, the phase boundary is represented as a sharp,<br />
shock-like interface. While for hydrodynamical shock waves it suffices to satisfy the homogeneous<br />
Rankine-Hugoniot conditions and to control the sign <strong>of</strong> the entropy condition, more delicate conditions<br />
characterise phase transitions: algebraic conditions to specify the correct amount <strong>of</strong> entropy<br />
dissipations and differential conditions like the Young-Laplace law, which take into account curvature<br />
effects. An essential numerical difficulty is the correct treatment <strong>of</strong> these conditions and<br />
to overcome the difficulties posed by a mixed type model.<br />
In our approach we separate the problem in two scales: with microscale models we treat the<br />
fluid dynamics at phase boundaries and with macroscale models the behaviour in bulk phases.<br />
Both scales are coupled with a ghost fluid approach.<br />
We present a microscale solver based on a generalisation <strong>of</strong> the classical Riemann problem to<br />
two-phase fluids. The phase transition is modelled as a discontinuous wave and effects <strong>of</strong> surface<br />
tension are included via the curvature <strong>of</strong> the phase boundary.<br />
The macroscale domain is divided in time dependent liquid and vapour domains and we use<br />
standard fluid solvers for the single phase areas. More complicated is the correct treatment <strong>of</strong> the<br />
interface. Detailed informations are present via the microscale solution and will applied here. In<br />
particular we drive the interface with informations <strong>of</strong> the microscale solution.<br />
Numerical solutions for multi-dimensional test settings display good accordance with the physical<br />
behaviour <strong>of</strong> bubbles and droplets.<br />
Bubble interaction during boiling process<br />
E.O. Didinska (Oles Honchar Dnipropetrovsk National University) Schedule<br />
Nevertheless a lot <strong>of</strong> new energetic technologies, boiling remain the most wide-spread and correspondingly<br />
important process for transformation <strong>of</strong> thermal energy into electricity. Nevertheless<br />
intensive investigation stimulated by importance <strong>of</strong> boiling study during enough long time, our<br />
understanding <strong>of</strong> boiling process from the physical point <strong>of</strong> view and especially in mathematical<br />
modeling is very far from satisfactory. The most complicated among variety <strong>of</strong> effects concerning<br />
boiling process is, <strong>of</strong> course, bubble growth on a heater surface. There exist several physical and<br />
correspondingly mathematical models <strong>of</strong> the last process; however neither boiling crises, nor separation<br />
<strong>of</strong> bubble can be properly calculated in any model. We propose to develop a series <strong>of</strong><br />
extremely simplified mathematical models, every <strong>of</strong> which describes one separate specific feature<br />
<strong>of</strong> boiling process. In particular, thermal interaction <strong>of</strong> bubbles growing on the heater surface is<br />
main object <strong>of</strong> the present work. Mathematical model <strong>of</strong> slow phase transition and homothetic<br />
growth are applied to the considered problems. Asymptotic model <strong>of</strong> slow phase transition gives<br />
an opportunity to replace initial parabolic problem by series <strong>of</strong> elliptic boundary-value problems.<br />
Consideration in the present work is restricted by zeroth and first approximations. BEM is used<br />
for numerical calculation <strong>of</strong> temperature field on each time step. The proposed approach is illustrated<br />
by several examples <strong>of</strong> numerical calculation.<br />
Observation <strong>of</strong> mass transfer <strong>of</strong> selected organic substances in supercritical carbon<br />
dioxide by means <strong>of</strong> shearing interferometer<br />
Miao Hu, Rainer Benning, Özgür Ertunc, Antonio Delgado (<strong>Universität</strong> Erlangen-Nürnberg)<br />
Schedule<br />
The research interests lie in a deeper understanding <strong>of</strong> the mechanism <strong>of</strong> organic solutes diffusing<br />
into the near- and supercritical state <strong>of</strong> a solvent, which counts as the most basic means <strong>of</strong> mass
230 Section 11: Interfacial flows<br />
transfer in the process engineering industry, especially in extraction and particle handling processes.<br />
Supercritical carbon dioxide, with a relatively low critical pressure and temperature, and<br />
<strong>of</strong> being non-toxic is one <strong>of</strong> the most popular alternatives to the traditional organic solvents, as<br />
well known in c<strong>of</strong>fee and tea decaffeination, pharmaceutical separation, etc. With the increasing<br />
awareness <strong>of</strong> environmental aspects, its promising potential is showing in more and more areas,<br />
e.g. surface cleaning, etc. One reason for the limitations <strong>of</strong> commercial applications in industrial<br />
scales is the disadvantage that the procedures in supercritical fluids related processes are basically<br />
experience-based and fundamental knowledge <strong>of</strong> their thermodynamic behaviors are still to be<br />
gained in order to achieve a better control <strong>of</strong> the process as well as to optimize the system [1].<br />
Special attention was paid to the direct visualization <strong>of</strong> the diffusion process <strong>of</strong> oil droplets in<br />
supercritical carbon dioxide as well as the quantitative analysis <strong>of</strong> the process by evaluating the<br />
important parameter-diffusion coefficients, which were experimentally obtained with a shearing<br />
interferometer. Considering the fact that diffusion is always accompanied by undesirable densitydriven<br />
convection on earth, it is meaningful to carry out the experiments also under microgravity,<br />
where the density variations causing the convection are largely reduced and a steady diffusion<br />
process can be observed. Two parabolic flight campaigns were carried out to perform the experiments<br />
under Microgravity (March 2010, 15th German Aerospace Agency (DLR) and May 2011,<br />
54th European Space Agency (ESA)-parabolic flight campaign). The project was funded by DLR<br />
under grant No. 50WM0840.<br />
[1] Y. Arai, T. Sako, Y. Takabayashi, Supercritical Fluids, Molecular Interactions, Physical<br />
Properties and New Applications (Eds.) Springer-Verlag, Berlin und Heidelberg (2002).<br />
S11.2: Two-Phase Flow Numerics Tue, 16:00–18:00<br />
Chair: Axel Voigt S1|03–123<br />
Surface fluids - a finite element approach<br />
Axel Voigt (TU Dresden) Schedule<br />
A two-phase Newtonian surface fluid is modeled as a surface Cahn-Hilliard-Navier-Stokes equation<br />
using a stream function formulation. This allows to circumvent the subleties in describing vectorial<br />
second-order partial differential equations on curved surfaces and allows for an efficient numerical<br />
treatment using parametric finite elements. The approach is validated for various test cases,<br />
including a vortex-trapping surface demonstrating the strong interplay <strong>of</strong> the surface morphology<br />
and the flow. Finally the approach is applied to a Rayleigh-Taylor instability and coarsening<br />
scenarios on various surfaces.<br />
Modeling the surface tension force using Discontinuous Galerkin FEM<br />
N. Emamy, R. Mousavi, F. Kummer, M. Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
In this study incompressible multiphase flow including the surface tension on the phase interface<br />
is considered. Governing equations are the Navier-Stokes and continuity equations based on the<br />
one-fluid approach. The interface is represented as the zero iso-value <strong>of</strong> the level set function φ.<br />
To maintain the signed distance property <strong>of</strong> the level set function a re-initialization equation is<br />
solved. The surface tension force is modeled using the continuum surface force (CSF) model [1]<br />
in the form<br />
�FS = σδ(φ)κ�n, (1)
Section 11: Interfacial flows 231<br />
where σ is the fluid surface tension, δ dirac delta function, κ surface curvature and �n is normal<br />
vector to the interface. The mentioned equations are solved using BoSSS [2] libraries, a general<br />
framework for solving conservation laws with the discontinuous Galerkin Finite Element method<br />
(DG-FEM). The surface tension term is calculated by using high degree polynomials for a precise<br />
calculation <strong>of</strong> the normal vector and curvature. As a numerical test case a stationary droplet with<br />
a surface tension induced inside to outside pressure difference is considered. Numerical results for<br />
the normal vector and curvature are in good agreement with analytic values.<br />
[1] J. U. Brackbill, D. B. Kothe, C. Zemach, A continuum method for modeling surface tension,<br />
J. Comput. Phys., 100, 335–354, 1992.<br />
[2] F. Kummer, The BoSSS Discontinuous Galerkin solver for incompressible fluid dynamics<br />
and an extension to singular equations, 2011, PhD dissertation, <strong>Darmstadt</strong> University <strong>of</strong><br />
Technology.<br />
Numerical integration and interface resolution for extended Discontinuous Galerkin<br />
Methods<br />
Björn Müller, Martin Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
For the simulation <strong>of</strong> multi-phase flows consisting <strong>of</strong> compressible fluids separated by a sharp<br />
interface, the classical Ghost Fluid Method [1] is widely-used. Even though it has originally been<br />
described in the context <strong>of</strong> Finite Difference schemes, an extension to the Discontinuous Galerkin<br />
Method (DGM) is straightforward [2]. This approach does not, however, exploit the full potential<br />
<strong>of</strong>fered by the DGM since the available sub-cell information in interface-cells is essentially lost.<br />
We thus propose a new method for the treatment <strong>of</strong> the interface which is able to retain this<br />
information.<br />
Our method employs a high order DGM for the advection <strong>of</strong> the level set function Φ that<br />
defines the interface I via the relation I = {�x ∈ Ω|Φ = 0}. This function can be used to enrich<br />
the polynomial basis in all cells with points in I. By means <strong>of</strong> such an extended Discontinuous<br />
Galerkin scheme, we gain an interface-conforming, piecewise polynomial representation <strong>of</strong> the<br />
solution without the need for re-meshing.<br />
Two main issues have to be resolved in order to make this approach practicable. First, we<br />
need a fast and accurate method to integrate over the curved sub-volumes without knowing I<br />
explicitly. We compared existing techniques based on the regularization <strong>of</strong> discontinuous/singular<br />
integrands [3] to methods based on adaptive subdivisions <strong>of</strong> the cell. Second, the degrees <strong>of</strong><br />
freedom associated with the local enrichments have to be resolved. Here, we will discuss the<br />
advantages and disadvantages <strong>of</strong> methods based on the direct enforcement <strong>of</strong> jump conditions,<br />
cell splitting/merging [4] and the GFM [2].<br />
[1] R. P. Fedkiw, T. Aslam, B. Merriman, S. Osher, A non-oscillatory Eulerian approach to<br />
interfaces in multimaterial flows (the Ghost Fluid Method), J. Comput. Phys. 152 (1999)<br />
[2] J. Qiu, T. Liu, B. C. Khoo, Simulations <strong>of</strong> compressible two-medium flow by Runge-Kutta<br />
Discontinuous Galerkin Methods with the Ghost Fluid Method, Commun. Comput. Phys.<br />
3 (2008)<br />
[3] A.-K. Tornberg, Multi-dimensional quadrature <strong>of</strong> singular and discontinuous functions, BIT<br />
42 (2002)
232 Section 11: Interfacial flows<br />
[4] J. Qiu, T. Liu, B. C. Khoo, Runge-Kutta Discontinuous Galerkin Methods for compressible<br />
two-medium flow simulations: One-dimensional case, J. Comput. Phys. 222 (2007)<br />
A Navier-Stokes solver based on a discontinuous Galerkin FEM, coupled with a level<br />
set interface tracker<br />
R. Mousavi, N. Emamy, F. Kummer, M. Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
A single fluid approach for modeling the multi-phase flows is followed by solving the multi-phase<br />
form <strong>of</strong> the Navier-Stokes equation. The surface tension and gravity effects are not considered. A<br />
velocity projection algorithm is applied to solve the the momentum equation accompanying the<br />
continuity equation. A modal discontinuous Galerkin finite element method is used for the spatial<br />
discretization. The density and viscosity distributions are obtained by tracking the interface as<br />
the zero iso-value <strong>of</strong> a level set function. It is done by solving the level set advection equation.<br />
As the interface is considered with a finite thickness requiring the signed distance property <strong>of</strong> the<br />
level set function, the level set re-initialization equation is also solved in a pseudo time-stepping<br />
sense. Considering the re-initialization equation as a Hamilton - Jacobi equation, the Hamiltonian<br />
term is numerically approximated using a Godunov’s method. The in-house solver BoSSS is used<br />
for all <strong>of</strong> the numerical calculations [1].<br />
[1] F. Kummer, The BoSSS Discontinuous Galerkin solver for incompressible fluid dynamics<br />
and an extension to singular equations, 2011, PhD dissertation, <strong>Darmstadt</strong> University <strong>of</strong><br />
Technology<br />
A discontinuous Galerkin based multiscale method for compressible multiphase flow<br />
F. Jaegle, M. Boger, S. Fechter, C.-D. Munz (<strong>Universität</strong> Stuttgart) Schedule<br />
The numerical simulation <strong>of</strong> compressible multiphase flow introduces additional difficulties compared<br />
to the incompressible treatment that is <strong>of</strong>ten found in two-phase numerical solvers today.<br />
Two elements are crucial: A method that allows to define the geometry and the temporal evolution<br />
<strong>of</strong> the interface between the two phases (level-set in this study) as well as a numerical strategy<br />
to treat the discontinuous nature <strong>of</strong> the interface as well as the related physics such as impinging<br />
waves, phase change or surface tension. We use a sharp interface multiscale approach, where the<br />
numerical scheme only resolves the macroscopic scales <strong>of</strong> the flow and allows discontinuous states<br />
at the interface position, where jump conditions have to be provided by an additional solver<br />
for the micro-scale. Many micro-scale solvers are conceivable, in the present study, we rely on<br />
Riemann-type solvers. The approach is suitable for general EOS.<br />
The macro-scale solver for the bulk phases <strong>of</strong> the flow uses a discontinuous Galerkin spectral<br />
element method, formulated for hexahedral elements. As no continuity constraint is enforced between<br />
the elements, the flux function at cell boundaries is replaced by a numerical flux. In the bulk<br />
phases, standard Riemann solvers are used. Near the phase interface, the jump in fluid quantities<br />
is assumed to coincide with the nearest element boundary, where the Riemann solver is replaced<br />
by the microscale solver. Instead <strong>of</strong> evaluating a single numerical flux, the microscale solver provides<br />
discontinuous fluxes, which are applied on the liquid and gaseous side respectively.<br />
The scheme allows high orders <strong>of</strong> accuracy with subcell resolution, which is particularly valuable<br />
for the calculation <strong>of</strong> interface curvature that can be obtained from derivation <strong>of</strong> the ansatz polynomials<br />
for the level-set variable. The model for surface tension is included in the microscale<br />
solution and takes effect in the macroscale via the numerical fluxes, thereby eliminating the need
Section 11: Interfacial flows 233<br />
for source terms to apply the surface force.<br />
Test cases considered include steady and unsteady droplets and bubbles with surface tension and<br />
phase change as well as shock droplet interaction without phase change.<br />
On the coupling <strong>of</strong> compressible and incompressible flow regions<br />
Markus Boger, Felix Jaegle (<strong>Universität</strong> Stuttgart), Rupert Klein (FU Berlin), Claus-Dieter Munz<br />
(<strong>Universität</strong> Stuttgart) Schedule<br />
In many cases, multiphase flows are simulated on the basis <strong>of</strong> the incompressible Navier-Stokes<br />
equations. This assumption is valid as long as the density changes in the gas phase can be neglected.<br />
Yet, for certain technical applications like fuel injection this is no longer the case and at<br />
least the gaseous phase has to be treated as a compressible fluid.<br />
In the present study, we present two different ways <strong>of</strong> coupling an incompressible flow region to<br />
a compressible one. Therefore, the one-dimensional Euler equations are used for fully compressible<br />
flows and in the case <strong>of</strong> their incompressible limit (vanishing Mach number limit). The first<br />
approach is based on the coupling <strong>of</strong> the thermodynamic pressure in the zero Mach number limit<br />
to the pressure <strong>of</strong> the compressible flow region. Hence, the primary variable for this iterative<br />
procedure is the pressure. The second coupling procedure only takes into account the effects <strong>of</strong><br />
the hydrodynamic pressure. In this case, the iteration is performed with the velocity as primary<br />
variable. In both cases, a half Riemann problem is solved at the interface. It consists <strong>of</strong> a shock<br />
or expansion wave in the compressible region and a contact discontinuity that represents the<br />
boundary between the compressible and the incompressible region.<br />
The coupling schemes are implemented in a one-dimensional simulation framework using a<br />
discontinuous Galerkin (DG) scheme with a sharp interface ghost-fluid type method for the coupling<br />
at the material interface. While the compressible flow domain is discretized with the DG<br />
scheme, the incompressible subdomain is solved analytically. As an alternative, the interaction<br />
between a compressible and a weakly compressible region can also be analysed using the ghostfluid<br />
approach <strong>of</strong> the simulation framework. In this case, both flow regions are described by the<br />
compressible Euler equations and incompressibility is approached by increasing the speed <strong>of</strong> sound<br />
in the weakly compressible region.<br />
Two different test cases are presented to assess the coupling procedures. The first example<br />
describes the pure compression <strong>of</strong> a liquid region. In the second case, the effects <strong>of</strong> hydrodynamics<br />
are considered and the liquid region is accelerated due to a pressure gradient. The obtained<br />
results are compared to simulations performed with the ghost fluid type scheme. We achieve a<br />
good agreement between the iterative coupling procedures and the ghost fluid type scheme.<br />
Linearly implicit time discretization for free surface problems<br />
Stephan Weller, Eberhard Bänsch (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
Time discretization for free surface problems is a widely neglected problem. Many existing approaches<br />
use an explicit decoupling which is only conditionally stable. Only few unconditionally<br />
stable methods are known, and known methods may suffer from too strong numerical dissipativity.<br />
They are also usually <strong>of</strong> first order only [1]. We are therefore looking for unconditionally<br />
stable, minimally dissipative methods <strong>of</strong> higher order.<br />
Linearly implicit Runge-Kutta (LIRK) methods are a class <strong>of</strong> one-step methods that require<br />
the solution <strong>of</strong> linear systems in each time step <strong>of</strong> a nonlinear system. They are well suited<br />
for discretized PDEs, e.g. parabolic problems [2]. They have been used successfully to solve the<br />
incompressible Navier-Stokes equations [3]. We suggest an adaption <strong>of</strong> these methods for free<br />
surface problems and compare different approximations to the Jacobian matrix needed for such<br />
methods.
234 Section 11: Interfacial flows<br />
We compare the approach with existing fully implicit approaches, which require similar solution<br />
techniques but are usually more expensive.<br />
A numerical realization <strong>of</strong> the method using a moving mesh finite element discretization will<br />
be presented. Extensions to more complex approaches (e.g. interface reconstruction methods like<br />
levelset or volume <strong>of</strong> fluid) will be discussed.<br />
[1] Bänsch, Eberhard (1998). „Numerical methods for the instationary Navier–Stokes equations<br />
with a free capillary surface“. Habilitationsschrift. <strong>Universität</strong> Freiburg.<br />
[2] Lubich, Ch. and A. Ostermann (1995). „Linearly implicit time discretization <strong>of</strong> nonlinear<br />
parabolic equations“. In: IMA Journal Num. Anal. 15(4), pp. 555–583.<br />
[3] Lang, Jens and I. Teleaga (2008). „Higher–order linearly implicit one–step methods for threedimensional<br />
incompressible Navier–Stokes equations“. In: Studia Univ. „Babes–Bolyai“, Mathematica<br />
LIII.1.<br />
S11.3: Computational Fluid Dynamics Wed, 13:30–15:30<br />
Chair: Bernhard Weigand S1|03–123<br />
On Compressible Extension <strong>of</strong> VOF Method Using Low-Mach Assumptions for Capturing<br />
Near Critical Behavior<br />
Illya Shevchuk, Amsini Sadiki, Johannes Janicka (TU <strong>Darmstadt</strong>) Schedule<br />
Due to continuous efficiency enhancement <strong>of</strong> technical combustion systems operating with liquid<br />
fuels in carrier gas environment, such as combustion chambers <strong>of</strong> aircraft engines and diesel<br />
engines, temperature, pressure or both these state quantities reach the vicinity <strong>of</strong> critical values<br />
<strong>of</strong> used liquids or can even exceed them. Understanding and simulative reproduction <strong>of</strong> droplet<br />
dynamics under these extreme conditions is essential for improvement <strong>of</strong> technical systems.<br />
The characteristics <strong>of</strong> the liquid and gas behavior in the vicinity <strong>of</strong> the critical point have<br />
strong dependence <strong>of</strong> their properties on temperature and pressure. Thus, assumptions <strong>of</strong> constant<br />
density, viscosity, heat conductivity etc. typically made in multiphase simulations cannot be made<br />
for these problems. The scope <strong>of</strong> the endeavor is to create a solver capable to capture major near<br />
critical phenomena for investigation <strong>of</strong> single droplets and droplet groups.<br />
In this contribution we present an approach to extend the existing incompressible solver from<br />
the OpenFOAM R○ toolbox in order to treat compressible flows and variable material properties.<br />
Focus is first put on low Mach number flows with constant mean pressure but steep temperature<br />
gradients. For that purpose, the governing equations for mass, momentum and enthalpy in conservative<br />
form are considered. Additionally a volume <strong>of</strong> fluid based method is used to capture the<br />
position <strong>of</strong> the gas-liquid interface. Thereby severe assumptions are made to reduce the complexity,<br />
e.g. heat production by viscous friction as well as heat transfer by radiation is neglected.<br />
Further, the dependency <strong>of</strong> fluid properties on pressure is neglected while the dependency on<br />
temperature is taken into account. The governing equations are discretized using finite volume<br />
method on unstructured meshes and solved using segregated solution procedure.<br />
To validate the modified solver, simulations <strong>of</strong> a natural convection driven single phase cavity<br />
flow characterized by high Rayleigh numbers with perfect gas conditions were carried out and<br />
compared to reference simulations found in literature [1]. Good agreement between the results<br />
achieved and the reference calculations was established with a mean Nusselt number deviation<br />
from the reference solution less than 3% (Nuref = 8.86 vs. Nusim = 8.61). A two-phase test
Section 11: Interfacial flows 235<br />
case (droplet <strong>of</strong> acetone in nitrogen environment) is being investigated where the thermodynamic<br />
droplet properties are described by Peng-Robinson equation <strong>of</strong> state. Preliminary results will be<br />
included in the final version.<br />
[1] P. Le Quéré et al., Modelling <strong>of</strong> natural convection flows with large temperature differences:<br />
a benchmark problem for low Mach number solvers. Part 1. Reference Solutions, ESAIM:<br />
M2AN 39 (2005), 609 – 616.<br />
The Extended Discontinuous Galerkin discretization <strong>of</strong> singular equations.<br />
Florian Kummer (TU <strong>Darmstadt</strong>) Schedule<br />
In multiphase flow problems, the solutions for velocity and pressure usually contain jumps<br />
and kinks. Indeed, for material interfaces, the introduction <strong>of</strong> surface tension models will induce a<br />
jump in the pressure field, while the velocity field will contain a kink. Solutions for non-material<br />
interfaces contain jumps in velocity and pressure field, even without any surface tension models.<br />
Since the derivatives <strong>of</strong> these – discontinuous – solutions are singular, i.e. Delta - distributions,<br />
we call the partial differential equations “singular”.<br />
For the computational domain Ω ⊂ R D the disjoint decomposition Ω = A ∪ I ∪ B is given,<br />
where I is an (D − 1) - dimensional interface that separates the phases A and B. On I, for<br />
some property u that is discontinuous at the interface, one defines the jump operator [u] as the<br />
difference between the value <strong>of</strong> u on B- and A - side. Given that, a discontinuous problem is e.g.<br />
the Poisson equation ⎧ ⎨<br />
⎩<br />
div(ν∇u) = f in Ω \ I<br />
[α1 u] = g1, [α2 ∇u · �n] = g2 on I<br />
Dirichlet or Neumann b.c. on ∂Ω<br />
Note that g1, g2, α1 and α2 are assumed to be non-constant and that especially [α1 ] �= 0 and also<br />
[α2 ] �= 0.<br />
The numerical treatment <strong>of</strong> discontinuities at the interface is considered to be challenging;<br />
basically two options are available: either, the jumps and kinks are regularised (‘smeared out’) or<br />
a special numerical discretisation which is capable <strong>of</strong> representing jumps and kinks is used. We<br />
will present an Extended Discontinuous Galerkin (XDG) method that is able to represent jumps<br />
mentioned above with sub-cell accuracy. In some “normal” computational cell, some field f(�x) is,<br />
as usually in Discontinuous Galerkin (DG), approximated as a series fh(�x) = �N n=1 φn(�x) · ˜ fn,<br />
where the polynomials φn are called the DG basis. In a “cut” cell K (i.e. I ∩ K �= ∅) these basis<br />
polynomials are multiplied by the characteristic functions χA and χB yielding separate degrees<strong>of</strong>-freedom<br />
for both phases, i.e.<br />
fh(�x) =<br />
N�<br />
n=1<br />
�<br />
φn(�x) · χA · ˜ fA,n + φn(�x) · χB · ˜ �<br />
fB,n . (2)<br />
The work that is going to be presented will discuss the computation <strong>of</strong> the additional degrees-<strong>of</strong>freedom<br />
in the XDG-Ansatz for linear boundary value problems like like the one given above.<br />
Numerical study <strong>of</strong> a liquid/liquid slug flow in a rectangular microreactor<br />
Ina Dittmar, Peter Ehrhard (TU Dortmund) Schedule<br />
The great advantages <strong>of</strong> microreactors are associated with an extremely–high surface–to–volume<br />
ratio. Hence, microreactors permit promising operating conditions, such as almost–perfect heat<br />
(1)
236 Section 11: Interfacial flows<br />
or mass transfer. The hydrodynamics <strong>of</strong> a liquid/liquid slug flow in a rectangular micro–channel<br />
is characterized by a complex vortex structure in both the disperse and the continuous phase.<br />
The disperse phase, in our investigations, is not wetting the walls and, thus, a thin film <strong>of</strong> the<br />
continuous phase persist between the disperse phase and the wall. Due to this phenomenon, a<br />
relative movement between disperse and continuous phase is possible and, indeed, observed. Understanding<br />
<strong>of</strong> these complex phenomena allows for a control <strong>of</strong> the hydrodynamics, and thus,<br />
to tailor the heat and mass transport in a desired manner. To study the physics <strong>of</strong> this complex<br />
two–liquid system, a modified level–set method in conjunction with an immersed–boundary formulation<br />
is engaged. Presently, the simulations are time-dependent and fully three-dimensional<br />
in nature. The mesh resolution represents a challenge, as the spatial resolution has to resolve the<br />
thin film between the disperse phase and the wall adequately. Different approaches to solve this<br />
challenge are presented. All simulations are implemented within the s<strong>of</strong>tware OpenFOAM.<br />
A numerical investigation on the fluid flow at the interface <strong>of</strong> a porous and a free<br />
flow domain<br />
Timo Reisner, Holger Steeb, Joerg Renner (<strong>Universität</strong> Bochum) Schedule<br />
Approaches in sediment transport modeling can be roughly subdivided into two categories: 1)<br />
Models based on the theory <strong>of</strong> mixtures using a macroscopic, volumetrically-coupled two-phase<br />
(fluid and sediment) continuum approach and 2) interface-coupled, i.e. staggered approaches assuming<br />
a rigid boundary at the sediment bed, calculating the shear stresses at the bed surface, in<br />
combination with an algebraic relation to calculate the sediment transport and in the last step,<br />
the change in morphology.<br />
Neither <strong>of</strong> these approaches takes into account the (Darcy / Brinkman) flow inside the sediment<br />
bed and how the different physics <strong>of</strong> the flow patterns influence each other. Hence we have<br />
developed a sediment transport model based on a three-phase mixture, which takes into account<br />
the notion that the porous sediment bed and the mobilized particles (commonly termed bed load)<br />
show distinctly different physical behaviours: The sediment bed can be described as a (more or<br />
less) rigid porous medium, while the mobilized particles exhibit a fluid-like behaviour.<br />
Here, we concentrate on a numerical investigation <strong>of</strong> the fluid flow at the interface between a<br />
porous medium and a free flow domain using a range <strong>of</strong> different coupling mechanisms between<br />
the equations governing the free (Navier-Stokes) and the porous medium (Brinkman) flows in<br />
order to examine the interaction mechanisms between both domains. The goal <strong>of</strong> this study is<br />
to answer the following questions: 1) How is the fluid flow in the porous domain influenced by<br />
the flow in the free flow domain, and, conversely, what is the influence <strong>of</strong> the porous domain on<br />
the free flow, and 2) Do these effects have a stabilizing or a destabilizing effect, i.e. are there<br />
any forces induced by the interdependence <strong>of</strong> the flow patterns in the two different domains that<br />
would lead to enhanced sediment erosion or deposition at the interface?<br />
The current implementation is based on the FE-Code Comsol Multiphysics. For the Navier-<br />
Stokes and Brinkman equations, common and widely-used stabilization schemes are applied for<br />
numerical stability. To work out the interfacial effects, we numerically analyse three different geometries<br />
each containing a free flow and a porous domain.<br />
Numerical Study <strong>of</strong> the Primary Breakup <strong>of</strong> Plane Liquid Sheet with Co-flowing Air<br />
Streams<br />
K. Suresh Kumar, B. Peters (<strong>Universität</strong> Luxemburg) Schedule<br />
The disintegration <strong>of</strong> a plane liquid sheet with co-flowing air streams is studied numerically using<br />
the quasi-DNS/LES-Volume <strong>of</strong> Fluid (VOF) multiphase flow approach. The liquid-gas interface<br />
is tracked using the interface compression scheme. A one equation eddy viscosity model has been
Section 11: Interfacial flows 237<br />
used to resolve the sub-grid scale stresses, which solves a transport equation for sub-grid scale<br />
kinetic energy. This numerical investigation is focused on demonstrating the capability <strong>of</strong> quasi-<br />
DNS/LES-VOF approach to predict the highly complex primary breakup phenomena <strong>of</strong> liquid<br />
sheet interacting with co-flowing air streams. As a first step the plane liquid sheet is modeled<br />
using a two dimensional (2D) approximation. The effect <strong>of</strong> mesh refinement on the breakup length<br />
and breakup characteristics is studied for the 2D case. Finally a three dimensional simulation <strong>of</strong><br />
the plane liquid sheet with co-flowing air streams is performed and results are compared with<br />
published experimental results for breakup length.<br />
Two-Phase Flow in Single-Screw Extruders<br />
Martin Lübke, Olaf Wünsch (<strong>Universität</strong> Kassel) Schedule<br />
In polymer processing industry extruders are used to perform functions such as melting, conveying<br />
and devolatization. In the process <strong>of</strong> devolatization the detection <strong>of</strong> the free-surface is<br />
important due to the fact that the degassing performance depends on the interfacial area. This<br />
study concerns numerical simulation <strong>of</strong> free-surface flows <strong>of</strong> highly viscous liquids in single-screw<br />
extruders. The numerical treatment <strong>of</strong> a partially filled extruder is a challenging task due to the<br />
complex geometry and the large differences in density and viscosity between the two phases, e.g.<br />
polymer melt and air. Furthermore, the rotation <strong>of</strong> the screw leads to a continuous renewing <strong>of</strong><br />
the free-surface. For this purpose an Euler-Euler two-fluid Volume <strong>of</strong> Fluid Method (VOF) within<br />
the open source framework OpenFOAM is used. First, a simplified two-dimensional model <strong>of</strong> a<br />
single-screw extruder consisting <strong>of</strong> a rotating cylindrical barrel and a fixed internal plate is considered.<br />
Different flow phenomena, including the forming <strong>of</strong> an interface cusp, can be observed.<br />
The resulting flow and the shape <strong>of</strong> the phase interface are compared against the experiments<br />
by [1]. Good agreement is obtained between the numerical and experimental results. Finally, the<br />
three dimensional flow in a partially filled single-screw extruder with dynamic mesh motion is<br />
presented. In addition the power characteristics <strong>of</strong> a conveying screw element with varying degree<br />
<strong>of</strong> filling is discussed.<br />
[1] G. Böhme, G. Pokriefke, A. Müller, Viscous flow phenomena in a partially filled rotor-stator<br />
system, Arch App Mech vol. 75 (2006), 619 – 634.<br />
S11.4: Capillary Flows Wed, 16:00–18:00<br />
Chair: Dieter Bothe S1|03–123<br />
Temperature effects in thin droplets<br />
K. Boettcher, P. Ehrhard (TU Dortmund) Schedule<br />
In this presentation we present the spreading <strong>of</strong> a thin droplet on a plane solid, which may<br />
be driven by gravity, centrifugal forces, and dynamic wetting. Viscous heating or an imposed<br />
temperature <strong>of</strong> the solid lead to a inhomogeneous temperature field in the liquid. This may affect<br />
several properties <strong>of</strong> a liquid, like free surface tension, viscosity or density.<br />
It is well known, that temperature-dependent surface tension leads to Marangoni stresses<br />
and convection cells in the liquid. The role <strong>of</strong> a temperature-dependent viscosity, though, has<br />
neither been investigated experimentally nor theoretically. Because spreading flows are governed<br />
by a Reynolds number Re ≪ 1, these flows are dominated by friction and the influence <strong>of</strong> a<br />
temperature-dependent viscosity should be important.<br />
Based on a lubrication approximation for droplets with a small contact angle, the conservation<br />
laws may be transformed in one single evolution equation by using all boundary conditions at
238 Section 11: Interfacial flows<br />
the interfaces. The influence <strong>of</strong> a temperature field on the velocity field and on the spreading rate<br />
<strong>of</strong> a thin droplet is investigated. The spreading is modeled by the empiric law <strong>of</strong> Tanner, which<br />
couples the speed <strong>of</strong> the contact line with a macroscopic contact angle, observable in experiments.<br />
Direct numerical simulation <strong>of</strong> thermocapillary two-phase flows using the VOF method<br />
and a 2-scalar approach for heat transfer<br />
Chen Ma, Dieter Bothe (TU <strong>Darmstadt</strong>) Schedule<br />
The thermal Marangoni effect can be used as an efficient way <strong>of</strong> enhancing heat and mass transfer<br />
in two phase flows. Due to the complex interaction with different phenomena like instability<br />
or film rupture, a direct numerical simulation <strong>of</strong> thermocapillary flows with a dynamically deformable<br />
interface is <strong>of</strong>ten desired. This contribution presents a method for DNS <strong>of</strong> the above<br />
mentioned thermocapillary flows. A continuum mechanical sharp interface model for incompressible<br />
two-phase flow is employed containing the two-phase continuity, Navier-Stokes and energy<br />
equations with suitably formulated jump conditions at the phase interface. For the numerical<br />
solution with the finite volumes scheme a one-field formulation <strong>of</strong> the two-phase model is applied<br />
based on spatial averaging <strong>of</strong> the equations. A rigorous separation <strong>of</strong> the different velocities due<br />
to phase change is derived. The fluid interface is captured using an extended Volume <strong>of</strong> fluid<br />
(VOF) method with additional piecewise linear interface reconstruction (PLIC). For a high accuracy<br />
<strong>of</strong> the numerical computation <strong>of</strong> Marangoni forces, which is essential for the simulation<br />
<strong>of</strong> thermocapillary flow, the modeling <strong>of</strong> interfacial heat transfer employs a two-scalar ghost-fluid<br />
approach, where the temperatures <strong>of</strong> the two phases are represented by two sharp temperature<br />
fields, i.e. without averaging. Validation on two-phase heat conduction shows very good results<br />
compared to analytical solution. Two applications in 3D are studied using the 2-scalar approach:<br />
the heat transfer enhencement in a liquid film on structured substrate due to Marangoni effect<br />
as well as the thermocapillary flow in locally heated liquid films. The method shows potential in<br />
simulating realistic thermocapillary flows with a dynamically deformable interface combined with<br />
evaporation.<br />
Integral analysis <strong>of</strong> the flow dynamics and mass transfer in a wavy liquid film on a<br />
spinning disk<br />
Doris Prieling, Helfried Steiner, Günter Brenn (TU Graz) Schedule<br />
Wet chemical etching <strong>of</strong> silicon wafers is an important process in the semiconductor device fabrication.<br />
The aqueous etchant is supplied through a vertical jet impinging onto the rotating<br />
wafer. Driven by centrifugal forces, a thin liquid film is formed, which exhibits non-linear surface<br />
waves. The etching process is mainly controlled by the convection dominated mass transfer <strong>of</strong><br />
the primary etchant component from the bulk liquid to the wafer surface. The combination <strong>of</strong> a<br />
thin boundary layer with steep concentration gradients and the strong disparity between the two<br />
governing length scales leads to excessively high computational costs <strong>of</strong> a fully resolved numerical<br />
simulation <strong>of</strong> the flow, especially in the wavy region. The present work applies a thin film approximation<br />
combined with the von Kármán-Pohlhausen method as a computationally efficient<br />
alternative approach for the description <strong>of</strong> the flow. This integral method was successfully used<br />
by Matar et al. [1] to analyze the gas absorption into a thin film flow on a spinning disk. The<br />
purpose <strong>of</strong> the present work is to analyze in particular the effect <strong>of</strong> the surface waves on the mass<br />
transfer characteristics from the liquid into the disk wall. The obtained results reproduce very<br />
well the etching behavior observed in experiments reported by Staudegger et al. [2]. In the waveless,<br />
radially inner region, the etching activity is determined by the growth <strong>of</strong> the concentration<br />
boundary layer. Radially further downstream, irregular large amplitude waves accompanied by
Section 11: Interfacial flows 239<br />
capillary ripples, distort the surface. In the troughs <strong>of</strong> the waves the etching rate is controlled by<br />
the decrease <strong>of</strong> the film height and the abundance <strong>of</strong> etchant component in the bulk liquid. In the<br />
regions around the wave crests the etching rate is controlled by the thickness <strong>of</strong> the concentration<br />
boundary layer. The observed enhancement <strong>of</strong> the mass transfer in the wavy region can be mainly<br />
attributed to the local thinning <strong>of</strong> the film. The analysis <strong>of</strong> the results makes it evident that the<br />
integral method is capable to describe the mass transfer towards the wall realistically, also in a<br />
film regime with a highly irregular surface.<br />
[1] O. K. Matar, C. J. Lawrence, G. M. Sisoev, The flow <strong>of</strong> thin liquid films over spinning disks:<br />
Hydrodynamics and mass transfer, Phys. Fluids 17 (2005), 052102<br />
[2] F. Staudegger, M. W. H<strong>of</strong>baur, and H.-J. Kruwinus, Analyses and modeling <strong>of</strong> a wet-chemicaletch<br />
process on rotating silicon wafers with an impinging etchant jet, J. Electrochem. Soc.<br />
156 (2009), 340–345<br />
Capillary transport between perforated plates under microgravity<br />
Diana Gaulke, Michael E. Dreyer (<strong>Universität</strong> Bremen) Schedule<br />
Propellant management devices are used to supply thrusters with gas free propellant. Therefore,<br />
these devices have to be able to store a minimal amount <strong>of</strong> propellant during the ballistic phase.<br />
This amount has to be sufficient for the chill down phase and the pre-acceleration for settling the<br />
liquid in the tank. Normally, propellant acquisition takes place by means <strong>of</strong> capillary forces. This<br />
includes modules for leading and holding the liquid.<br />
In the thrusting phase these modules have a negative influence. They induce a higher pressure<br />
loss in the propellant feeding system. Some parts are made out <strong>of</strong> perforated plates to reduce this<br />
pressure loss. Such perforations influence the capillary transport and change the flow pattern.<br />
In this talk, the application <strong>of</strong> perforated plates to propellant management devices is introduced.<br />
An experimental study is presented to understand the influence <strong>of</strong> the perforations. Capillary<br />
transport between parallel plates is analyzed and influence <strong>of</strong> certain macroscopic properties <strong>of</strong><br />
perforations is presented.<br />
Stability limits <strong>of</strong> unsteady capillary channel flow: experiments on the International<br />
Space Station (ISS)<br />
P.M.Bronowicki, A.Grah, P.Canfield, M.Dreyer (<strong>Universität</strong> Bremen) Schedule<br />
The main subjects <strong>of</strong> this work are numerical and experimental studies on capillary channel flow<br />
in a compensated gravitational environment. Capillary forces are used in fluid management systems<br />
to acquire the liquid and preserve a continuous, bubble- free path between two variable<br />
points e.g., in surface tension tanks between fuel pool and outlet to the thruster.<br />
The capillary channels considered in this work consist <strong>of</strong> glass plates with several geometric<br />
configurations i.e., parallel plates, groove and wedge. For every configuration at least one channel<br />
side remains open what results in a creation <strong>of</strong> the free surface between the liquid phase and the<br />
ambient gas phase. The maximal flow rate is achieved when the pressure difference between the<br />
liquid and gas phase is no longer balanced by the curvature <strong>of</strong> the free surface and the free surface<br />
collapses. This leads to gas ingestion into the flow path, a phenomenon known as choking, which<br />
may cause technical disadvantages. The critical flow rate depends on the channel geometry, the<br />
liquid properties and the flow regime.<br />
Prior to the experiments on the ISS, extensive research on capillary channel flows was performed.<br />
One-dimensional and three-dimensional models were developed to study the unsteady<br />
flow behavior. The one-dimensional model is based on the unsteady Bernoulli and the continuity
240 Section 11: Interfacial flows<br />
equations. Critical steady flow rates were accurately predicted with one- and three-dimensional<br />
computations. A theory for steady and transient surface stability was developed. A transient<br />
stability constant, influenced by the system feedback effect, is observed and explained.<br />
In 2011, series <strong>of</strong> experiments were performed on board <strong>of</strong> International Space Station to<br />
study the capillary channel flows and verify the stability theory for steady and transient flows.<br />
The experiment was controlled via telecommands from a Ground Station in Bremen (Germany).<br />
Different geometric configurations and flow regimes were investigated. References: Grah et al.,<br />
Phys. Fluids 22 (2010) Rosendahl et al., Phys. Fluids 22 (2010) Grah et al., J. Fluid Mech. 600,<br />
271289 (2008) Rosendahl et al.,J. Fluid Mech. 518, 187214 (2004)<br />
Stability limits <strong>of</strong> two-phase open capillary channel flow in a wedge<br />
Peter Canfield, Michael Dreyer, Max Bronowicki (<strong>Universität</strong> Bremen) Schedule<br />
Previous studies have shown that surface stability in steady open capillary channel flow is defined<br />
by the flow rate, the physical properties <strong>of</strong> the liquid, and the geometrical properties <strong>of</strong> the<br />
channel [1, 2]. Surface stability is a limiting factor in fluid management devices that use capillary<br />
channels to position and transport liquid. Experiments have shown that once a critical flow<br />
rate is reached the free surface <strong>of</strong> a capillary channel flow collapses and gas is ingested into<br />
the channel. This phenomenon is called ‘choking’. In an operational scenario, inclusion <strong>of</strong> gas<br />
bubbles in the liquid flow may be detrimental to the device that the liquid is being provided<br />
to. A complete understanding <strong>of</strong> the underlying physics <strong>of</strong> this phenomenon will help improve<br />
current mathematical models that are used to determine maximum flow rates for a given setup. In<br />
turn, these models may be used to improve designs for fluid management devices that implement<br />
capillary channel flow, e.g. propellant management devices that are used in space vehicles.<br />
In 2011, experiments were conducted onboard the ISS in cooperation with Portland State<br />
University and NASA to determine critical flow rates <strong>of</strong> single-phase and two-phase flow within<br />
an open capillary channel with a triangular cross-section. The results <strong>of</strong> the experiments are<br />
compared with the predictions that were determined numerically using a one-dimensional model<br />
that incorporates the determining factors <strong>of</strong> the phenomenon or using a three-dimensional CFD<br />
model based on VOF methods.<br />
[1] U. Rosendahl, A. Ohlh<strong>of</strong>f, M. E. Dreyer, and H. J. Rath, Investigation <strong>of</strong> Forced Liquid Flows<br />
in Open Capillary Channels Microgravity Sci. Technol. 13 (2002), 53 – 59<br />
[2] Aleksander Grah, Dennis Haake, Uwe Rosendahl, Joerg Klatte, and Michael Dreyer Stability<br />
limits <strong>of</strong> unsteady open capillary channel flow. J. Fluid Mech. 600 (2008), 271 – 289<br />
S11.5: Complex Interfaces and Surface PDEs Thu, 13:30–15:30<br />
Chair: Konrad Boettcher S1|03–123<br />
Modeling the surface tension force using Discontinuous Galerkin FEM<br />
N. Emamy, R. Mousavi, F. Kummer, M. Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
In this study incompressible multiphase flow including the surface tension on the phase interface<br />
is considered. Governing equations are the Navier-Stokes and continuity equations based on the<br />
one-fluid approach. The interface is represented as the zero iso-value <strong>of</strong> the level set function φ.<br />
To maintain the signed distance property <strong>of</strong> the level set function a re-initialization equation is<br />
solved. The surface tension force is modeled using the continuum surface force (CSF) model [1]
Section 11: Interfacial flows 241<br />
in the form<br />
�FS = σδ(φ)κ�n, (1)<br />
where σ is the fluid surface tension, δ dirac delta function, κ surface curvature and �n is normal<br />
vector to the interface. The mentioned equations are solved using BoSSS [2] libraries, a general<br />
framework for solving conservation laws with the discontinuous Galerkin Finite Element method<br />
(DG-FEM). The surface tension term is calculated by using high degree polynomials for a precise<br />
calculation <strong>of</strong> the normal vector and curvature. As a numerical test case a stationary droplet with<br />
a surface tension induced inside to outside pressure difference is considered. Numerical results for<br />
the normal vector and curvature are in good agreement with analytic values.<br />
[1] J. U. Brackbill, D. B. Kothe, C. Zemach, A continuum method for modeling surface tension,<br />
J. Comput. Phys., 100, 335–354, 1992.<br />
[2] F. Kummer, The BoSSS Discontinuous Galerkin solver for incompressible fluid dynamics<br />
and an extension to singular equations, 2011, PhD dissertation, <strong>Darmstadt</strong> University <strong>of</strong><br />
Technology.<br />
Surface fluids - a finite element approach<br />
Axel Voigt (TU Dresden) Schedule<br />
A two-phase Newtonian surface fluid is modeled as a surface Cahn-Hilliard-Navier-Stokes equation<br />
using a stream function formulation. This allows to circumvent the subleties in describing vectorial<br />
second-order partial differential equations on curved surfaces and allows for an efficient numerical<br />
treatment using parametric finite elements. The approach is validated for various test cases,<br />
including a vortex-trapping surface demonstrating the strong interplay <strong>of</strong> the surface morphology<br />
and the flow. Finally the approach is applied to a Rayleigh-Taylor instability and coarsening<br />
scenarios on various surfaces.<br />
Simulation <strong>of</strong> interfacial convection-diffusion equations by Discontinuous Galerkin<br />
methods and a new conservative formulation<br />
Christina Kallendorf (TU <strong>Darmstadt</strong>), Alexei F. Cheviakov (University <strong>of</strong> Saskatchewan), Martin<br />
Oberlack, Yongqi Wang (TU <strong>Darmstadt</strong>) Schedule<br />
We consider interfacial convection and convection-diffusion equations describing, for instance,<br />
the transport <strong>of</strong> surfactants in an incompressible two-phase flow. In our setting, the interface<br />
is presented implicitly by a level set formulation and all differential operators intrinsic to the<br />
interface are defined in an extrinsic manner by projection <strong>of</strong> standard differential operators onto<br />
their tangential components.<br />
Using the direct construction method, infinite families <strong>of</strong> conservation laws that essentially<br />
involve surfactant concentration are derived in both convection and convection-diffusion settings.<br />
The conserved quantity is a combination <strong>of</strong> the surfactant concentration and some metric properties<br />
<strong>of</strong> the local interface geometry. Hence, the system <strong>of</strong> governing equations, originally consisting<br />
<strong>of</strong> the surfactant transport, level set and continuity equations, can be rewritten in a fully conserved,<br />
i.e. divergence form. In consequence, the interfacial transport equation may be treated as a<br />
conservation law by the Discontinuous Galerkin method, using a convenient embedding approach<br />
based on the Eulerian grid defined in the three-dimensional domain.<br />
ALE-FEM For Two-Phase Flows With Insoluble Surfactants<br />
Andreas Hahn, Lutz Tobiska (<strong>Universität</strong> Magdeburg) Schedule
242 Section 11: Interfacial flows<br />
We present a finite element method for the flow <strong>of</strong> two immiscible incompressible fluids in two<br />
and three dimensions. Thereby the presence <strong>of</strong> surface active agents (surfactants) on the interface<br />
is allowed, which alter the surface tension.<br />
The model consists <strong>of</strong> the incompressible Navier-Stokes equations for velocity and pressure and<br />
a convection-diffusion equation on the interface for the distribution <strong>of</strong> the surfactant. A moving<br />
grid technique is applied to track the interface, on that account a Arbitrary-Lagrangian-Eulerian<br />
(ALE) formulation <strong>of</strong> the Navier-Stokes equation is used. The surface tension force is incorporated<br />
directly by making use <strong>of</strong> the Laplace-Beltrami operator technique. Furthermore, we use a finite<br />
element method for the convection-diffusion equation on the moving hyper surface. In order to get<br />
a high accurate method the interface, velocity and pressure are approximated by isoparametric<br />
finite elements.<br />
Iso-surface Computation in 3D using graph-theoretical Approach<br />
Abdulaziz Ali, Dieter Bothe (TU <strong>Darmstadt</strong>) Schedule<br />
Numerical computations <strong>of</strong> transport processes and adsorption <strong>of</strong> surfactants and their mixtures at<br />
fluidic interfaces under dynamic conditions require a connected interface representation. Common<br />
numerical approaches based on the Volume-<strong>of</strong>-Fluid (VOF) method do not provide connected<br />
interfaces. Hence, we develop a new graph-theoretical method to compute a connected interface<br />
(iso-surface) which can be applied for VOF-based numerical approaches in the context <strong>of</strong> twophase<br />
and interfacial flow computations.<br />
An iso-surface is a level set <strong>of</strong> a continuous function whose domain in 3d space is bounded.<br />
Traditionally, the Marching Cubes method [1] is applied for the computation <strong>of</strong> iso-surfaces where<br />
the domain is triangulated in cuboids. This method is not complete and hence surface connectedness<br />
is not guaranteed, although a first step in this direction is given in [2]. Furthermore,<br />
the usual combinatorical approaches lack information about surface neighbourships and surface<br />
connectedness which are crucial for surface PDE computations.<br />
We introduce a graph-theoretical method for the computation <strong>of</strong> iso-surface on which surface<br />
PDE and surface integration can be carried on. Our aim is not only the computation <strong>of</strong> this<br />
iso-surface but also the decomposition <strong>of</strong> the iso-surface into connected components. The application<br />
<strong>of</strong> surface PDE and surface integration on each component is possible. The decomposed<br />
components <strong>of</strong> the iso-surface are connected and oriented. The graph-theoretical method for the<br />
computation <strong>of</strong> iso-surface enables us to find the complete iso-surface boundaries in each cuboid.<br />
Using the boundary paths, we recover the underlying iso-surface. The appoach also includes a<br />
discrete geometrical curvature computation.<br />
[1] William E. Lorensen and Harvey E. Cline, Marching cubes: a high resolution 3d surface<br />
construction algorithm, Proceedings <strong>of</strong> the 14th annual conference on Computer graphics<br />
and interactive techniques (New York, NY, USA), SIGGRAPH ’87, ACM, 1987, pp. 163-169.<br />
[2] Jacques-Olivier Lachaud, Topologically defined isosurfaces, IN PROC. 6TH DISCRETE<br />
GEOMETRY FOR COMPUTER IMAGERY, Springer-Verlag, 1996, pp. 245-256.<br />
Direct Numerical Simulation <strong>of</strong> Multicomponent Surfactant Transport on Fluidic<br />
Interfaces<br />
Kathrin Kissling, Holger Marschall, Dieter Bothe (TU <strong>Darmstadt</strong>) Schedule<br />
In chemical industry dispersed fluid-fluid systems <strong>of</strong> immiscible phases are the basis for the synthesis<br />
<strong>of</strong> various products. The systems are usually prepared by a mixing apparatus but the process
Section 11: Interfacial flows 243<br />
can be substantially improved by adding surfactants, which will change the surface properties and<br />
allow higher dispersion rates. The influence <strong>of</strong> the surfactants on the surface tension is usually<br />
measured by drop methods, e.g., pendant or sessile drop methods. The present study focusses<br />
on the numerical simulation <strong>of</strong> these processes and especially on the surfactant transport on the<br />
fluidic interface based on the computational fluid dynamics library OpenFOAM [2] [6].<br />
Crucial features <strong>of</strong> such simulations are: a sharp interface representation, the capability <strong>of</strong><br />
topological changes <strong>of</strong> the interface and the physically correct solution <strong>of</strong> the surfactant transport<br />
equations along the interface. To model the area-based surfactant transport on the fluid interface,<br />
the finite-area method <strong>of</strong> Tukovic and Jasak [5] is applied. The interface is represented by a two<br />
dimensional polygonal computational grid, which deforms according to the surrounding fluid flow.<br />
Large deformations and topological changes are achieved by applying the swapping-edge library<br />
<strong>of</strong> Menon [4].<br />
The surfactant is present both in the bulk phases and on the fluidic interface. While the surfactants<br />
can be treated as dilute in the bulk, we find high concentrations on the interface.Therefore,<br />
the transport <strong>of</strong> the surfactants on the fluidic interface is described by coupled species transport<br />
equations and multicomponent diffusion is modeled applying the Maxwell-Stefan equations,<br />
which need to be inverted in order to compute the diffusion fluxes. An iterative inversion method<br />
according to Giovangigli [1] is adapted and implemented in the OpenFOAM library, to lower<br />
the computational effort for systems with multiple surfactants. The resulting diffusive fluxes are<br />
inserted into the species transport equations and the model is completed by the total mass balance<br />
and the momentum equation. Since the transport processes <strong>of</strong> the surfactants are strongly<br />
coupled, a segregated solution procedure does not lead to physically correct results. Hence, the<br />
equation system is solved applying a block-coupled linear solver, which we adapted to fit the<br />
finite-area method [3]. Since the surface tension is strongly dependent on the concentration <strong>of</strong><br />
surfactants, it cannot be treated constant on the interface. Therefore we model the local variation<br />
<strong>of</strong> the surface tension. Sorption processes are modeled using a multi-region coupling algorithm,<br />
in which different sorption isotherms can be adopted.<br />
We show the application <strong>of</strong> the developed solver on pending drops and the influence <strong>of</strong> the<br />
surfactant on the surface tension.<br />
[1] V. Giovangigli, Convergent iterative methods for multicomponent diffusion. IMPACT Comput.<br />
Sci. Eng. 3(2), (1991) 244–276.<br />
[2] H. Jasak, A. Jemcov and Z. Tukovich: A C++ library for complex physics simulations.<br />
In: International Workshop on Coupled Methods in Numerical Dynamics IUC, Dubrovnik,<br />
Croatia, September, (2007) 19-21.<br />
[3] K. Kissling, H. Marschall, D. Bothe: Direct numerical solution <strong>of</strong> multicomponent surfactant<br />
transport on fluid interfaces. 6th International Berlin Workshop on Transport Phenomena<br />
with Moving Boundaries 24th-25th November 2011, Berlin, Germany (2011).<br />
[4] S. Menon, A Numerical Study <strong>of</strong> Droplet Formation and Behaviour Using Interface Tracking<br />
Methods. PhD Thesis University <strong>of</strong> Massachusetts (2011).<br />
[5] Z. Tukovic and H. Jasak, Simulation <strong>of</strong> Free-Rising Bubble with Soluble Surfactant using<br />
Moving Mesh Finite Volume/Area Method. 6th International Conference on CFD in Oil &<br />
Gas, Metallurgical and Process Industries (2008).<br />
[6] H. G. Weller, G. Tabor, H. Jasak, and C. Fureby. A tensorial approach to computational<br />
continuum mechanics using object orientated techniques. Comput. Phys., 12(6) (1998),<br />
620-631.
244 Section 11: Interfacial flows<br />
Molecular dynamics simulation <strong>of</strong> lubricated contact between textured surfaces<br />
Oleg Khromov, Wenzhe Shan, Udo Nackenhorst (<strong>Universität</strong> Hannover) Schedule<br />
The influence <strong>of</strong> surface texture on the evolution <strong>of</strong> lubricated contact is quite important. Careful<br />
manufacturing <strong>of</strong> the contacting surface can lead to its drag reduction with further achievement <strong>of</strong><br />
superhydrophobic state. Besides, it changes the macroscopic boundary condition to allow nonzero<br />
slip velocity.<br />
In this contribution a sophisticated 3D molecular dynamic simulation approach is presented<br />
and results for the lubricated contact between textured surfaces will be shown. The contacting<br />
surfaces are assumed to be deformable and the accumulation <strong>of</strong> worn-out debris is considered.<br />
The lubrication liquid layer is considered to be compressible polyatomic fluid. For studying the<br />
macroscopic behavior <strong>of</strong> the lubricated surfaces, the friction coefficient has been interpolated<br />
and investigated under the influence <strong>of</strong> various modeling parameters. The external pressure is<br />
taken as one <strong>of</strong> the simulation parameters governing the degree <strong>of</strong> textured surface wetting and,<br />
consequently, the slippage <strong>of</strong> the fluid on the solid. The relative direction <strong>of</strong> the flow to the<br />
textured surface affects the apparent friction as well. Comparative studies <strong>of</strong> the values <strong>of</strong> the<br />
friction coefficient are performed to assume the conditions leading to longer lifetime <strong>of</strong> the texture.<br />
S11.6: Waves and Jets Thu, 16:00–18:00<br />
Chair: Holger Marschall S1|03–123<br />
Growth rate and dominant frequency <strong>of</strong> unstable interfacial waves in air-water mixing<br />
layers<br />
Thomas Otto (TU Ilmenau), Maurice Rossi (Institute d’Alembert, CNRS/University Pierre and<br />
Marie Curie), Thomas Boeck (TU Ilmenau) Schedule<br />
We are interested in the linear instability <strong>of</strong> growing interfacial waves that appear near the nozzle<br />
or splitter plate in liquid atomization by fast gas streams. Inviscid models have not been able<br />
to explain the growth rates <strong>of</strong> these waves measured in experiments. We apply viscous stability<br />
analysis to this problem in order to determine if the properties <strong>of</strong> these waves can be described<br />
within the limitations <strong>of</strong> the parallel flow assumption.<br />
To this end, we construct a basic velocity distribution with a velocity deficit near the interface.<br />
This modification accounts for the proximity <strong>of</strong> the splitter plate, where the liquid and gas have<br />
zero velocity. It leads to an additional parameter describing the velocity deficit at the interface<br />
relative to the free-stream velocities in the liquid and gas phase. For the streamfunction perturbations<br />
we solve the traditional Orr-Sommerfeld problem for two coupled layers in both temporal<br />
and spatial setting.<br />
We apply our stability analysis to two different atomisation model experiments performed<br />
with air and water using a concentric and a planar nozzle configuration. In these experiments<br />
the spatial growth rate and dominant frequency <strong>of</strong> the unstable waves have been measured for<br />
a range <strong>of</strong> different air and water velocities. In contrast to purely inviscid stability theory, our<br />
viscous analysis can reproduce the growth rates satisfactorily. Agreement with the experimental<br />
frequencies is less favorable, which may be caused by non-parallel effects. The importance <strong>of</strong><br />
different physical instability mechanisms will also be discussed.
Section 11: Interfacial flows 245<br />
High-speed jet formation after solid object impact<br />
Stephan Gekle (TU München), Jose Manuel Gordillo (Universidad de Sevilla), Devaraj van der<br />
Meer, Detlef Lohse (University <strong>of</strong> Twente) Schedule<br />
A circular disc hitting a water surface creates an impact crater which after collapse leads to<br />
a vigorous jet. Upon impact an axisymmetric air cavity forms and eventually pinches <strong>of</strong>f in a<br />
single point halfway down the cavity. Two fast sharp-pointed jets are observed shooting up- and<br />
downwards from the closure location, which by then has turned into a stagnation point surrounded<br />
by a locally hyperbolic flow pattern. This flow, however, is not the mechanism feeding the jets.<br />
Using high-speed imaging and numerical simulations we show that jetting is fed by the local flow<br />
around the base <strong>of</strong> the jet, which is forced by the colliding cavity walls. We show how the wellknown<br />
theory <strong>of</strong> a collapsing void (using a line <strong>of</strong> sinks on the symmetry axis) can be continued<br />
beyond pinch-<strong>of</strong>f to obtain a new and quantitative model for jet formation which agrees well with<br />
our numerical and experimental data.<br />
A fully adaptive finite element scheme for the Cahn-Hilliard Navier-Stokes system<br />
Michael Hinze, Christian Kahle (<strong>Universität</strong> Hamburg) Schedule<br />
We consider the Cahn-Hilliard Navier-Stokes system (CHNSS) in the phasse field approximation<br />
with the double obstacle potential, and apply a semi-implicit scheme to its time discretization.<br />
We relax the variational inequalities appearing in every time step by a penalization approach<br />
and develop reliable and effective residual based a posteriori error estimators for the resulting<br />
PDE system along the lines <strong>of</strong> [1]. Several numerical experiments show the performance <strong>of</strong> our<br />
approach. The work presented extends the investigations <strong>of</strong> [1] on adaptivity for the Cahn Hilliard<br />
system to the CHNSS.<br />
[1] An adaptive finite element Moreau-Yosida-based solver for a non-smooth Cahn-Hilliard problem,<br />
to appear in OMS.
246 Section 12: Waves and acoustics<br />
Section 12: Waves and acoustics<br />
Organizers: Claus-Dieter Munz (<strong>Universität</strong> Stuttgart), Wolfgang Schröder (RWTH Aachen)<br />
S12.1: Aeroacoustic Tue, 13:30–15:30<br />
Chair: Wolfgang Schröder S2|02–C120<br />
Computational aeroacoustics - Advanced finite element scheme for acoustic perturbation<br />
equations<br />
Manfred Kaltenbacher, Andreas Hüppe (<strong>Universität</strong> Klagenfurt), Aaron Reppenhagen (Virtual Vehicle<br />
Research and Test Center Graz), Barbara Wohlmuth (TU München) Schedule<br />
Since the beginning <strong>of</strong> computational aeroacoustics (CAA) several numerical methodologies have<br />
been proposed. Due to practical advantages provided by the separate treatment <strong>of</strong> fluid and<br />
acoustic computations, hybrid methodologies still remain the most commonly used. Therewith, a<br />
splitting <strong>of</strong> the unknowns velocity �u, pressure p and density ρ into mean (denoted by an overline)<br />
and fluctuating (denoted by the superscript a) parts is performed. Such an ansatz results, e.g., in<br />
the acoustic perturbation equations [1]<br />
∂pa ∂t + c2ρ ∇ · �u a + �u · ∇p a = qc ; ρ ∂�ua<br />
∂t + ρ(�u · ∇)�u a + ∇p a = �qm<br />
with c the speed <strong>of</strong> sound and qc, �qm acoustic source terms. Its variational formulation is then<br />
given as follows (for simplification we use homogeneous Dirichlet boundary conditions): Find<br />
(�u a , pa ) ∈ V × W such that<br />
�<br />
∂<br />
∂t<br />
p a ϕdx − c 2 �<br />
ρ �u a �<br />
· ∇ϕ dx +<br />
�<br />
�u · ∇p a� �<br />
ϕ dx = qcϕ dx (1)<br />
ρ ∂<br />
∂t<br />
�<br />
�v a · � �<br />
ψ dx +<br />
Ω<br />
Ω<br />
∇p a · � �<br />
ψ dx + ρ<br />
Ω<br />
Ω<br />
�<br />
�u · ∇�u a� · � �<br />
ψ dx =<br />
Ω<br />
Ω<br />
�qm · � ψ dx (2)<br />
for all ( � ψ , ϕ) ∈ V × W .<br />
Following [2] we apply a mixed formulation and apply spectral finite elements. In order to<br />
stabilize our formulation, we use similar techniques as for DG-approaches and reformulate the<br />
third term in (2) as a special flux term (upwinding) and furthermore add a jump-term in the<br />
acoustic particle velocity �u a along common element interfaces.<br />
Within our talk, we will present the efficiency <strong>of</strong> the proposed numerical scheme and demonstrate<br />
its applicability to industrial relevant applications.<br />
[1] R. Ewert and W. Schröder. Acoustic perturbation equations based on flow decomposition via<br />
source filtering. Journal <strong>of</strong> Comp. Phys., 188:365398, 2003.<br />
[2] G. Cohen and S. Fauqueux. Mixed finite elements with mass-lumping for the transient wave<br />
equation. Journal <strong>of</strong> Comp. Acoustics, 8:171188, 2000.<br />
Simulation <strong>of</strong> a Nozzle-Jet Configuration including the Acoustic Near-Field<br />
Stefan Bühler, Leonhard Kleiser (ETH Zürich) Schedule<br />
A numerical setup is presented which allows to study a circular jet flow configuration in which<br />
the nozzle is included in the simulation domain. Direct Numerical Simulations (DNS) are performed<br />
using up to 10 th order compact finite-difference schemes which are stabilized by applying
Section 12: Waves and acoustics 247<br />
a mild low-pass filter. A parallelization approach has been implemented which shows good weak<br />
and strong scaling behavior. At the inflow the Synthetic Eddy Method is employed to generate<br />
turbulent fluctuations in the nozzle boundary layer with prescribed statistics, which are imposed<br />
by a sponge (forcing) layer technique. A comparison <strong>of</strong> the flow field within the nozzle and in the<br />
vicinity <strong>of</strong> the trailing edge is made to a recent DNS study in which a fully developed turbulent<br />
pipe flow serves as a model for the upstream unsteadiness <strong>of</strong> the subsequent jet. Simulation results<br />
for the jet flow field obtained at Reynolds number ReR = 9050 and a Mach number Ma = 0.9<br />
as well as for the acoustic near-field are found to be in good agreement with recent nozzle-jet<br />
simulation results at higher Reynolds number.<br />
Airframe noise prediction on unstructured grids<br />
Marcus Bauer (DLR Braunschweig) Schedule<br />
Airframe noise is an important contributor to the overall noise generated by modern airliners with<br />
quiet engines, especially during the approach and landing phase <strong>of</strong> flight. Then, main airframe<br />
noise sources are geometrically complex objects like the landing gear or the airfoils’ deployed<br />
slats and flaps. The goal <strong>of</strong> this work is to efficiently predict such kinds <strong>of</strong> noise. Therefore, the<br />
acoustic perturbation equations (APE) are solved, a discontinuous Galerkin (DG) method with<br />
nodal shape functions given in terms <strong>of</strong> Lagrange polynomials providing their spatial discretization<br />
on flexible, unstructured meshes. The unsteady, turbulent source term <strong>of</strong> the APE is efficiently<br />
modelled via the FRPM (fast random particle mesh) method based on statistical turbulence information<br />
from a RANS (Reynolds-Averaged Navier-Stokes) solution. Slat noise <strong>of</strong> various high-lift<br />
airfoil configurations is computed in two space dimensions. Computations are indeed cheap and<br />
deliver good agreement with wind tunnel measurements and expensive scale-resolving approaches<br />
like large eddy simulation (LES). Future work aims at the application <strong>of</strong> the DG-APE-FRPM<br />
approach to predict flap side edge noise. To this end, a three-dimensional DG-APE solver is<br />
currently under development at German Aerospace Center (DLR).<br />
On the impact <strong>of</strong> thermal sources on noise generation<br />
A. Hahnenkamm, M. Münsch, H. Lienhart, R. Masood, E. Lopez, L. Zhou, A. Delgado (<strong>Universität</strong><br />
Erlangen-Nürnberg) Schedule<br />
Sound emission is nowadays considered as a major environmental issue. The sound emission is<br />
generated, amongst other sources, due to an increasing amount <strong>of</strong> traffic and transport, i.e. road<br />
transport, rail and air traffic. Here, sound emission presents a significant risk to public health and<br />
a major cause <strong>of</strong> stress, especially in industrial countries. In this framework the present work is<br />
addressed to the topic <strong>of</strong> active noise control with the target <strong>of</strong> noise reduction.<br />
The investigated method is based on the idea <strong>of</strong> noise control due to thermal sources which<br />
are assumed to have an impact on the flow field due to weakly compressible effects <strong>of</strong> the flowing<br />
media. For that purpose two benchmark test cases were developed to investigate the effects <strong>of</strong><br />
thermal sources. In detail the flow over a forward facing step and flow around a circular cylinder<br />
with heated walls was investigated. In the first test case the step itself and some part up- and<br />
downstream <strong>of</strong> the step was heated to affect the re-circulating flow downstream <strong>of</strong> the step and<br />
the base vortex in front <strong>of</strong> the step. The cylinder was heated entirely. Wall temperatures up to<br />
550 K were obtained for both benchmarks. Measurements <strong>of</strong> sound emission conducted in an<br />
aero-acoustic wind tunnel showed an only limited effect <strong>of</strong> the heating on the sound emission for<br />
the test cases and not in all the cases sound reduction was achieved.<br />
For the cylinder test case the sound emission was reduced due to heating effects, specially the<br />
tonal emission connected with the Strouhal frequency was reduced up to 10 dB depending on the<br />
flow velocity. LDA measurements <strong>of</strong> the flow in the wake <strong>of</strong> the cylinder indicated an expansion <strong>of</strong>
248 Section 12: Waves and acoustics<br />
the wake in crosswise direction, a reduction <strong>of</strong> velocity gradients and also a decrease <strong>of</strong> turbulence<br />
intensity in the shear layer <strong>of</strong> about 30 Percent was observed.<br />
For the forward facing step an increasing wall temperature caused a broadband amplification<br />
<strong>of</strong> sound emission within the whole frequency spectrum. In contrast to the cylinder test case the<br />
velocity field was just slightly influenced due to the heating. In the vicinity <strong>of</strong> the step and up<br />
to one step height above the step, turbulence intensity increased perceptibly whereas turbulence<br />
intensity was reduced in the outer region.<br />
In addition to the experimental investigations, also numerical simulations <strong>of</strong> the test cases were<br />
conducted for detailed source term analyses. Preliminary results showed the expected relation<br />
between heating, source term generation and sound emission.<br />
Experimental and numerical findings <strong>of</strong> the impact <strong>of</strong> thermal sources on sound emission on<br />
the background <strong>of</strong> two benchmark test cases will be presented in the talk.<br />
Aerodynamic sound generation by turbulence in plane shear flows<br />
G.Khujadze, G.Chagelishvili (E. Kharadze Georgian Astrophysical Observatory), M.Oberlack (TU<br />
<strong>Darmstadt</strong>), A.Tevzadze (Iv. Javakhishvili University Tbilisi), J.Hau (TU <strong>Darmstadt</strong>), G.Bodo<br />
(Osservatorio Astronomico di Torino) Schedule<br />
The nonlinear aerodynamic sound generation by turbulence has been long analyzed since the<br />
foundation <strong>of</strong> the theory <strong>of</strong> aerodynamic sound in pioneering papers by Lighthill [1,2]. He noted<br />
that velocity shear can increase the acoustic wave emission in the aerodynamic situation due to the<br />
existence <strong>of</strong> linear terms in the inhomogeneous part <strong>of</strong> the analogy equations. In the paper [3] it<br />
was described a mechanism <strong>of</strong> linear aerodynamic sound generation. Therein it was shown that the<br />
linear phenomenon <strong>of</strong> the conversion <strong>of</strong> vortex mode into the acoustic wave mode induced by the<br />
non-normality <strong>of</strong> the flow is the only contributor to the acoustic wave production <strong>of</strong> the unbounded<br />
shear flows and the potential vorticity was identified as the linear source <strong>of</strong> acoustic waves. The<br />
results <strong>of</strong> comparative analysis <strong>of</strong> linear and nonlinear aerodynamic sound generation by turbulent<br />
perturbations in these flows, especially in plane Couette flow and jets are presented. Numerical<br />
study <strong>of</strong> the generation <strong>of</strong> acoustic waves by stochastic/turbulent perturbations embedded in<br />
these flows are performed. The spectrum has a peak at some steamwise wave-number k0 in the<br />
form<br />
Vx ′ (x, y) = Be −y2 /L2 �<br />
cos(2πζ1(y))<br />
+∞<br />
−∞<br />
dkx<br />
� kx<br />
k0<br />
� 6<br />
e −<br />
�<br />
kx<br />
k0<br />
� 6<br />
e ikxx+i2πζ2(kx) , (1)<br />
where ζ1(y) and ζ2(kx) are random numbers in the range [0, 1] varying with y and kx respectively,<br />
L denotes the localization scale in the cross-stream direction. The half-width <strong>of</strong> the spectrum <strong>of</strong><br />
the inserted perturbation meets the condition ∆k0 ≪ k0, that allows to discriminate linearly<br />
and nonlinearly generated acoustic waves and to carry out comparative analysis <strong>of</strong> linear and<br />
nonlinear aerodynamic sound generation by turbulent perturbation.<br />
According to our study the linear aerodynamic sound generation dominates over the nonlinear<br />
one at moderate and high shear rates up to large amplitudes (B ∼ 1000) <strong>of</strong> the turbulent<br />
perturbations. The mean flow vorticity is larger than the perturbation potential vorticity.<br />
[1] Lighthill M. J.: Proc. R. Soc. London, Ser. A 211, 564 (1952).<br />
[2] Lighthill M. J.: Proc. R. Soc. London, Ser. A 222, 1 (1954).<br />
[3] Chagelishvili G., Tevzadze A. et al.: Phys.Rev.Lett. 79, 3178 (1997).
Section 12: Waves and acoustics 249<br />
S12.2: Waves in Structures Tue, 16:00–18:00<br />
Chair: Claus-Dieter Munz S2|02–C120<br />
Study <strong>of</strong> mode conversion at defects in rope structures using ultrasonic waves<br />
Stefan Bisch<strong>of</strong>f, Lothar Gaul (<strong>Universität</strong> Stuttgart) Schedule<br />
Ultrasonic waves travel in rope structures over long distances as guided waves (see lamb waves in<br />
plates), allowing for effective monitoring. In order to localize and characterize defects, an exact<br />
knowledge <strong>of</strong> the propagation, reflection and transmission properties <strong>of</strong> the ultrasonic waves is<br />
required. These properties can be obtained using the Finite Element Method by modeling a<br />
segment <strong>of</strong> the periodic wave guide with a periodicity condition. The solution <strong>of</strong> the corresponding<br />
eigenvalue problem leads to all propagating modes <strong>of</strong> the waveguide as well as locally generated<br />
evanescent modes.<br />
The Boundary Element Method is used in combination with the Finite Element Method for<br />
the characterization <strong>of</strong> the wave propagation. The mode conversion at discontinuities, such as<br />
cracks or notches, can be subsequently described by reflection and transmission coefficients. The<br />
reliability and numerical accuracy <strong>of</strong> the simulation results are verfied by comparison with experimental<br />
findings.<br />
Numerical computation <strong>of</strong> dispersion relations in wave guides<br />
Hauke Gravenkamp (BAM Berlin), Chongmin Song (University <strong>of</strong> New South Wales, Sydney),<br />
Jens Prager (BAM Berlin) Schedule<br />
Guided waves in thin-walled structures, such as plates or pipes, are widely used for non-destructive<br />
testing and structural health monitoring applications. For high frequencies, a large number <strong>of</strong><br />
propagating modes can be excited. As in general all modes are strongly dispersive, the accurate<br />
calculation <strong>of</strong> the dispersion relations is essential. Analytical models, which are used for homogeneous<br />
or simply layered structures, fail to give sufficient results, if the geometries become more<br />
complex or if the material parameters vary continuously on the specimen’s cross section.<br />
In the present work, a numerical approach is presented for the computation <strong>of</strong> the frequencydependent<br />
wave numbers and group velocities <strong>of</strong> the propagating modes in wave guides. The<br />
formulation is based on the Scaled Boundary Finite Element Method. The cross section <strong>of</strong> the wave<br />
guide is discretized in the Finite Element sense. The governing equations <strong>of</strong> general elastodynamics<br />
are applied. A standard eigenvalue problem is then derived for the calculation <strong>of</strong> wave numbers.<br />
The group velocities can directly be obtained as the eigenvalue derivatives. For the discretization<br />
<strong>of</strong> the boundary, higher-order elements have been employed as they have shown to drastically<br />
improve the accuracy and efficiency <strong>of</strong> the computation. Polynomials up to 14th order have been<br />
applied as the element shape functions.<br />
This approach is not limited to homogeneous materials. Complex wave guides consisting <strong>of</strong><br />
an arbitrary number <strong>of</strong> layers or materials with continuously varying elastic parameters can<br />
accurately be described.<br />
Simulation <strong>of</strong> Lamb wave interaction with defects in laminated plates by SFEM.<br />
Andreas Asmus, Bianca Hennings, Rolf Lammering (<strong>Universität</strong> der Bundeswehr Hamburg) Schedule<br />
A variety <strong>of</strong> online structural health monitoring systems are based on the use <strong>of</strong> Lamb-Waves<br />
which are guided waves that propagate in thin plate or shell structures, [1]. The main problems in<br />
the numerical analysis <strong>of</strong> high frequency elastic waves are related to spatial and time discretization.<br />
A huge number <strong>of</strong> degrees <strong>of</strong> freedom and small time steps are needed in order to guarantee a<br />
sufficient accurate solution. In the context <strong>of</strong> Finite Elements (FEM) a fully populated mass-
250 Section 12: Waves and acoustics<br />
matrix is a drawback in respect to the computational cost <strong>of</strong> the analysis.<br />
A solution <strong>of</strong> this problem is the Spectral Finite Element Method (SFEM) which is a masslumping<br />
technique and consists in using the Gauss-Lobatto quadrature formula for computing<br />
the mass-matrix which is then diagonal. Thus, an algorithm based on an explicit time scheme is<br />
truly explicit and a noticeable decrease <strong>of</strong> computational cost can be expected, [2].<br />
The presentation deals with the implementation <strong>of</strong> Spectral Finite Elements for a first-order<br />
laminated plate. Related numerical results concerning the wave interaction with defects are presented<br />
and compared with the Literature and calculations which are based on a plane strain plate<br />
Spectral Finite Element.<br />
[1] Zhongqing Su, Lin Ye, Identification <strong>of</strong> damage using lamb waves, Lecture Notes in Applied<br />
and Computational Mechanics Vol. 48, 2009.<br />
[2] Cohen, Gary C., Higher-order numerical methods for transient wave equations, Springer,<br />
2002.<br />
Inter-wire Coupling Model Development for Health Monitoring <strong>of</strong> Cable Structures<br />
Natalie Higgins, Christoph Schaal (<strong>Universität</strong> Stuttgart) Schedule<br />
Structural Health Monitoring (SHM) allows the integrity <strong>of</strong> a system to be monitored in situ,<br />
detecting weaknesses as they form. Due to the waveguide nature <strong>of</strong> cylindrical structures, ultrasonic<br />
waves can be used to detect defects in cables over large distances. Common power line cables<br />
consist <strong>of</strong> numerous individual wires, making modeling <strong>of</strong> the energy interactions within the entire<br />
multi-wire cable very complex. Moreover, handling the multi-modal and dispersive nature <strong>of</strong> the<br />
guided wave propagation itself is already a challenge.<br />
Considering the mathematical complexity each additional wire brings, a straightforward energybased<br />
model is chosen to describe inter-wire coupling in the entire cable. This model takes into<br />
account wave propagation energy as well as energy losses due to damping and friction.<br />
While detecting cracks in two-wire cables has proven to be successful, in order to detect defects<br />
in cables with several wires, inter-wire coupling must be well understood. The purpose <strong>of</strong> this<br />
investigation is to better qualify inter-wire coupling and extend the current coupling model to include<br />
more wires. This goal is achieved through theoretical model development and experimental<br />
verification.<br />
Dispersion in Cylindrical Waveguides with Uncertain Parameters<br />
Christoph Schaal, Miriam Krautter, Michael Hanss (<strong>Universität</strong> Stuttgart) Schedule<br />
Current wave-based Structural Health Monitoring (SHM) methods <strong>of</strong> cylindrical structures rely<br />
on the accurate description <strong>of</strong> the wave numbers as a function <strong>of</strong> frequency, called dispersion. An<br />
efficient algorithm to calculate dispersion for propagating and non-propagating waves in cylindrical<br />
waveguides <strong>of</strong> a specific material has been recently developed. Using the Waveguide Finite<br />
Element method, only a segment <strong>of</strong> the waveguide is modeled with a common FEM package. By<br />
introducing a periodicity condition, the wave numbers follow directly from the eigensolutions <strong>of</strong><br />
the resulting transfer matrix.<br />
In this work, a new approach is presented where the calculations <strong>of</strong> the wave numbers and<br />
the according phase and group velocities are based on uncertain parameters, describing real-world<br />
applications more adequately. Modeling <strong>of</strong> uncertainties in parameters can be accomplished by representing<br />
the parameters as fuzzy numbers; a special kind <strong>of</strong> fuzzy sets. With the Transformation<br />
Method, which is an increasingly evolving strategy in the field <strong>of</strong> advanced fuzzy arithmetic, the
Section 12: Waves and acoustics 251<br />
effects <strong>of</strong> uncertain model parameters are investigated by simulating their propagation towards<br />
the system’s outputs.<br />
In addition to tracking the uncertain parameters to the wave numbers and velocities, overall<br />
imprecision <strong>of</strong> the results as well as measures <strong>of</strong> influence are also discussed to identify further<br />
possibilities to improve performance and robustness <strong>of</strong> SHM algorithms for cylindrical structures.<br />
Numerical simulations <strong>of</strong> pile integity tests using a coupled FEM SBFEM approach<br />
Marco Schauer, Sabine Langer (TU Braunschweig) Schedule<br />
Piles are widely-used to build a proper foundation for various buildings. The pile’s quality in<br />
soil can be tested by a so called pile integrity test. In order to apply this test, an acceleration<br />
sensor has to be attached to the pile’s head to which an impulse is sent afterwards. Due to this<br />
impulse a p-wave runs through the pile. The major part <strong>of</strong> this wave is reflected on the pile’s toe<br />
and can be measured by the attached acceleration sensor on top <strong>of</strong> the pile. This yields to an<br />
acceleration-time plot which has to be analysed to determine the pile’s condition.<br />
Sometimes the interpretation <strong>of</strong> these plots is difficult, specially when the cross-section <strong>of</strong> the<br />
pile is changing or influenced by the surrounding soil. For a better understanding <strong>of</strong> these kind<br />
<strong>of</strong> measurements, numerical simulations can be performed. For these simulations a coupled finite<br />
element method (FEM) and scaled boundary finite element method (SBFEM) approach is used.<br />
This approach satisfies the Sommerfeld radiation condition and allows the simulations <strong>of</strong> an<br />
infinite half-space. This ensures that the applied impulse is not going to be reflected at the<br />
artificial boundary which is intoduced by the numerical discretization and hence the discretised<br />
domain can be smaller than the approach which uses FEM only.<br />
S12.3: Wave Propagation Wed, 13:30–15:30<br />
Chair: Claus-Dieter Munz S2|02–C120<br />
Microscale Investigations <strong>of</strong> Highfrequency Wave Propagation Through Highly Porous<br />
Media<br />
David Uribe (Universidad EAFIT, Medellin, Colombia/<strong>Universität</strong> Bochum), Erik Saenger (ETH<br />
Zürich), Ralf Jänicke, Holger Steeb (<strong>Universität</strong> Bochum), Oscar Ruiz (Universidad EAFIT, Medellin,<br />
Colombia) Schedule<br />
Wave propagation in highly porous materials has a well established theoretical background, still<br />
there are parameters which require complex laboratory experimentation in order to find numerical<br />
values. This paper presents an effective method to calculate the tortuosity <strong>of</strong> aluminum foam<br />
using numerical simulations. Additionally, the interaction mechanisms between fluid and foam<br />
phases was determined. The work flow begins with the acquisition <strong>of</strong> the foam geometry by<br />
means <strong>of</strong> a micro-ct machine and further image segmentation and analysis. The elastodynamic<br />
wave propagation equation is solved using a displacement-stress rotated staggered finite-difference<br />
technique. The effective wave velocities are calculated and using the fluid and aluminum effective<br />
properties, the tortuosity is determined. The numerical simulations closely match the results from<br />
our experimental data.<br />
Experiments on Peregrine soliton type deep water gravity waves<br />
H<strong>of</strong>fmann, N.P., Chabchoub, A. (TU Hamburg-Harburg) Schedule<br />
The Peregrine soliton solution <strong>of</strong> the Nonlinear Schrödinger equation is <strong>of</strong>ten regarded as the<br />
prototype <strong>of</strong> oceanic rogue waves. We present measurements <strong>of</strong> laboratory realizations obtained<br />
in a water wave tank for first and higher order solutions. The experimental data is compared with
252 Section 12: Waves and acoustics<br />
theoretical predictions based on Peregrine and Peregrine-Akhmediev solutions <strong>of</strong> the Nonlinear<br />
Schrödinger Equation. For small steepness <strong>of</strong> the underlying carrier wave, excellent agreement<br />
can be observed.<br />
Internal Flow And Pressure Waves In Reciprocating Compressors<br />
Thomas Müllner (TU Wien) Schedule<br />
In reciprocating compressors gas is compressed from the pressure level in the suction chamber to<br />
a higher pressure in the discharge chamber using the driving power from a moving piston. The gas<br />
flow is controlled by self-acting valves. In a first approach a simple valve model is considered. The<br />
suction valves open if the in-cylinder pressure is lower then the suction pressure and close if the<br />
pressure is higher, while the discharge valves open when the pressure inside the cylinder exceeds<br />
the discharge pressure. Valve opening and closing cause internal pressure waves. The 3D-flow and<br />
the waves inside the compressor are computed using the unsteady Euler-equations. Results for<br />
the flow and the pressure waves will be presented.<br />
Studies on material properties used for noise barriers<br />
Alin-Cosmin Tot, Calin Lumei, Mariana Arghir (Technical University <strong>of</strong> Cluj-Napoca) Schedule<br />
Noise barriers are typically used to reduce noise near to the highway or near to the building<br />
construction. Factors that characterize the barrier effectiveness are the position and geometry <strong>of</strong><br />
the barrier, its height and materials which is made from. Considering the interaction <strong>of</strong> noise with<br />
the surface <strong>of</strong> the barrier we can distinguish three principles: reflection, resonance and absorption<br />
<strong>of</strong> the waves. The phenomenon <strong>of</strong> reflection is met in special on barriers made <strong>of</strong> rigid material<br />
and a surface roughness which does not contribute to noise mitigation. Resonant element consists<br />
<strong>of</strong> a cavity which communicates with the outside environment through <strong>of</strong> a hole or a membrane.<br />
Under the action <strong>of</strong> wave sound that penetrates through the hole or the membrane, the volume<br />
<strong>of</strong> air in the cavity resonators running alternative movements <strong>of</strong> oscillation, sound energy will be<br />
dissipated due to the phenomena <strong>of</strong> inertia and viscosity. Areas with barriers absorbent coverings<br />
materials contain porous elements attenuate <strong>of</strong> airborne noise intensity. The main feature is<br />
that the phonon absorbent materials have a porous structure, with intercommunicating canals<br />
communicating through channels or openings in the material. Thus, attenuation and absorption<br />
<strong>of</strong> sound is produced by multiple reflections <strong>of</strong> sound waves in the material and wave refractions<br />
inside it. The structure <strong>of</strong> porous materials can be cellular, fibrous or granular. Determination <strong>of</strong><br />
sound-absorbing nature <strong>of</strong> these materials is one <strong>of</strong> the most important acoustic characteristics.<br />
Measurement <strong>of</strong> sound absorption coefficients in an impedance tube is achieved by two different<br />
methods: Wave ratio method [1] and transfer function method [2]. In conclusion, this paper may<br />
be considered as guidance in choosing a proper absorbing material using an impedance tube.<br />
[1] ISO 10534-1:1996, Acoustics - Determination <strong>of</strong> sound absorption coefficient and impedance<br />
in impedance tubes - Part 1: Method using standing wave ratio<br />
[2] ISO 10534-2:1998, Acoustics determination <strong>of</strong> sound absorption coefficient and impedance<br />
in impedance tubes. Part 2: transfer function method.<br />
Anti-plane shear waves in a structurally-nonlinear fibrous composite material<br />
Igor V. Andrianov (RWTH Aachen), Vladyslav V. Danishevskyy, Olexandr I. Ryzhkov (Prydniprovska<br />
State Academy <strong>of</strong> Civil Engineering and Architecture, Ukraine), Dieter Weichert (RW-<br />
TH Aachen) Schedule
Section 12: Waves and acoustics 253<br />
Elastic waves propagating in heterogeneous solids can undergo the effects <strong>of</strong> nonlinearity and<br />
dispersion. The types <strong>of</strong> nonlinearity can be classified as geometrical, physical, and structural.<br />
Dispersion is caused by successive reflections and refractions <strong>of</strong> local waves at the interfaces<br />
between the components. The balance state between nonlinearity and dispersion results in the<br />
formation <strong>of</strong> stationary nonlinear waves. Increase in nonlinearity leads to the appearance <strong>of</strong> localized<br />
nonlinear modes that accumulates all the mechanical energy and can propagate for long<br />
distances keeping stable the shape and velocity. We study 2D anti-plane shear waves propagating<br />
in a structurally-nonlinear fibrous composite material with an imperfect interface between<br />
the matrix and fibres. The macroscopic wave equation is obtained by the method <strong>of</strong> asymptotic<br />
homogenization. Explicit analytical expressions for the effective linear and nonlinear elastic<br />
moduli are obtained. Magnitude <strong>of</strong> the coefficient at the dispersive term is determined by the<br />
Floquet-Bloch approach. For stationary plane waves, analytical solutions are derived in terms<br />
<strong>of</strong> elliptic functions. A number <strong>of</strong> nonlinear phenomena are detected, such as (i) dependence <strong>of</strong><br />
the wave shape, velocity and attenuation upon the amplitude and (ii) development <strong>of</strong> localized<br />
solitary and kink (shock) waves. Obtained results can be practically important for the purposes<br />
<strong>of</strong> non-destructive testing in Materials Science as well as for design <strong>of</strong> new acoustic devices in<br />
Engineering (such as wave-guides, acoustic filters, ultrasonic transducers, etc.)<br />
Acoustical performance <strong>of</strong> concreted wood fiber materials<br />
Calin Lumei, Alin-Cosmin Tot, Mariana Arghir (Technical University <strong>of</strong> Cluj-Napoca) Schedule<br />
The paper presents the acoustical properties <strong>of</strong> a material which is made from a mixture <strong>of</strong> wood<br />
and concrete. Its composed <strong>of</strong> recycled waste wood which is first chipped in wood fiber and then<br />
is mineralized and bonded with Portland cement. Measurements on small specimens were performed<br />
in an impedance tube [1] to find the absorption coefficient. A mathematical model [2] is<br />
also presented in order to determine the absorption coefficient analytically. It is then optimized<br />
to fit the data results. Originally, this model was proposed to describe the impact <strong>of</strong> porous asphalt<br />
on highway noise levels. The model consists <strong>of</strong> three parameters: flow resistivity, porosity<br />
and structure factor or tortuosity. These parameters can be independently determined. For the<br />
optimization <strong>of</strong> the model, a simple approximation <strong>of</strong> these three parameters to data results is<br />
made. Knowing the acoustic performance <strong>of</strong> concreted wood fiber materials is important as it is<br />
100% recyclable that can used for building constructions or noise barriers.<br />
[1] ISO 10534-2:1998, Acoustics determination <strong>of</strong> sound absorption coefficient and impedance in<br />
impedance tubes. Part 2: transfer function method.<br />
[2] Bérengier, M., M. Stinson, et al. (1997), Porous road pavements: Acoustical characterization<br />
and propagation effects. Journal <strong>of</strong> the Acoustical Society <strong>of</strong> America 101(1): 155-162.<br />
S12.4: Elastic Waves Wed, 16:00–18:00<br />
Chair: Claus-Dieter Munz S2|02–C120<br />
Nonlinear Rayleigh elastic surface waves:new wave equations, solutions, and effects<br />
J.J. Rushchitsky, O.O. Khotenko (P Timoshenko Institute <strong>of</strong> Mechanics, Kyiv, Ukraine) Schedule<br />
The presented results can be thought as next to the publication, in which a row <strong>of</strong> new nonlinear<br />
wave equations is obtained for the two-dimensional case <strong>of</strong> elastic quadratic nonlinear deformation<br />
within the framework <strong>of</strong> Murnaghan model. It should be noted that the Rayleigh wave theory<br />
is no the complete fragment <strong>of</strong> classical theory, it is still developing. In the classical statement
254 Section 12: Waves and acoustics<br />
<strong>of</strong> the problem on Rayleigh surface waves, the wave along the plane x3 = 0 is studied, when the<br />
elastic medium occupies the upper half-space. It is assumed further that the problem is the twodimensional<br />
one (the plane problem in the plane Ox1x3 ). The direction <strong>of</strong> motion is choosing along<br />
the axis Ox1. The motion equations are then transforming into two non-linear wave equations.<br />
These equations are the basic ones in analysis <strong>of</strong> nonlinear elastic waves propagating in the<br />
plane Ox1x3, including the waves localized near the boundary surface. One <strong>of</strong> such waves is the<br />
classical Rayleigh wave. The new nonlinear wave equations are solved by the method <strong>of</strong> successive<br />
approximations.<br />
Main observations: 1. The corresponding to the 2nd approximation wave picture is described<br />
by the wave parameters <strong>of</strong> the 1 st (linear) approximation. 2. The 2 nd approximation is characteristic<br />
by the 2 nd harmonic in contrast to the 1 st approximation characteristic by the 1 st harmonic<br />
- the 2 nd harmonic relative to the propagating in direction <strong>of</strong> the horizontal coordinate wave and<br />
the 2 nd harmonic relative to the exponential delay <strong>of</strong> wave along the vertical coordinate. These<br />
harmonics amplitudes depend nonlinearly on coordinates and then increase with increasing <strong>of</strong><br />
time <strong>of</strong> the Rayleigh wave propagation. As a result, the 1 st harmonic will distort. 3. The dependence<br />
<strong>of</strong> the 2 nd harmonics amplitudes on the squared 1 st harmonics amplitudes is the standard<br />
situation for the method <strong>of</strong> successive approximations and has some consequences relative to the<br />
1 st harmonic distortion. In particular, because the amplitudes in engineering materials and the<br />
earth’s crust have very distinguishing orders (they are measured in millimeters-microns in the<br />
first case and centimeters in the second case), then to detect the effect <strong>of</strong> distortion, a smallness<br />
<strong>of</strong> the squared amplitudes must be compensated by the larger values <strong>of</strong> wave numbers (larger<br />
values <strong>of</strong> frequencies). 4. The second approximation is zeroth for the pure surface wave, but this<br />
approximation can intro-duce the essential contribution in to the wave picture for the near-thesurface<br />
wave. 5. The derived new nonlinear equation for determination <strong>of</strong> the wave number shows<br />
the new factor <strong>of</strong> an initial wave pr<strong>of</strong>ile distortion - distortion owing the wave length changing<br />
with unchanging frequency.<br />
On the geometric transformations and new materials<br />
Veturia Chiroiu (Institute <strong>of</strong> Solid Mechanics <strong>of</strong> Romanian Academy) Schedule<br />
In this paper, yet another idea <strong>of</strong> designing new materials is investigated. The property <strong>of</strong> Helmholtz<br />
equation to be invariant under geometric transformations is exploited to obtain new materials<br />
with inhomogeneous and anisotropic distribution <strong>of</strong> elastic properties. This approach opens<br />
up the possibility to configure new materials that might be useful in the design <strong>of</strong> elastic cloaking<br />
devices. As an example, the conventional foam which occupies a given domain is transformed into<br />
an auxetic material which fills another domain. The new material is inhomogeneous and anisotropic<br />
and exhibits new interesting properties. All computations are performed in the framework <strong>of</strong><br />
the Cosserat theory <strong>of</strong> elasticity which admits degrees <strong>of</strong> freedom not present in classical elasticity,<br />
i.e. rotation <strong>of</strong> points in the material and couple stresses<br />
Conservation laws and implectic operators <strong>of</strong> two-dimensional Zakharov-Kuznetsov<br />
nonlinear dynamical system<br />
Arkadii Kindybaliuk, Mykola Prytula (Ivan Franko National University in Lviv, Ukraine) Schedule<br />
Following two-dimensional nonlinear dynamical system is considered in this paper:<br />
ut = uxxx + uxxy + uxyy + uyyy − uux − uuy = K[u], (1)<br />
where K[u] - smooth by Frechét functionally polynomial vector field [1].<br />
System (1) has been derived as a sum <strong>of</strong> two nonlinear models describing wave propagation
Section 12: Waves and acoustics 255<br />
in x-direction [2]: ut = uxxx + uxyy − uux and y-direction: ut = uyyy + uxxy − uuy . Derived system<br />
(1) is isotropic, since it describes wave propagation in x and y direction simultaneously.<br />
Conserved quantities and implectic operators are fundamental conceptions in theory <strong>of</strong> dynamical<br />
systems [1].<br />
Infinite hierarchy <strong>of</strong> conservation laws has been found. First three <strong>of</strong> them are presented below:<br />
��<br />
γ0 =<br />
Ω<br />
��<br />
u dxdy, γ1 =<br />
Ω<br />
u 2 dxdy, γ2 = − 1<br />
2<br />
Also implectic operators for system (1) have been found:<br />
η = − (∂x + ∂y) ,<br />
��<br />
Ω<br />
�<br />
u 2 x + u 2 y + u3<br />
�<br />
dxdy.<br />
3<br />
ϑ = ∂xxx + ∂xxy + ∂xyy + ∂yyy − 1<br />
3 (u∂x + ∂xu + u∂y + ∂yu) .<br />
In our case correspondal Hamiltonians are:<br />
Hη = γ2, Hϑ = γ1<br />
Obtained results are useful for investigating complete integrability <strong>of</strong> dynamical system and verification<br />
<strong>of</strong> numeric schemes for their solving.<br />
[1] Prykarpatsky A.K., Mykytiuk I. V., Algebraic integrability <strong>of</strong> nonlinear dynamical systems<br />
on manifolds: classical and quantum aspects. - Netherlands: Kluwer, - 1999. - 560p.<br />
[2] Zakharov V.E., Kuznetsov E. A., On three dimensional solitons, Sov. Phys. JETP, 39 (1974)<br />
285-286 pp.
256 Section 13: Flow control<br />
Section 13: Flow control<br />
Organizers: Christian O. Paschereit (TU Berlin), Cameron Tropea (TU <strong>Darmstadt</strong>)<br />
S13.1: Flow Control - Boundary Layers Tue, 13:30–15:30<br />
Chair: Elfriede Friedmann S1|01–A04<br />
Variation <strong>of</strong> friction drag via spanwise transversal surface waves<br />
P. Meysonnat, S. Klumpp, M. Meinke , W. Schröder (RWTH Aachen) Schedule<br />
Introducing spanwise motion into the near-wall flow field <strong>of</strong> turbulent boundary layer has proven<br />
to be an effective mean <strong>of</strong> active flow control aiming at the reduction <strong>of</strong> wall shear stress [1]. The<br />
skin-friction is responsible for about 50% <strong>of</strong> the total drag <strong>of</strong> an aircraft, making this approach<br />
very attractive for the increasing demand in greener transportation.<br />
Miscellaneous approaches for introducing spanwise motions have been studied in several experimental<br />
and numerical investigations in order to reduce the wall shear stress. Du et al. [2] used<br />
spanwise traveling excitations, realized by near wall volume forces, in a channel flow yielding a<br />
reduction in friction <strong>of</strong> up to 30%. Itoh et al.[3] experimentally investigated the drag reduction via<br />
a spanwise traveling transversal sinusoidal wall oscillation achieving a drag reduction <strong>of</strong> 7.5% in a<br />
turbulent boundary layer. Klumpp et al. [4] set-up an LES with the same mechanism to investigate<br />
the near wall features <strong>of</strong> the flow. Whereas over the unactuated wall a streaky structure is evident,<br />
for the actuated case a ribbon-like structure is formed corresponding to the excitation, affecting<br />
the friction drag [5]. They found a drag reduction <strong>of</strong> 9% compared to an unactuated wall for a<br />
particular combination <strong>of</strong> amplitude, wavelength and period, whereas other combinations even led<br />
to drag increase. In the present study two set-ups <strong>of</strong> traveling wall oscillations are investigated via<br />
LES. The first set-up (ˆy + = 30, λ + = 870, T + = 50) which matches the case in [4] possesses a higher<br />
amplitude, wavelength and period than the second case (ˆy + = 10, λ + = 174, T + = 10) which<br />
yields a drag increase <strong>of</strong> 8%. The comparison between the two set-ups evidences the existence <strong>of</strong><br />
a key feature <strong>of</strong> drag reduction with spanwise traveling wave excitation. A detailed analysis <strong>of</strong><br />
the flow field, fluctuating vorticity components, and energy balance in the system <strong>of</strong> the different<br />
configurations will be given at the conference.<br />
[1] G. E. Karniadakis and K.-S., Choi Mechanisms on transverse motions in turbulent wall flows,<br />
Annu. Rev. Fluid Mech., 35:45–62, 2003.<br />
[2] Y. Du, V. Symeonidis, and G. E. Karniadakis, Drag reduction in wall-bounded turbulence<br />
via a transverse travelling wave, J. Fluid Mech., 457:1–34, Apr. 2002.<br />
[3] M. Itoh, S. Tamano, K. Yokota, and S. Taniguchi, Drag reduction in a turbulent boundary<br />
layer on a flexible sheet undergoing a spanwise traveling wave motion, J. Turbulence, 7:1–17,<br />
2006.<br />
[4] S. Klumpp, M. Meinke and W. Schröder, Drag Reduction by Spanwise Transversal Surface<br />
Waves, J. Turbulence,22:1–13 ,2010.<br />
[5] A.-T. Le, G. N. Coleman and J. Kim., Near-wall turbulence in three-dimensional boundary<br />
layers, Int. J. Heat Fluid Flow, 21:480–488,2000.<br />
Turbulent drag reduction at moderate Reynolds numbers via spanwise velocity waves<br />
Davide Gatti (TU <strong>Darmstadt</strong>), Maurizio Quadrio (Politecnico di Milano) Schedule
Section 13: Flow control 257<br />
Several techniques are currently under investigation to decrease the friction drag in turbulent wall<br />
flows. Among the most promising ones, the streamwise-traveling waves <strong>of</strong> spanwise wall velocity<br />
have been recently shown (Quadrio et al., JFM 2009) to be simple and open-loop, to relaminarize<br />
low-Re turbulent flows and yield large reductions <strong>of</strong> drag at higher Re, and to require little energy<br />
to operate.<br />
Of course, the question whether such large drag reductions can be obtained at the high values <strong>of</strong><br />
Re typical <strong>of</strong> applications remains to be answered. Answering such question, either by experiments<br />
or DNS, is obviously challenging. For DNS, the problem lies in the tremendous increase <strong>of</strong> the<br />
computational cost with Re, that has to be appreciated in view <strong>of</strong> the need <strong>of</strong> carrying out<br />
an entire parametric study at every Re, owing to the unknown location <strong>of</strong> the optimal forcing<br />
parameters.<br />
In this paper we investigate the behaviour <strong>of</strong> the streamwise-traveling waves at relatively high<br />
Re. We use DNS <strong>of</strong> a turbulent plane channel flow with Re up to 73, 000 (or Reτ = 2, 000).<br />
To achieve high Re while keeping the computational cost affordable, computational domains <strong>of</strong><br />
reduced size are employed. Though much larger than the Minimal Flow Unit that guarantees a<br />
self-sustained turbulence (Jiménez & Moin, JFM 1991), their limited size requires special care to<br />
interpret results that are indeed still box-size dependent. Space-averaged quantities (like friction)<br />
show large temporal fluctuations when the domain size is small, and thus require longer averaging<br />
times to converge: a suitable compromise between space- and time-average is required. We<br />
instrument the DNS results with an error bar, related to the finite averaging time, which helps<br />
setting such a compromise.<br />
We focus on friction drag reduction rate R, as well as the net savings S that result from<br />
accounting for the power input Pin <strong>of</strong> the control. The effects <strong>of</strong> Re on the energetic budget and<br />
on the optimal parameters <strong>of</strong> the wall forcing are both studied.<br />
Our results indicate that up to R = 0.29 can be obtained at Reτ = 2, 000. The maximum R is<br />
found to decrease as R ∼ Re−0.22 τ in the Reynolds range investigated. This seems to confirm the<br />
trend suggested by J.I.Choi et al. (AIAA J, 2002) on the basis <strong>of</strong> a numerical study carried out<br />
up to Reτ = 400 and for the oscillating wall alone. By extrapolation we infer that R = 0.1 could<br />
be achieved at Reτ ≈ 3 × 105 . Moreover, we find that the sensitivity <strong>of</strong> R to Re becomes smaller<br />
when far from the low-Re optimum parameters: in this region, we suggest R ∼ Re−0.05 τ .<br />
Boundary behavior <strong>of</strong> viscous fluids: Influence <strong>of</strong> wall roughness and friction-driven<br />
boundary conditions<br />
Dorin Bucur (Universite de Savoie), Eduard Feireisl, Sarka Necasova (Czech Academy <strong>of</strong><br />
Sciences) Schedule<br />
We consider a family <strong>of</strong> solutions to the evolutionary Navier-Stokes system supplemented with<br />
the complete slip boundary conditions on domains with rough boundaries. We give a complete<br />
description <strong>of</strong> the asymptotic limit by means <strong>of</strong> Γ−convergence arguments, and identify a general<br />
class <strong>of</strong> boundary conditions.<br />
[1] Bucur, Dorin; Feireisl, Eduard; Nečasová, Šárka Boundary behavior <strong>of</strong> viscous fluids: influence<br />
<strong>of</strong> wall roughness and friction-driven boundary conditions. Arch. Ration. Mech. Anal. 197<br />
(2010), no. 1, 117-138.<br />
Non-sinusoidal wall oscillation for drag reduction<br />
A. Cimarelli (University <strong>of</strong> Bologna), B. Frohnapfel (TU <strong>Darmstadt</strong>), Y. Hasegawa (TU <strong>Darmstadt</strong>;<br />
University <strong>of</strong> Tokyo), E. De Angelis (University <strong>of</strong> Bologna), M. Quadrio (Politecnico di<br />
Milano) Schedule
258 Section 13: Flow control<br />
The control <strong>of</strong> wall-bounded turbulent flows with the aim <strong>of</strong> reducing the wall-shear stress is an<br />
important and challenging topic in modern fluid mechanics. Indeed, such a reduction has very<br />
important beneficial effects for engineering flow systems. One prominent control technique which<br />
allows to achieve a significant reduction <strong>of</strong> turbulent drag is based on the modification <strong>of</strong> wall<br />
turbulence by the cyclic spanwise movement <strong>of</strong> the wall, [1]. Despite the studies available in the<br />
literature, there are a number <strong>of</strong> issues related to drag reduction properties <strong>of</strong> the oscillating wall<br />
that have not yet received a definite answer. For example, it is well known that the frequency and<br />
the amplitude <strong>of</strong> the oscillation play a first-order role in determining the amount <strong>of</strong> the turbulent<br />
drag reduction rate but the effects <strong>of</strong> the shapes <strong>of</strong> the wall oscillations are still not determined.<br />
Indeed, all the attemps carried out towards achieving a reduction <strong>of</strong> turbulent friction have used<br />
a sinusoidal shape for the spanwise oscillation <strong>of</strong> the wall. For that reasons, we investigate the<br />
drag reducing properties <strong>of</strong> non-sinusoidal wall oscillations. The present work aims at answering<br />
two related questions:<br />
• How do deviations from the sinusoidal wave shape - which might occur when trying to<br />
realize an oscillating wall in practice - influence the control performance?<br />
• Is it possible to obtain flow control performance superior to the sinusoidal wall oscillations<br />
with other oscillations shapes?<br />
The analysis <strong>of</strong> the non-sinusoidal wall oscillations is performed using direct numerical simulation<br />
data <strong>of</strong> a turbulent channel flow. The simulations are carried out with an highly accurate<br />
numerical code. The friction Reynolds number <strong>of</strong> the reference simulation without wall oscillation<br />
is Reτ = 200 and the computational domain is 6.67h×2h×3.33h. All simulations for the different<br />
boundary conditions <strong>of</strong> spanwise velocity at the walls are performed starting from the same initial<br />
condition <strong>of</strong> fully developed channel flow without wall oscillation.<br />
The obtained results illustrate the dependency <strong>of</strong> the drag reduction rate, R, and <strong>of</strong> the power<br />
spent to move the walls, Pin, with respect the shape <strong>of</strong> the wall motion. An analytical model<br />
based on the generalization <strong>of</strong> the laminar solution <strong>of</strong> the Stokes layer is derived which allows<br />
the a priori prediction <strong>of</strong> R and Pin for different wall motions in turbulent flows under certain<br />
constraints.<br />
[1] M. Quadrio, Drag reduction in turbulent boundary layers by in-plane wall motion, Phil.<br />
Trans. R. Soc. A 369 (2011), 1428 – 1442.<br />
On the effect <strong>of</strong> superhydrophobic surfaces in turbulent channel flow<br />
Sebastian Türk, Gerti Daschiel, Yosuke Hasegawa, Bettina Frohnapfel (TU <strong>Darmstadt</strong>) Schedule<br />
From experimental and numerical investigations it is known that superhydrophobic surfaces lead<br />
to a decrease in skin friction drag in laminar and turbulent channel flow [2]. For turbulent channel<br />
flow, a drag reduction up to 50% can be achieved. This reduction in skin friction drag is achieved<br />
by providing an alternating gas-liquid solid-liquid interface that results in an alternating no-slip<br />
no-shear boundary condition. For laminar flow an analytic solution for calculating the effective<br />
slip length in the Stokes limit exists for certain geometries, namely for ribs oriented parallel and<br />
perpendicular to the flow [3]. The effective slip length is a parameter for quantifying the benefit<br />
<strong>of</strong> a superhydrophobic surface. For turbulent flow, no analytic solution or correlation functions<br />
are available.<br />
Within the present investigation, the impact <strong>of</strong> a superhydrophobic surface pattern oriented<br />
parallel to the main flow direction on turbulent channel flow is shown using direct numerical
Section 13: Flow control 259<br />
simulation (DNS). The predictions are carried out with a constant pressure gradient, respectively<br />
uτ = const. The friction Reynolds number is chosen to be Reτ = 180. It is shown, that for<br />
short-wave surface structures, the effective slip length in turbulent channel flow is in good agreement<br />
to the corresponding Stokes solution. However, for an increase in the wave-length <strong>of</strong> the<br />
alternating boundary conditions a deviation in effective slip length occurs. In order to identify<br />
the mechanism responsible for the observed phenomenon, the FIK-Identity [1] is used. In doing<br />
so, the resulting bulk mean velocity can be decomposed into a slip contribution, a laminar contribution<br />
and a turbulent contribution. Special attention is given to the influence <strong>of</strong> the modified<br />
surface on the turbulent quantities. In addition a critical assessment <strong>of</strong> the potential benefit <strong>of</strong><br />
using superhydrophobic surfaces in laminar and turbulent channel flows is presented.<br />
[1] Koji Fukagata, Kaoru Iwamoto, and Nobuhide Kasagi. Contribution on reynolds stress distribution<br />
to the skin friction in wall-bounded flows. Physics <strong>of</strong> Fluids, 14(11):L73, 2002.<br />
[2] Jonathan P. Rothstein. Slip on superhydrophobic surfaces. Annual Review <strong>of</strong> Fluid Mechanics,<br />
42(1):89-109, January 2010.<br />
[3] Christophe Ybert, Catherine Barentin, Cecile Cottin-Bizonne, Pierre Joseph, and Lyderic<br />
Bocquet. Achieving large slip with superhydrophobic surfaces: Scaling laws for generic geometries.<br />
Physics <strong>of</strong> Fluids, 19(12):123601, 2007.<br />
Using the γ-Reθ-model for simulating, quantifying and delaying transition on dolphin<br />
geometries<br />
Donald Riedeberger, Dina-Marie Zimmermann, Ulrich Rist (<strong>Universität</strong> Stuttgart) Schedule<br />
Simulation <strong>of</strong> laminar to turbulent transition in finite volume CFD codes has recently seen some<br />
interesting new approaches regarding modelling the underlying process. The set <strong>of</strong> the Reynolds<br />
Averaged Navier-Stokes equations has been extended by two transport equations <strong>of</strong> the γ-Reθmodel<br />
[1] that uses empirical correlations to determine transition onset and blends in an underlying<br />
eddy viscosity turbulence model. This local modelling approach <strong>of</strong>fers possibilities to manipulate<br />
the underlying transition onset - for example to indirectly account for damping mechanisms at<br />
the wall.<br />
In the present project the flow around a geometry <strong>of</strong> a common dolphin [2] was simulated<br />
in a low to moderate turbulence environment at varying free stream velocities. Although Gray’s<br />
paradox that suggested laminarization techniques on the dolphin skin was solved and compliant<br />
walls do not necessarily need to be present on the dolphin [3] studies on the dolphin flow remain<br />
<strong>of</strong> interest in regard to transition location and correlation with dermal structures [2]. Results<br />
are presented and evaluated regarding overall flow topology and transition location depending on<br />
Reynolds number and turbulence level.<br />
In a second step the empirical correlation for transition onset was manipulated to shift transition<br />
location downstream to assess possible benefits <strong>of</strong> turbulence damping capabilites in the<br />
dolphin skin - i.e. accounting for flow control mechanisms <strong>of</strong> a compliant wall. The results show,<br />
that the model is very much capable to support this kind <strong>of</strong> simulations. Comparing results at<br />
moderate turbulence intensities with and without a modified (i.e. delayed) transition location one<br />
can see that drag reduction potential is as high as 40 percent - mostly coming from skin friction<br />
reduction in the parts where flow is sustained laminar for a longer amount <strong>of</strong> body surface.<br />
Summarizing this talk will highlight the possibilities <strong>of</strong> the empirical transition model and its<br />
potential in accounting for effects influencing the transition process.
260 Section 13: Flow control<br />
[1] R. B. Langtry and F. R. Menter. Correlation-based transition modeling for unstructured parallelized<br />
computational fluid dynamics codes. AIAA JOURNAL, 47(12):28942906, (2009).<br />
[2] V. V. Pavlov, Dolphin skin as a natural anisotropic compliant wall. Institute <strong>of</strong> Physics<br />
Publishing: Bioinspiration & Biomimetics 1 3140, (2006).<br />
[3] F. E. Fish, The myth and reality <strong>of</strong> grays paradox: implication <strong>of</strong> dolphin drag reduction for<br />
technology. Bioinspiration & Biomimetics, 1(2):R17 R25, (2006).<br />
S13.2: Flow Control II Wed, 13:30–15:30<br />
Chair: Andre Thess S1|01–A04<br />
Turbulent Flow with Embedded Vortical Structures Induced by Vortex Generators<br />
in a Cascade<br />
Natalie Souckova, Vaclav Uruba (Czech Academy <strong>of</strong> Sciences) Schedule<br />
Vortex generators (VGs) are passive flow control devices that are widely used in both internal<br />
and external flow. VGs occur in many different configurations. The choice <strong>of</strong> the optimal VGs<br />
configuration for a particular case is still quite obscure. The way to make the selection <strong>of</strong> suitable<br />
actuators arrangement easier can lead through the comprehension <strong>of</strong> generated vortices behaviour.<br />
The vortical structures produced by several configurations <strong>of</strong> vortex generators cascade have<br />
been studied to better understand the influence <strong>of</strong> spacing between pairs <strong>of</strong> VGs and vortex generator<br />
shape on the generated vortices behaviour. The used vane type VGs were integrated in<br />
straight channel so that they were submerged in the boundary layer. The turbulent flow affected<br />
by VGs has been examined by means <strong>of</strong> Stereoscopic Particle Image Velocimetry technique in<br />
several cross-sections downstream <strong>of</strong> VGs.<br />
Reactive control <strong>of</strong> spatially developing turbulent boundary layer<br />
Alexander Stroh, René Simon, George Khujadze (TU <strong>Darmstadt</strong>), Yosuke Hasegawa (TU <strong>Darmstadt</strong>;<br />
University <strong>of</strong> Tokyo), Bettina Frohnapfel, Martin Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
Reduction <strong>of</strong> losses caused by turbulent skin friction drag is <strong>of</strong> great economical and ecological<br />
interest. One <strong>of</strong> the promising turbulence control strategies is a reactive control, where instantaneous<br />
flow field information captured by sensors is used in order to determine actuator operation.<br />
Such control schemes exhibit high energy gain due to low power consumption. Although most<br />
previous control schemes have been assessed in fully developed turbulent channel flows, their<br />
applicability in spatially developing turbulent flows are not fully investigated.<br />
We focus on opposition control proposed by [1] as a representative reactive control scheme.<br />
The investigation is performed using direct numerical simulations <strong>of</strong> a turbulent boundary layer<br />
with zero pressure gradient in a Reynolds number range <strong>of</strong> ReΘ = 400 − 750. Opposition control<br />
is applied partially in the middle <strong>of</strong> domain between x ∗ = 250 and 350 covering 16.6% <strong>of</strong> the total<br />
domain length.<br />
The total drag reduction is estimated as 13.8% with net energy saving rate <strong>of</strong> 13.2% and<br />
local energy gain up to 23. It is found that the reduction <strong>of</strong> skin friction is mainly caused by the<br />
reduction <strong>of</strong> the turbulent term and the spatial development term appearing in the FIK-Identity<br />
[2]. Whereas the turbulent term is decreased due to a decrease <strong>of</strong> Reynolds shear stress, the<br />
spatial development term is mainly affected by the streamwise gradient <strong>of</strong> the streamwise velocity<br />
fluctuations, ∂u ′ u ′ /∂x, and streamwise gradient <strong>of</strong> streamwise mean velocity product, ∂UU/∂x.<br />
While ∂u ′ u ′ /∂x demonstrates essential deviations from the uncontrolled state in the beginning<br />
and at the end <strong>of</strong> the control area, ∂UU/∂x shows a decrease over the entire control area.
Section 13: Flow control 261<br />
In the presentation we will report the influence <strong>of</strong> control area length on the control performance<br />
and on the flow state in the recovery region.<br />
[1] Choi, H., Moin, P. & Kim, J., Active turbulence control for drag reduction in wall-bounded<br />
flows. J. Fluid Mech. 262, (1994), 75 - 110.<br />
[2] Fukagata, K., Iwamoto, K. & Kasagi, N., Contribution <strong>of</strong> Reynolds stress distribution to the<br />
skin friction in wall-bounded flows. Phys. Fluids 14, (2002) L73 - L76.<br />
Rotation-Symmetric Reference Geometries for Energyefficient Flow Around Bodies<br />
Michael Quarti, Andreas Gottlieb, Karl Bühler, Gerhard Kachel (Hochschule Offenburg) Schedule<br />
Topology optimization is used to optimize problems <strong>of</strong> flow around bodies and problems <strong>of</strong> guided<br />
flow. Within the context <strong>of</strong> research, optimization criteria are developed to increase the energy<br />
efficiency <strong>of</strong> these problems [1,2,3,4]. In order to evaluate the new criteria in respect to the<br />
increasing <strong>of</strong> energy efficiency, reference bodies for different Reynolds numbers in combination<br />
with given design space limitations are needed. Therefore, an optimal body at Reynolds number<br />
against 0 was analytically determined by Bourot [5]. At higher Reynolds numbers, in the range<br />
<strong>of</strong> laminar and turbulent flows, no analytical solution is known. Accordingly, reference bodies are<br />
calculated on the basis <strong>of</strong> CFD calculations at three technical relevant Reynolds numbers (1.000,<br />
32.000, 100.000) in combination with parameter optimization. The cross section <strong>of</strong> the bodies is<br />
described by a parameterized model.<br />
To get the optimal body, a parameter optimization, is used to optimize with regard to the friction<br />
loss and pressure loss in order to minimize the total loss (cw-value). The result is an optimal<br />
parameter constellation, depending on the Reynolds number. Within the results, it is possible to<br />
generate the optimal geometries. The identified characteristics <strong>of</strong> the flow field around the bodies<br />
are used as base for new optimization criterias.<br />
[1] K. Bühler, G. Kachel, and A. Gottlieb, Von der umströmten Scheibe zur optimierten Körperform,<br />
in: FB HS Offenburg. - 2010, 75-77 (2011).<br />
[2] A. Gottlieb, A. Strobel, and M. Stephan, Anwendung der Topologieoptimierung für strömungsführende<br />
Bauteile im Fahrzeugentwicklungsprozess, in: VDI-Tagungsband 2107: SIMVEC<br />
Berechnung und Simulation im Fahrzeugbau, (2010).<br />
[3] C. Hinterberger and M. Olesen, Automatic Geometry Optimization <strong>of</strong> Exhaust Systems<br />
Based on Sensitivities Computed by a Continuous Adjoint CFD Method in OpenFOAM,<br />
in: General emissions, (SAE International, Warrendale and PA, 2010).<br />
[4] F. Klimetzek, J. Paterson, and O. Moos, AutoDuct: topology optimization for fluid flow, in: 1.<br />
Konferenz für Angewandte Optimierung in der Virtuellen Produktentwicklung, (FE-Design<br />
GmbH, Karlsruhe, 2006).<br />
[5] J. M. Bourot, Journal <strong>of</strong> Fluid Mechanics 65(03), 513-515 (1974).<br />
Boundary layer simulations <strong>of</strong> turbulent flow over drag reducing surfaces<br />
Elfriede Friedmann (<strong>Universität</strong> Heidelberg) Schedule<br />
We are interested in passive turbulent flow control by manipulating the boundary layer <strong>of</strong> turbulent<br />
flow using tiny microstructures. Direct Numerical Simulations (DNS) <strong>of</strong> fully developed
262 Section 13: Flow control<br />
turbulent flows are very time consuming if one would like to resolve both: the turbulence and the<br />
microstructures. The focus <strong>of</strong> our work lies on model reduction and on high quality numerical<br />
methods needed for precise drag calculations. Following the boundary layer theory <strong>of</strong> Prandtl and<br />
Schlichting, we will present a model for the viscous sublayer (steady Navier-Stokes equations) and<br />
for the buffer layer (unsteady Navier-Stokes equations) which we use for drag predictions. In the<br />
steady case flow characteristics can be calculated with less numerical effort using homogenization<br />
theory. Applying the results <strong>of</strong> [6], we can replace the boundary layer model on rough surfaces<br />
(microscopic model) by the so-called homogenized model (macroscopic model) with smooth surface.<br />
The solution <strong>of</strong> the effective equations can be given analytically and the influence <strong>of</strong> the<br />
roughness are calculated from an auxiliary problem resulting from the homogenization process.<br />
The complexity <strong>of</strong> this auxiliary problem depends on the shape <strong>of</strong> the roughness. For universal<br />
structures a three-dimensional Stokes problem with an additional jump condition on the interface<br />
must be solved in a periodic cell domain. For riblets, only a two-dimensional Laplace problem<br />
with this jump condition in the solution must be solved. We will validate the drag prediction with<br />
this reduced model with the drag resulting from the microscopic model on non-optimal riblets and<br />
pimpels. In [3], where an optimization problem for such structures was solved, we find shapes with<br />
higher contribution to drag reduction. In general, the contribution here is small because the steady<br />
situation deals with small structures within the viscous sublayer. An unsteady model reaching<br />
inside the buffer layer <strong>of</strong> the turbulent boundary layer was developed to consider the higher and<br />
more relevant structures for drag reduction. Initial and boundary conditions were provided here<br />
from turbulent smooth channel flow simulations (Center <strong>of</strong> Smart Interfaces, <strong>Darmstadt</strong>, [9]. We<br />
will present DNS <strong>of</strong> the boundary layer models over riblets and pimpels which are performed with<br />
the s<strong>of</strong>tware Gascoigne [5] developed in Rolf Rannachers group based on Finite Elements. With<br />
the high quality numerical methods implemented in this s<strong>of</strong>tware like adaptive mesh refinement,<br />
multigrid algorithms and error control [2], [8] and by using isoparametric elements for the boundary<br />
approximation [3], we can resolve the rough boundary well and provide drag calculations<br />
with an accuracy per mill [7]. Our research will allow us a small contribution to the boundary<br />
layer theory concerning the comparability <strong>of</strong> the different (but non-optimal) microstructures.<br />
Mathematics Subject Classification 2000 (MSC 2000): 76D05, 76D10, 35B27<br />
[1] Bechert, D.W. and Bruse, M. and Hage, W., Experiments with three-dimensional riblets as<br />
an idealized model <strong>of</strong> shark skin, Experiments in Fluids, 28:403-412, 2000.<br />
[2] Becker, R., Rannacher, R., An optimal control approach to a posteriori error estimation in<br />
finite element methods, Acta Numerica 10, 1102, 2001.<br />
[3] Friedmann, E., Richter, T., Optimal microstructures. Drag reducing mechanism <strong>of</strong> riblets, J.<br />
<strong>of</strong> Math. Fluid Mech., 13 (3), 429-447, 2010.<br />
[4] Friedmann, E., The optimal shape <strong>of</strong> riblets in the viscous sublayer, J. <strong>of</strong> Math. Fluid Mech.,<br />
12(2), 243-265, 2010.<br />
[5] GASCOIGNE, High Performance Adaptive Finite Element Toolkit, URL: http://www.<br />
numerik.uni-kiel.de/~mabr/gascoigne/.<br />
[6] Jäger, W. and Mikelić, A., Couette flows over a rough boundary and drag reduction, Communications<br />
in Mathematical Physics, Springer, 232(3), 429-455, 2003.<br />
[7] Maier M., Simulation von Grenzschichtströmungen über Ribletstrukturen, diploma thesis,<br />
Heidelberg University, 2011.
Section 13: Flow control 263<br />
[8] Rannacher, R., Adaptive finite element discretization <strong>of</strong> flow problems for goal-oriented model<br />
reduction, Computational Fluid Dynamics Review 2010, (M. M. Hafez, K. Oshima, D. Kwak,<br />
eds), 51-70, World Scientific, 2010.<br />
[9] Stroh, A., Frohnapfel, B., Hasegawa, Y., Kasagi, N., Tropea, C., The influence <strong>of</strong> frequencylimited<br />
and noise-contaminated sensing on reactive turbulence control schemes, The Seventh<br />
International Symposium on Turbulence and Shear Flow Phenomena, Ottawa, Canada,<br />
2011.<br />
On the flow resistance <strong>of</strong> wide surface structures<br />
Gerti Daschiel, Tobias Baier, Jürgen Saal, Bettina Frohnapfel (TU <strong>Darmstadt</strong>) Schedule<br />
It has been shown that riblet-mounted surfaces can reduce the skin-friction drag by up to 10%<br />
compared to flat surfaces in turbulent channel flows [3]. In the laminar regime, however, the use<br />
<strong>of</strong> these surface geometries was found to result in drag increase [2]. Using a variational principle<br />
for the surface shape, Pironneau et al. [4] were able to show analytically that in the laminar case<br />
benefits can only be expected if the surface structures are wide enough compared to the channel<br />
height, in particular if the ratio obeys the condition l/L > π/z where z ≈ 1.2 is the root <strong>of</strong><br />
1 − x tanh x (2l: width <strong>of</strong> the structure, 2L: mean channel height).<br />
In the present investigation the curved optimum surface shape found numerically by Pironneau<br />
et al. is analysed further. Using an analogy between structural mechanics and fluid mechanics,<br />
namely the analogy between torsion <strong>of</strong> beams and fully developed laminar flow in ducts (the governing<br />
equation in both cases is Poissons equation), the pressure drop, and thus the skin-friction<br />
drag, arising from various curved structures can be calculated using Saint Venants principle [1].<br />
In this respect the analysis concentrates on surface modifications described by a trigonometric<br />
function <strong>of</strong> the form x2 = ± ((a/2)cos(πx3/l) + 2b) with b + a/2 = L. Based on this approach<br />
the impact on flow resistance for the variation <strong>of</strong> all parameters determining the trigonometric<br />
structure is taken into account. Drag is found to be reduced up to about 50% compared to the<br />
flow through a rectangular channel <strong>of</strong> the same cross section and the same width (here: 2l) for<br />
a certain range <strong>of</strong> parameters. In addition, numerical simulations <strong>of</strong> the flow in the structured<br />
channels are performed. Currently, these simulations are extended to higher Reynolds numbers<br />
in order to also study the drag reduction potential <strong>of</strong> these wide surface structures in turbulent<br />
flows.<br />
[1] M. Bahrami, M. Yovanovich, J. Culham, A novel solution for pressure drop in singly connected<br />
microchannels <strong>of</strong> arbitrary cross-section, International Journal <strong>of</strong> Heat and Mass Transfer<br />
50 (2007), 2492 – 2502.<br />
[2] H. Choi, P. Moin, and J. Kim, On the effect <strong>of</strong> riblets in fully developed laminar channel<br />
flows, Physics <strong>of</strong> Fluids3 (1991), 1892 – 1896.<br />
[3] H. Choi, P. Moin, J. Kim, Direct numerical simulation <strong>of</strong> turbulent flow over riblets, Journal<br />
<strong>of</strong> Fluid Mechanics 225 (1993), 503 – 539.<br />
[4] O. Pironneau, G. Arumugam, On riblets in laminar flow, Control <strong>of</strong> boundaries and stabilization<br />
(1989), 51 – 65.
264 Section 13: Flow control<br />
Assessment <strong>of</strong> Flow Control Techniques in Terms <strong>of</strong> Time and Energy Savings<br />
Bettina Frohnapfel, Yosuke Hasegawa (TU <strong>Darmstadt</strong>), Maurizio Quadrio (Politecnico di Milano)<br />
Schedule<br />
The performance <strong>of</strong> drag reducing flow control techniques for internal flows is customarily evaluated<br />
by either measuring the flow rate achieved with a fixed pressure drop or determining the<br />
pressure drop needed to drive the flow at a fixed flow rate. The obtained results are typically<br />
presented in a plot <strong>of</strong> skin friction drag (i.e. pressure drop) versus bulk Reynolds number (i.e.<br />
flow rate) where either the reduction <strong>of</strong> skin friction drag at fixed Reynolds number or the increase<br />
<strong>of</strong> Reynolds number at a fixed skin friction drag represent successful control. In this conventional<br />
cf − Re−plot the two key aspects <strong>of</strong> practical fluid transport systems, namely the time required<br />
to transport a given amount <strong>of</strong> fluid over a certain distance and the energy required to realize<br />
this transport, cannot be viewed independently. This mainly stems from the fact that the energy<br />
consumption is directly related to the product <strong>of</strong> flow rate and pressure drop. Based on the idea<br />
to put potential energy and time savings in the focus <strong>of</strong> flow control evaluation we derive two<br />
dimensionless parameters which quantify the energy consumption and the transportation time for<br />
flows through an arbitrary duct independently. These parameters span a novel evaluation plane<br />
that allows reevaluating the performance <strong>of</strong> passive and active drag reduction techniques in one<br />
framework also including the energy expenditure to run active control. This novel evaluation plane<br />
allows including application-dependent cost functions such that the optimal control strategy<br />
for a given application can be determined.<br />
S13.3: Flow Control III Wed, 16:00–18:00<br />
Chair: Stefan Odenbach S1|01–A04<br />
Experimental Investigation <strong>of</strong> magnetoactive composites<br />
Thomas Gundermann, Dmitry Borin, Stefan Günther, Stefan Odenbach (TU Dresden) Schedule<br />
Magneto-switchable composite materials consisting <strong>of</strong> a polymer matrix and magnetizable components<br />
<strong>of</strong>fer enormous potential for innovation. Such material systems enable a targeted response<br />
to external loads and can be used advantageously as adaptive structures. By applying a magnetic<br />
field, the viscoelastic and dynamic mechanical properties can be active and reversible changed.<br />
The main goal <strong>of</strong> this study was to investigate the mechanical properties <strong>of</strong> these composites<br />
under the influence <strong>of</strong> an external magnetic field using a compression test unit. For this purpose<br />
a dynamic table-top test machine with a servopneumatic drive has been equipped with a<br />
fixture based on electromagnets combined with permanent magnets. Furthermore, studies were<br />
undertaken with a micro-computed tomography system which provides information about the<br />
internal structure under the influence <strong>of</strong> a magnetic field. For the experimental investigations<br />
samples based on the carbonyl iron particles have been used. The particles were dispersed in<br />
a polymeric matrix and after the cross-linking procedure they were limited in their movement,<br />
but stable towards sedimentation, forming the elastic magnetoactive composite. Combinations <strong>of</strong><br />
the mechanical tests with microstructural observations represent the fundamental basis for the<br />
understanding <strong>of</strong> the behavior <strong>of</strong> magneto-switchable composite materials.<br />
This project is funded by the European Union (ERDF) and the Free State <strong>of</strong> Saxony.<br />
Thermal conductivity measurements in magnetic fluids<br />
Martin Krichler, Stefan Odenbach (TU Dresden) Schedule<br />
Material properties like viscosity and sound propagation in magnetic fluids are known to depend<br />
on external magnetic fields due to structure formation <strong>of</strong> the magnetic particles. In this experimental<br />
study thermal transport behaviour is investigated on the basis <strong>of</strong> thermal conductivity
Section 13: Flow control 265<br />
measurements. Therefore an improved measuring technique - a plane heat source method - is used<br />
for thermal conductivity measurements in magnetic fluids. Initially four magnetic fluid samples<br />
varying in particle interaction and Brownian motion behaviour are selected for the fundamental<br />
investigation <strong>of</strong> the effect <strong>of</strong> chain-like structure formation on thermal behaviour. Thermal<br />
conductivity is measured as a function <strong>of</strong> strength and direction <strong>of</strong> an external magnetic field<br />
relative to heat flux. Unlike former experimental investigations our results show consistency with<br />
theoretical predictions.<br />
The anisotropy <strong>of</strong> the magnetoviscous effect in ferr<strong>of</strong>luids with interparticle interactions<br />
J. Linke, M. Gerth-Noritzsch, D. Y. Borin, S. Odenbach (TU Dresden) Schedule<br />
Ferr<strong>of</strong>luids are colloidal suspensions <strong>of</strong> coated magnetic nanoparticles in a carrier liquid. The viscosity<br />
and the flow behaviour <strong>of</strong> ferr<strong>of</strong>luids may be tuned by an externally applied magnetic field<br />
which opens a range <strong>of</strong> interesting technical applications. The change <strong>of</strong> the viscosity is caused<br />
by two effects. In highly dilute ferr<strong>of</strong>luids, the free rotation <strong>of</strong> the magnetic particles in the flow is<br />
slowed down by their magnetic torque. This causes a raise in the viscosity, the so called rotational<br />
viscosity. In concentrated ferr<strong>of</strong>luids on the other hand, the dipole-dipole interaction between the<br />
particles supports chain-like microstructures that obstruct the flow and increase the viscosity.<br />
This effect is known as the magnetoviscous effect (MVE) [1]. Both effects are anisotropic; however,<br />
the majority <strong>of</strong> experimental investigations <strong>of</strong> the MVE have been carried out with only one<br />
fixed orientation <strong>of</strong> the magnetic field.<br />
In the present work, pressure flow viscometers with a capillary and a slit geometry have been<br />
used to access the viscosity coefficients for three orientations <strong>of</strong> the magnetic field, i.e. parallel<br />
and perpendicular to the direction <strong>of</strong> flow, as well as parallel to the vorticity <strong>of</strong> the flow. The MVE<br />
has been measured in cobalt-based ferr<strong>of</strong>luids with strong interparticle interactions [2]. In these<br />
ferr<strong>of</strong>luids the change in viscosity is more than a magnitude higher than the maximum rotational<br />
viscosity. This supports the theory <strong>of</strong> structure formation due to dipole-dipole interactions. The<br />
MVE for the field direction perpendicular to the flow is lower than the MVE for the parallel direction<br />
due to shear-induced disintegration <strong>of</strong> the chain-like structures. Furthermore, it has been<br />
investigated how this anisotropy <strong>of</strong> the MVE, together with the flow pr<strong>of</strong>ile, changes by varying<br />
the strength <strong>of</strong> the applied magnetic field, and the results are compared with microstructural<br />
simulations.<br />
We gratefully acknowledge the financial support <strong>of</strong> our research by the Deutsche Forschungsgemeinschaft<br />
(DFG grant Od18-18).<br />
[1] S. Odenbach, Magnetoviscous Effects in Ferr<strong>of</strong>luids, Lecture Notes in Physics (2002), Springer.<br />
[2] M. Gerth-Noritzsch, D. Y. Borin, S. Odenbach, Anisotropy <strong>of</strong> the magnetoviscous effect in ferr<strong>of</strong>luids<br />
containing nanoparticles exhibiting magnetic dipole interaction, J. Phys.: Condens.<br />
Matt. 23 (2011), 346002.<br />
Investigations on a branched tube model in magnetic drug targeting systematic<br />
measurements and simulation<br />
K. Gitter, S. Odenbach (TU Dresden) Schedule<br />
Magnetic drug targeting has been established as a promising technique for tumour treatment. Due<br />
to its high targeting efficiency unwanted side effects are considerably reduced, since drug-loaded
266 Section 13: Flow control<br />
nanoparticles are concentrated within a target region due to the influence <strong>of</strong> a magnetic field. In<br />
order to contribute to the understanding <strong>of</strong> basic phenomena experiments on a half-Y-branched<br />
glass tube model as a model-system for a blood vessel supplying a tumour were performed. As<br />
a result <strong>of</strong> measurements, novel drug targeting maps, combining e.g. the magnetic volume force,<br />
the position <strong>of</strong> the magnet and the net amount <strong>of</strong> targeted nanoparticles were presented. In a first<br />
targeting-map, which summarizes results for 63 magnet positions, the concentration <strong>of</strong> the injected<br />
ferr<strong>of</strong>luid is 2.95vol. Up to 97 <strong>of</strong> the nanoparticles were successfully targeted into the chosen<br />
branch; however, the region where yield was considerable is rather small. A high concentration<br />
<strong>of</strong> injected ferr<strong>of</strong>luid brings the danger <strong>of</strong> accretion in the tube. It is shown that an increase in<br />
magnetic volume force does not necessarily lead to a higher amount <strong>of</strong> targeted nanoparticles. In<br />
a second targeting-map the concentration <strong>of</strong> injected ferr<strong>of</strong>luid is reduced to 0.14vol. At a first<br />
glance the result with low concentration is promising, since the danger <strong>of</strong> accretion is avoided.<br />
Nevertheless, one has to consider, that, unless the magnetic volume force in the branch-point<br />
was provided in the necessary strength, an application would not be successful. The current<br />
focus is a finite-element simulation based on the considered setup and artery-model. The fluid<br />
flow is described by the Navier-Stokes equations, the magnetic field is derived from Maxwells<br />
equations and mass flux is given by the diffusion equation. The magnetic volume force acting on<br />
a volume <strong>of</strong> magnetic fluid combines the magnet and the ferr<strong>of</strong>luid data and is proportional to<br />
the field dependent magnetisation and the gradient <strong>of</strong> the field strength. The diffusion equation<br />
allows the implementation <strong>of</strong> concentration-dependent magnetic volume force and viscosity. In<br />
the experiments, the model, the injection-procedure and the ferr<strong>of</strong>luid were chosen close to the<br />
parameters <strong>of</strong> a medical application in order to allow a transfer <strong>of</strong> the results to future medical<br />
investigations.<br />
Creep experiments on ferr<strong>of</strong>luids with clustered nanoparticles<br />
Dmitry Borin (TU Dresden), Andrey Zubarev (Ural State Univeristy Ekaterinburg), Stefan Odenbach<br />
(TU Dresden) Schedule<br />
Even a small amount <strong>of</strong> magnetite nanoparticles larger than 12 nm gives rise to a variety <strong>of</strong><br />
interesting changes <strong>of</strong> the rheological behavior <strong>of</strong> ferr<strong>of</strong>luids in applied magnetic elds [1]. Recently<br />
[2], we observed the effect <strong>of</strong> the slow relaxation <strong>of</strong> the rheological properties <strong>of</strong> a ferrouid with<br />
clustered iron nanoparticles under joint action <strong>of</strong> shear ow and magnetic eld. In the present study<br />
we invistigate the inverse creep for this ferr<strong>of</strong>luid experimentally as well as from a theoretical point<br />
<strong>of</strong> view. With a magnetic field applied to the fluid, the shear force has been suddenly removed<br />
and the subsequent relaxation <strong>of</strong> the shear stress has been measured. The relaxation time can<br />
reach several minutes analogous to [2] and depends on magnetic field strength and initial shear<br />
rate. Furthermore, an <strong>of</strong>fset in the shear stress after removing the shear force is observed and<br />
can be attributed to the yield stress in ferr<strong>of</strong>luids [3]. The proposed theoretical model tries to<br />
explain the observed effects on the basis <strong>of</strong> the formation <strong>of</strong> long chains <strong>of</strong> magnetic particles in<br />
the ferr<strong>of</strong>luid under action <strong>of</strong> the magnetic field.<br />
[1] S. Odenbach, Magntoviscous effect in ferr<strong>of</strong>luids, Springer Lecture Note in Physics m71,<br />
Berlin, Heidelberg, Springer-Verlag (2002)<br />
[2] D. Borin et al, Ferrouid with clustered iron nanoparticles: slow relaxation <strong>of</strong> rheological<br />
properties under joint action <strong>of</strong> shear ow and magnetic eld, J. Magn. Magn. Mater. 323<br />
(2011), 1273–1277<br />
[3] H. Shahnazian and S. Odenbach, Rheological investigations <strong>of</strong> ferr<strong>of</strong>luids with a shear stress<br />
controlled rheometer, J. Phys.: Condens. Matter 20 (2008), 204137
Section 13: Flow control 267<br />
Determining <strong>of</strong> Velocity Fields During Real and Experimental Simulated Beer Fermentations<br />
by UDV and LDA<br />
Kai Böttcher, Heiko Meironke (Fachhochschule Stralsund) Schedule<br />
Beer fermentation is a very complex process, especially in the fluid-mechanical and the biochemical<br />
point <strong>of</strong> view. Our aim is to optimize the fermentation by flow control, which requires<br />
quantities <strong>of</strong> data. The applied velocity measuring techniques should be non-invasive to ensure<br />
that neither the flow nor the fermentation in the green beer gets influenced. Therefore, an Ultrasonic<br />
Doppler Velocimetry (UDV) system is used to determine velocity fields with 128 measuring<br />
points. It works in the turbid fluid with the existing yeast cells as tracer particles and can be<br />
applied easily to the industrial scale.<br />
For the validation <strong>of</strong> CFD-codes and the better understanding <strong>of</strong> measurements and flow processes,<br />
model fluids are used. They can be adapted to real fluid properties like density and viscosity<br />
and allow measurements with Laser Doppler Anemometry (LDA). Another advantage over the<br />
real fluid is their fixed composition, which leads to negligible natural variations.<br />
All experiments are performed in a 270 liter fermenter. Besides the real process, measurements<br />
through optical access points and the simulation <strong>of</strong> fermentations with CO2 and heat emission<br />
are enabled. Eight individually controllable cooling zones are used as thermal actors. Resulting<br />
changes in boundary conditions induce temperature gradients and hence allow to control the flow<br />
inside the tank.<br />
This work deals with the experimental setup and the results on the one hand and a comparison<br />
between real and simulated fermentations on the other hand. Special attention is given to investigations<br />
<strong>of</strong> the multi-phase flow inside the vessel and the effects <strong>of</strong> changing constraints. The<br />
usability <strong>of</strong> UDV measurement techniques is the key benefit in that case, because it can be used<br />
in green beer and model fluids and does not influence the flow.<br />
S13.4: Flow Control IV Thu, 13:30–15:30<br />
Chair: Bettina Frohnapfel S1|01–A04<br />
Non-sinusoidal wall oscillation for drag reduction<br />
A. Cimarelli (University <strong>of</strong> Bologna), B. Frohnapfel (TU <strong>Darmstadt</strong>), Y. Hasegawa (TU <strong>Darmstadt</strong>;<br />
University <strong>of</strong> Tokyo), E. De Angelis (University <strong>of</strong> Bologna), M. Quadrio (Politecnico di<br />
Milano) Schedule<br />
The control <strong>of</strong> wall-bounded turbulent flows with the aim <strong>of</strong> reducing the wall-shear stress is an<br />
important and challenging topic in modern fluid mechanics. Indeed, such a reduction has very<br />
important beneficial effects for engineering flow systems. One prominent control technique which<br />
allows to achieve a significant reduction <strong>of</strong> turbulent drag is based on the modification <strong>of</strong> wall<br />
turbulence by the cyclic spanwise movement <strong>of</strong> the wall, [1]. Despite the studies available in the<br />
literature, there are a number <strong>of</strong> issues related to drag reduction properties <strong>of</strong> the oscillating wall<br />
that have not yet received a definite answer. For example, it is well known that the frequency and<br />
the amplitude <strong>of</strong> the oscillation play a first-order role in determining the amount <strong>of</strong> the turbulent<br />
drag reduction rate but the effects <strong>of</strong> the shapes <strong>of</strong> the wall oscillations are still not determined.<br />
Indeed, all the attemps carried out towards achieving a reduction <strong>of</strong> turbulent friction have used<br />
a sinusoidal shape for the spanwise oscillation <strong>of</strong> the wall. For that reasons, we investigate the<br />
drag reducing properties <strong>of</strong> non-sinusoidal wall oscillations. The present work aims at answering<br />
two related questions:<br />
• How do deviations from the sinusoidal wave shape - which might occur when trying to
268 Section 13: Flow control<br />
realize an oscillating wall in practice - influence the control performance?<br />
• Is it possible to obtain flow control performance superior to the sinusoidal wall oscillations<br />
with other oscillations shapes?<br />
The analysis <strong>of</strong> the non-sinusoidal wall oscillations is performed using direct numerical simulation<br />
data <strong>of</strong> a turbulent channel flow. The simulations are carried out with an highly accurate<br />
numerical code. The friction Reynolds number <strong>of</strong> the reference simulation without wall oscillation<br />
is Reτ = 200 and the computational domain is 6.67h×2h×3.33h. All simulations for the different<br />
boundary conditions <strong>of</strong> spanwise velocity at the walls are performed starting from the same initial<br />
condition <strong>of</strong> fully developed channel flow without wall oscillation.<br />
The obtained results illustrate the dependency <strong>of</strong> the drag reduction rate, R, and <strong>of</strong> the power<br />
spent to move the walls, Pin, with respect the shape <strong>of</strong> the wall motion. An analytical model<br />
based on the generalization <strong>of</strong> the laminar solution <strong>of</strong> the Stokes layer is derived which allows<br />
the a priori prediction <strong>of</strong> R and Pin for different wall motions in turbulent flows under certain<br />
constraints.<br />
[1] M. Quadrio, Drag reduction in turbulent boundary layers by in-plane wall motion, Phil.<br />
Trans. R. Soc. A 369 (2011), 1428 – 1442.<br />
Numerical Investigation <strong>of</strong> Vortex Generator Jets On The Trailing Edge Shroud <strong>of</strong><br />
Improved High-Lift Configuration<br />
Saqib Mahmood, Marcus Casper, Ingmar Hartung, Peter Scholz (TU Braunschweig) Schedule<br />
This paper focuses on numerical simulation <strong>of</strong> active flow control devices by means <strong>of</strong> vortex<br />
generator jets on the trailing edge shroud <strong>of</strong> improved high-lift configurations. The test case used<br />
for the numerical work is the DLR F-15 two-element high lift airfoil. The vortex generator jets<br />
produce longitudinal vortices within the boundary layer which suppresses the stalling <strong>of</strong> an airfoil.<br />
The numerical work has been carried out using the TAU-Code developed by German Aerospace<br />
Centre (DLR), which is a Compressible Finite Volume based unstructured solver. The effect <strong>of</strong> grid<br />
refinement is described in detail. Numerical results without active flow control are compared with<br />
experiments conducted at the Institute <strong>of</strong> Fluid Mechanics, <strong>Technische</strong> <strong>Universität</strong> Braunschweig.<br />
The numerical results agree well with experimental data by predicting trailing edge type stall.<br />
Stabilization <strong>of</strong> Laminar Boundary-Layer Flow using Dielectric Barrier Discharges<br />
Alexander Duchmann, Debora Gleice da Silva Del Rio Vieira, Sven Grundmann, Cameron Tropea<br />
(TU <strong>Darmstadt</strong>) Schedule<br />
Drag reduction <strong>of</strong> immersed bodies is <strong>of</strong> major importance to the aeronautical industry and is an<br />
expanding field <strong>of</strong> research. In this contribution the development <strong>of</strong> active flow control techniques<br />
is examined with the aim to retain the laminar flow state, and hence a reduction <strong>of</strong> skin friction<br />
drag.<br />
Dielectric Barrier Discharges (DBD) are used to delay laminar-turbulent transition initiated<br />
by Tollmien-Schlichting instabilities. An electric potential <strong>of</strong> several thousand Volts between two<br />
electrodes separated by a dielectric material leads to ionization <strong>of</strong> the surrounding air. Interaction<br />
between the resulting weakly ionized plasma and the electric force field causes an acceleration <strong>of</strong><br />
the fluid molecules close to the surface. This effect can be used to change the stability properties<br />
<strong>of</strong> the laminar boundary-layer flow and postpone the turbulent breakdown.
Section 13: Flow control 269<br />
The present study demonstrates that DBD actuators cannot only delay transition triggered<br />
by controlled disturbances, as shown by Grundmann et. al. [1], but are also effective in delaying<br />
natural transition. Transitional boundary-layer flow along a flat plate inside an open-circuit<br />
wind tunnel is experimentally investigated. A combination <strong>of</strong> hot-wire measurements and particle<br />
image velocimetry provides the time-resolved velocity distribution in wall normal and tangential<br />
direction. Integral boundary-layer quantities and statistical data enable an analysis <strong>of</strong> the transition<br />
process which is affected by the discharges. Linear stability theory is considered to analyze<br />
the stability characteristics <strong>of</strong> the boundary-layer flow with and without flow control [2]. Direct<br />
numerical simulations enable a close-up view <strong>of</strong> momentum coupling in the immediate vicinity <strong>of</strong><br />
the discharge and the impact on the flow stability.<br />
[1] S. Grundmann, C. Tropea, Experimental Damping <strong>of</strong> Boundary-Layer Oscillations using<br />
DBD Plasma Actuators, International Journal <strong>of</strong> Heat and Fluid Flow 30, (2009), 394–402.<br />
[2] A. Duchmann, A. Reeh, R. Quadros, J. Kriegseis, C. Tropea, Linear Stability Analysis for Manipulated<br />
Boundary-Layer Flows using Plasma Actuators, In: Seventh IUTAM Symposium<br />
on Laminar-Turbulent Transition, ISBN 978-90-481-3723-7.<br />
Phase-avaraged vortex train flow generated by plasma DBD actuator<br />
Pavel Procházka, Václav Uruba (Czech Academy <strong>of</strong> Sciences) Schedule<br />
The way how plasma actuator can generate wall-jet-like flow or train <strong>of</strong> periodical vortices depending<br />
on the generator setting will be shown. The high-frequency high-voltage AC is used for<br />
generation. Low-frequency modulation <strong>of</strong> the supply voltage is required to generate vortices. Data<br />
acquisition will be performed using time-resolved PIV technique. Phase-avaraging will be studied<br />
from two different perspectives. Firstly, sampling <strong>of</strong> phases will be ensured using trigger that is<br />
contained in the PIV s<strong>of</strong>tware and, secondly, phase-avaraged flow will be computed from two main<br />
modes <strong>of</strong> POD analysis. The generated flow patterns are to be applied for control <strong>of</strong> a boundary<br />
layer.<br />
Feedback-control <strong>of</strong> Tollmien-Schlichting waves and laminar-turbulent transition in<br />
a Blasius boundary layer<br />
Ulrich Rist (<strong>Universität</strong> Stuttgart) Schedule<br />
In a low-disturbances environment, laminar-turbulent transition starts with the amplification <strong>of</strong><br />
small-amplitude disturbances. Any disturbance can then be decomposed into a sum <strong>of</strong> Tollmien-<br />
Schlichting waves such that the initial (linear) development becomes predictable using linear<br />
stability theory (LST). The present talk will relate results <strong>of</strong> LST to features occurring in the<br />
flow field and thus try to clarify some misconceptions about Tollmien-Schlichting waves that exist<br />
in literature.<br />
Control <strong>of</strong> boundary-layer transition in the early stage relies on controlling either the amplitude<br />
or the growth <strong>of</strong> linear Tollmien-Schlichting waves. The present talk will address both paths: The<br />
wave-superposition principle for amplitude reduction, and feedback control for growth reduction.<br />
Here, feedback control connects actuation at the wall with the time-derivative <strong>of</strong> the wall shear<br />
(here I wanted to show a figure). 1<br />
Results <strong>of</strong> LST and direct numerical simulations (DNS) will be used to illustrate the basic<br />
mechanisms, the relative merits <strong>of</strong> each method and their limits. The wave-superposition principle<br />
1 The complete abstract with figure is here:<br />
http://www.iag.uni-stuttgart.de/people/ulrich.rist/<strong>GAMM</strong><strong>2012</strong>.pdf
270 Section 13: Flow control<br />
is shown to be very sensitive to phase differences between the target wave and the control wave.<br />
Since it is by definition based on linear superposition it can only work in the linear regime. In the<br />
non-linear regime where finite-amplitude effects come into play and where different disturbance<br />
modes interact with each other it is better to use the feedback control scheme. The underlying<br />
mechanisms which have been identified by LST and DNS for both, the linear and the non-linear,<br />
regimes will be discussed.<br />
Advancing active wave cancellation using plasma actuators for in-flight transition<br />
control<br />
A. Kurz, S. Grundmann, C. Tropea (TU <strong>Darmstadt</strong>), Nikolas Goldin, Rudibert King (TU Berlin)<br />
Schedule<br />
Active flow control has increasingly attracted attention over the past years and has led to improvements<br />
in aerodynamic performance, like enhanced lift or reduced drag.<br />
Transition to turbulence in low Reynolds number flows is usually triggered by two-dimensional,<br />
wave like velocity fluctuations, commonly known as Tollmien-Schlichting (TS) waves. Once initiated,<br />
the amplitude <strong>of</strong> the TS waves grows until breakdown to turbulence occurs. If the amplitude<br />
<strong>of</strong> these initial waves can be lowered at an early stage, it is possible to delay the transition, and,<br />
for example, lower the drag <strong>of</strong> the aerodynamic surface.<br />
In an attempt to advance active wave cancellation (AWC) using plasma actuators one step<br />
closer to real aerodynamic applications, an existing experimental setup has been adapted to<br />
a testing platform capable <strong>of</strong> examining the feasibility <strong>of</strong> free-flight operation. It consists <strong>of</strong> a<br />
wing glove that can be used as a sleeve on the wing <strong>of</strong> a full-sized Grob G109 motorized glider,<br />
available at the <strong>Technische</strong> <strong>Universität</strong> <strong>Darmstadt</strong>. The hollow carbon-fiber composite design<br />
allows for the installation <strong>of</strong> measurement equipment, sensors and actuators inside the wing<br />
glove, without altering the structural integrity <strong>of</strong> the aircraft. Several further constraints have to<br />
be addressed in order to achieve the goal <strong>of</strong> sucessful in-flight AWC experiments. This includes not<br />
only the development <strong>of</strong> lightweight high-voltage power supplies, which allow for a precise control<br />
<strong>of</strong> the force production, but also the application <strong>of</strong> more sophisticated, fast closed-loop control<br />
algorithms. In collaboration with the <strong>Technische</strong> <strong>Universität</strong> Berlin a robust extremum-seeking<br />
controller and in addition, a FIR-Model, which is adapted online by a filtered-xLMS approach,<br />
has been implemented on a dSPACE system and tested in the wind tunnel. Both controllers were<br />
applied sucessfully for the first time in combination with plasma actuators on a full size airfoil<br />
geometry.<br />
Another set <strong>of</strong> experiments has been conducted using an amplitude modulation for the body<br />
force originating directly from the high frequency carrier wave driving the plasma actuator. This<br />
approach exploits the fact that the force production is highly unsteady at the actuator driving<br />
frequency and opens up the possibility to operate the plasma actuator directly at TS wave frequency.<br />
The results demonstrate that a substantial increase <strong>of</strong> the achievable forcing frequency,<br />
and with it <strong>of</strong> the flight Reynolds number, will be possible.<br />
S13.5: Flow Control V Thu, 16:00–18:00<br />
Chair: Ulrich Rist S1|01–A04<br />
Flow rate measurements in turbulent liquid metal channel flow using time-<strong>of</strong>-flight<br />
Lorentz force velocimetry<br />
Dandan Jian, Christian Karcher (TU Ilmenau) Schedule<br />
Non-contact flow control and flow measurements in hot and aggressive metal melts are big challenges<br />
in metallurgical applications. For instance, during the production <strong>of</strong> secondary aluminum,
Section 13: Flow control 271<br />
the primary melt flows in a channel from a melting furnace to a holding furnace. To determine<br />
both the scrap yield rate during the melting process and the exact amount <strong>of</strong> alloying elements to<br />
be put into the holding furnace during charge makeup, exact measurement <strong>of</strong> global flow rate in<br />
the channel is crucial for process control. Lorentz force velocimetry (LFV) is an electromagnetic<br />
measurement technique to meet these challenges. It is based on measuring the Lorentz force acting<br />
on a magnet system when liquid metal flow is crossing the field lines that are stretched by the magnet<br />
system. The respective measurement device, called Lorentz force flow meter, mainly consists<br />
<strong>of</strong> such a magnet system equipped with a digital force sensor. According to the basic principles<br />
<strong>of</strong> magnetohydrodynamics, the recorded force is proportional to the flow rate, the square <strong>of</strong> the<br />
characteristic amplitude <strong>of</strong> the applied magnetic field, and the electrical conductivity <strong>of</strong> the melt.<br />
However, in application the conductivity is <strong>of</strong>ten unknown or changes in time due to its strong<br />
dependence on both temperature and composition <strong>of</strong> the melt. In the present paper we describe<br />
an extended method called time-<strong>of</strong>-flight Lorentz force velocimetry (t<strong>of</strong> LFV). Here, two identical<br />
flow meters are arranged in a certain distance D one behind the other. In this case, flow rate can<br />
be determined by just cross-correlating the two force signals recorded by the flow meters. In more<br />
detail, we measure the transit time τ <strong>of</strong> a tagging signal that is transported by the flow with a<br />
certain velocity U between the flowmeters. In this case the flow rate can easily be determined<br />
using the simple relation Q = cUA = cAD/τ, where A is the cross-section <strong>of</strong> channel and c is a<br />
calibration constant. Hence the measurement becomes independent <strong>of</strong> any fluid property data or<br />
magnetic field characteristics.<br />
Within this context we study experimentally and numerically turbulent liquid metal channel<br />
flow affected by two localized magnetic fields. The flow rate measurements are conducted in the<br />
model test stand EFCO (electromagnetic flow control channel) using the low-melting test melt<br />
GaInSn as a test melt. EFCO is a closed channel with rectangular cross section <strong>of</strong> height and width<br />
equal to H ×W = 80×10mm 2 . The overall length and breadth <strong>of</strong> the test stand are L×B = 860×<br />
350mm 2 . The channel walls consist <strong>of</strong> electrically insulating plexiglass. The channel is equipped<br />
with two Lorentz force flow meters each <strong>of</strong> which consisting <strong>of</strong> two permanent magnets that<br />
generate a localized spanwise magnetic field. Attached to the magnetic field is a digital strain gage<br />
that records the Lorentz force acting in the streamwise direction. Tagging signals are produced<br />
by a cylindrical obstacle submerged into the flow. The flow is driven by an electromagnetic pump<br />
(EMP) on basis <strong>of</strong> rotating permanent magnets mounted on two disks. The disks are put into<br />
rotation by a frequency-controlled electrical motor. Upon controlling the rotation frequency f <strong>of</strong><br />
the pump, we adjust the Reynolds number <strong>of</strong> the flow. At the highest achievable frequency <strong>of</strong><br />
f = 25Hz, the corresponding Reynolds number is Re = 1.6e4. Hence, we are in the regime <strong>of</strong><br />
turbulent liquid metal channel flow. During the model experiments we additionally measure the<br />
pressure produced by the EMP, velocity pr<strong>of</strong>iles using Ultrasonic Doppler Velocimetry (UDV), and<br />
local velocity using Vives probe. The latter two techniques serve to calibrate the time-<strong>of</strong>-flight flow<br />
meter. Moreover, the motor is equipped with a switch to allow changing <strong>of</strong> the flow direction from<br />
the counterclockwise mode into the clockwise mode. Hence, using UDV we are able to measure<br />
both purely hydrodynamic flow pr<strong>of</strong>iles and magnetohydrodynamic flow pr<strong>of</strong>iles, respectively.<br />
Finally, a water-based heat exchanger is integrated in the loop to guarantee isothermal conditions<br />
during the experimental runs. Melt temperature is measured using a submerged thermocouple.<br />
Our experimental results demonstrate that time-<strong>of</strong>-flight LFV is a suitable method to measure<br />
flow rate in turbulent liquid metal channel flow. We find a linear dependence <strong>of</strong> the measured<br />
characteristic vortex transportation velocity U and the mean velocity <strong>of</strong> the flow. Moreover, the<br />
measured flow pr<strong>of</strong>iles are in very good agreement with predictions <strong>of</strong> numerical simulations using<br />
the commercial program Package FLUENT MHD.<br />
We are greatful to the Deutsche Forschungsgemeinschaft (DFG) and the Bundesministerium
272 Section 13: Flow control<br />
für Bildung und Forschung (BMBF) for financial support. We have benefited from discussions<br />
with Dr. Ch. Resagk, and form the technical help by students J. Schumacher and S. Badtke.<br />
Electromagnetic interaction <strong>of</strong> a conducting cylinder with a magnetic dipole caused<br />
by steady translation and rotation<br />
Sonja Engert, Thomas Boeck, André Thess (TU Ilmenau) Schedule<br />
The electromagnetic interaction between a translating respectively rotating solid cylinder and<br />
the magnetic field <strong>of</strong> a point dipole is studied by numerical simulation and asymptotic analysis.<br />
The cylinder has finite electric conductivity and is assumed to be much longer than the distance<br />
between dipole and cylinder. Our investigation is motivated by the novel, non-invasive techniques<br />
named Lorentz force velocimetry and the Lorentz force eddy current testing. Both techniques<br />
are based on Lenz rule <strong>of</strong> electromagnetic induction and utilize the force on a magnet system<br />
produced by the movement <strong>of</strong> a conducting body. They allow one to measure integral and local<br />
velocities in conducting liquids and to detect deep-lying flaws in solid conductors.<br />
Our model problem has the advantage <strong>of</strong> conceptual simplicity, which allows us to compare<br />
analytical and numerical results in the limiting cases when the distances between the dipole and<br />
the cylinder are small and large compared to the cylinder radius. The governing equations are<br />
the induction equations for a prescribed velocity field. They are simplified by assuming that the<br />
magnetic Reynolds number is small, and that the induced eddy currents are stationary. In this<br />
so-called quasistatic approximation one only has to compute the electric potential from a Poisson<br />
equation with the scalar product <strong>of</strong> magnetic field and vorticity as right hand side. The Lorentz<br />
force and torque are then obtained from Ohm’s law for a moving conductor. At small distances<br />
h, our numerical computations for the Lorentz force agree with the h −3 behavior for a translating<br />
infinite conducting plate. At large separation, the force shows a h −6 decay for the rotating cylinder,<br />
and h −7 for the translating case, which is in agreement with the asymptotic analysis.<br />
Oscillating flow driven by a rotating magnetic field in liquid metal with an upper<br />
free surface<br />
V. Travnikov, K. Eckert, S. Odenbach (TU Dresden), T. Vogt, S. Eckert (Helmholtz-Zentrum<br />
Dresden-Rossendorf) Schedule<br />
The oscillatory flow instability in a liquid metal cylinder with a free upper surface, exposed<br />
to a rotating magnetic field (RMF), is analysed by numerical simulations <strong>of</strong> the axisymmetric<br />
Navier-Stokes equations [1]. The critical Taylor number designating the onset <strong>of</strong> the oscillatory<br />
flow regime is lower than that for the development <strong>of</strong> Taylor-Görtler vortices and decreases with<br />
increasing aspect ratio A = H . The instability sets in as a Hopf bifurcation and is initiated<br />
2R<br />
near the free surface, where an oscillatory variation <strong>of</strong> both the size and the position <strong>of</strong> the<br />
upper vortex in the secondary flow can be observed accompanied by horizontal oscillations <strong>of</strong><br />
the azimuthal velocity maximum at the free surface. We found that the flow frequency depends<br />
linear on the Taylor-number for all A investigated. Moreover, the Taylor-number interval, where<br />
the flow oscillations occur, becomes narrower. The predicted flow regime has been observed in<br />
corresponding model experiments with GaInSn using Ultrasound Doppler Velocimetry (UDV) for<br />
flow field measurements. The occurrence <strong>of</strong> the oscillatory flow regime depends sensitively on the<br />
cleanliness <strong>of</strong> the liquid metal surface.<br />
[1] V. Travnikov, K. Eckert, P. A. Nikrityuk, S. Odenbach, T. Vogt, S. Eckert, J. Crystal Growth<br />
(in press)
Section 13: Flow control 273<br />
Thermomagnetic convection under the influence <strong>of</strong> thermodiffusion<br />
Lisa Sprenger, Adrian Lange, Stefan Odenbach (TU Dresden) Schedule<br />
Thermomagnetic convection denotes a transport phenomenon induced by a temperature gradient<br />
and a magnetic field applied to a layer <strong>of</strong> a magnetisable fluid [1]. The onset <strong>of</strong> the convective<br />
motion is thereby described by a critical value <strong>of</strong> the sum <strong>of</strong> the Rayleigh and magnetic Rayleigh<br />
number<br />
Ra + Ram = (βT d 3 g∆T )/(νκ) + (K 2 ∆T 2 d 2 µ0)/(ηκ), (1)<br />
where K denotes the pyromagnetic coefficient, ∆T the temperature difference over the layer,<br />
d the layers height, g the acceleration due to gravity, βT the coefficient <strong>of</strong> thermal expansion,<br />
µ0 the magnetic permeability <strong>of</strong> vacuum, ν (η) the kinematic (dynamic) viscosity, and κ the<br />
heat coefficient. Considering the magnetic fluid as a binary fluid thermodiffusion may have to be<br />
considered if a temperature gradient is present. Former experiments carried out with a magnetic<br />
fluid revealed a dependence <strong>of</strong> the direction <strong>of</strong> thermodiffusion on the magnetic field. The direction<br />
is predicted to be in favor <strong>of</strong> the onset <strong>of</strong> convection for small magnetic field strengths and<br />
hindering it for large magnetic fields [2].<br />
The actual influence <strong>of</strong> thermodiffusive transport processes on the onset <strong>of</strong> convection is investigated<br />
with a linear stability analysis <strong>of</strong> the relevant hydrodynamic equations [1, 3]. The set<br />
<strong>of</strong> equations is composed <strong>of</strong> the continuity equation, the diffusion equation, the heat equation,<br />
and the Navier-Stokes equation, including the magnetic volume force as well as thermodiffusive<br />
terms.<br />
Experimental and numerical investigations on thermodiffusion complement the theoretical<br />
analyses aiming at a more detailed understanding <strong>of</strong> thermodiffusion. The experiments are set<br />
up in a horizontal diffusion cell based on a design presented in [2]. The change in concentration<br />
due to thermodiffusion is measured by sensor coils wrapped around the separation reservoirs <strong>of</strong><br />
the setup. The inductivities change <strong>of</strong> these coils is measured by a precision LCR meter. The<br />
measured concentrations are compared with numerical results obtained by a finite differences<br />
code in three dimensions for the relevant partial differential equation <strong>of</strong> the ferr<strong>of</strong>luid-dynamics<br />
theory [4].<br />
[1] B. A. Finlayson, J. Fluid Mech. 40, 753-767 (1970)<br />
[2] T. Völker, S. Odenbach, Phys. Fluids 17, 037104 (2005)<br />
[3] A. Ryskin et al., Phys. Rev. E 67, 046302 (2003)<br />
[4] A. Lange, Phys. Rev. E 70, 046308 (2004)<br />
Flow distortion <strong>of</strong> liquid metal in a square duct due to a magnetic point dipole<br />
Saskia Tympel, Thomas Boeck, Dmitry Krasnov, Jörg Schumacher (TU Ilmenau) Schedule<br />
Lorentz force velocimetry is a new contactless technique to measure the velocities <strong>of</strong> hot and<br />
agressive conductiong liquids. The Lorentz force on the magnet is highly sensitive to the velocity<br />
pr<strong>of</strong>ile that is influenced by the magnetic field. Thus the knowlegde <strong>of</strong> the flow transformation<br />
and the influence <strong>of</strong> an inhomogeneous local magnetic field on liquid metal flow is essential for<br />
obtaining velocity information from the measured forces.<br />
We consider liquid metal flow in a square duct with electrically insulating walls under the<br />
influence <strong>of</strong> a magnetic point dipole using three-dimensional direct numerical simulations with
274 Section 13: Flow control<br />
a finite-difference method. The dipole acts as a magnetic obstacle. A wide range <strong>of</strong> parameters<br />
affects the created wake. In this canonical setting, we study the modification <strong>of</strong> the flow for<br />
different Hartmann and Reynolds numbers. We observe a strong dependence <strong>of</strong> the magnetic<br />
obstacle effect and the corresponding Lorentz force on the orientation <strong>of</strong> the dipole as well as on<br />
its position.<br />
Secondary Flow Effects as Physical Mechanism <strong>of</strong> Molecular Species Transport in<br />
Highly Oscillating Generic-Trachea Flows<br />
Markus Rütten, Lars Krenkel, Roland Kessler (DLR) Schedule<br />
The high frequency oscillation artificial respiration technique is <strong>of</strong>ten the last hope for patients<br />
to survive highly damaged lung tissue. The mortality can significantly be reduced. In comparison<br />
to conventional artificial respiration the applied volume flow rate and pressure is significantly<br />
lowered in order to avoid further damaging <strong>of</strong> lung tissue and remaining intact alveolae. However,<br />
the physical mechanism <strong>of</strong> transport <strong>of</strong> oxygen to the aeriols under high frequency oscillation<br />
is not well understood. In the upper part <strong>of</strong> the lung convection is dominant, in contrast, the<br />
gas exchange in the lower parts <strong>of</strong> the lung is mainly driven by diffusion. It is not clear how<br />
associated gradients <strong>of</strong> concentrations <strong>of</strong> different molecular species are then achieved. Highly<br />
oscillating fluid flows has been a long research topic in fluid dynamics. It is known that oscillating<br />
pressure fluctuations are able to induce secondary flows, in particular, in curved ducts and pipes.<br />
The question is, whether the trachea enforces the generation <strong>of</strong> secondary flow by its kidney like<br />
cross section geometry. The influence <strong>of</strong> molecular species <strong>of</strong> different densities onto the formation<br />
<strong>of</strong> secondary flows and the convectional transport within the trachea is investigated. In order to<br />
clarify the physical mechanisms behind flow simulations have been conducted by using state <strong>of</strong> the<br />
art CFD techniques. We concentrate on a generic trachea configuration with a smoothed kidney<br />
like cross sections [3]. Thereto, we have reduced the complexity <strong>of</strong> the real trachea in order to<br />
clearly separate mechanism inducing secondary flows. In our numerical experiment the trachea has<br />
been filled with a mixture <strong>of</strong> oxygen and solcane, a tracer gas <strong>of</strong>ten used in clinical applications [1].<br />
A well known method in analytical fluid dynamics is the transformation <strong>of</strong> boundary conditions,<br />
see [2]. In this work we will discuss our numerical simulation results, special attention is given<br />
to the formation <strong>of</strong> the secondary flow structures and their impact on the netto transport <strong>of</strong> the<br />
different species.<br />
[1] Chang HK.: Flow dynamics in the respiratory tract. In: Respiratory Physiology: An Analytical<br />
Approach, edited by Chang HK and Paiva M. Dekker: New York, 1989, p. 57 - 138.<br />
[2] Lacor C., Jayaraju S. T., Brouns M., Verbanck S.: Simulation <strong>of</strong> the Airflow in the Upper Airways<br />
with Applications to Aerosols Coupled Methods in Numerical Dynamics (eds: Zdravko<br />
Terze and Chris Lacor), SBN-ISSN: 978-953-6313-88-4, 2007.<br />
[3] Landau L. D., Lifschitz J. M.: Lehrbuch der theoretischen Physik in 10 Bänden, Akademie-<br />
Verlag Berlin, neu: Harri Deutsch-Verlag Frankfurt/Main
Section 14: Applied analysis 275<br />
Section 14: Applied analysis<br />
Organizers: Robert Denk (<strong>Universität</strong> Konstanz), Friedemann Schuricht (TU Dresden)<br />
S14.1: Applied analysis, Session A Tue, 13:30–15:30<br />
Chair: Friedemann Schuricht S1|03–113<br />
Linearized elastoplasticity is the evolutionary Γ-limit <strong>of</strong> finite elastoplasticity<br />
Alexander Mielke (WIAS Berlin), Ulisse Stefanelli (IMATI, Pavia) Schedule<br />
We provide a rigorous justification <strong>of</strong> the classical linearization approach in plasticity. By taking<br />
the small-deformations limit, we prove via Γ-convergence for rate-independent processes that<br />
energetic solutions <strong>of</strong> the quasi-static finite-strain elastoplasticity system converge to the unique<br />
strong solution <strong>of</strong> linearized elastoplasticity.<br />
The work combines the static approach <strong>of</strong> [DNP02] with the abstract Γ-convergence result for<br />
energetic rate-independent system developed in [MRS08]. The crucial step is the construction <strong>of</strong><br />
a suitable mutual recovery sequence that transforms the additive split <strong>of</strong> the strain tensor in the<br />
linearized theory into a carefully chosen multiplicative decomposition <strong>of</strong> the strain tensor as is<br />
needed in the setting <strong>of</strong> finite-strain elastoplasticity.<br />
[DNP02] G. Dal Maso, M. Negri, and D. Percivale. Linearized elasticity as Γ-limit <strong>of</strong> finite<br />
elasticity. Set-Valued Anal., 10(2-3):165–183, 2002.<br />
[MRS08] A. Mielke, T. Roubíček, and U. Stefanelli. Γ-limits and relaxations for rate-independent<br />
evolutionary problems. Calc. Var. Partial Differential Equations, 31(3):387–416, 2008.<br />
On the passage from atomistic systems to nonlinear elasticity theory<br />
Julian Braun, Bernd Schmidt (<strong>Universität</strong> Augsburg) Schedule<br />
The main aim <strong>of</strong> our work in [1] is to provide a rigorous derivation <strong>of</strong> nonlinear elasticity functionals<br />
from atomistic models. A fundamental contribution towards this aim has been made by<br />
Alicandro and Cicalese in [2], where they prove a general integral representation result for continuum<br />
limits <strong>of</strong> atomistic pair interaction potentials. It is our main aim, departing from this result,<br />
to derive a continuum theory for more general interaction potentials which, in particular, can also<br />
incorporate bond-angle dependent potentials. Such an extension is desirable in applications, as<br />
many atomistic models such as, e.g., the Stillinger-Weber potential, cannot be written as a pure<br />
pair potential. In fact, the class <strong>of</strong> potentials our theory applies to is rich enough to model any<br />
continuum energy density, even if the Cauchy-relations are violated.<br />
The limiting density is described in terms <strong>of</strong> a sequence <strong>of</strong> cell problems. This is related to<br />
standard homogenization results <strong>of</strong> nonconvex integral functionals. Using the results in [3], we<br />
prove, that under appropriate conditions, this limiting density is given by the Cauchy-Born-rule<br />
for small (but finite) strains.<br />
In order to prove our main representation result we resort to abstract integral representation<br />
results for functionals on Sobolev spaces and thus follow the scheme set forth in [2], which is<br />
dictated by verifying the hypotheses <strong>of</strong> that abstract theorem. There are, however, some major<br />
differences as compared to the pair interaction case treated by Alicandro and Cicalese. While these<br />
authors use slicing arguments in order to obtain energy estimates on the usual d × d deformation<br />
gradients in the direction <strong>of</strong> interacting pairs, we will have to estimate the much higher dimensional<br />
d × 2 d discrete deformation gradients. In fact, as in general our discrete energies cannot be
276 Section 14: Applied analysis<br />
recovered by slicing techniques, we will instead work with very carefully chosen interpolations <strong>of</strong><br />
the discrete deformations which encode the full discrete gradient on lattice cells.<br />
[1] Julian Braun, Bernd Schmidt, On the passage from atomistic systems to nonlinear elasticity<br />
theory, preprint, arXiv:1107.4155 (2011).<br />
[2] Roberto Alicandro and Marco Cicalese, A General Integral Representation Result for Continuum<br />
Limits <strong>of</strong> Discrete Energies with Superlinear Growth, SIAM J. Math. Anal. 36(1)<br />
(2004), 1 – 37.<br />
[3] Sergia Conti, Georg Dolzmann, Bernd Kirchheim, Stefan Müller, Sufficient conditions for the<br />
validity <strong>of</strong> the Cauchy-Born rule close to SO(n), J. Eur. Math. Soc. (JEMS) 8 (2006), 515<br />
– 539.<br />
Global spatial regularity for elastic fields with cracks and contact<br />
Dorothee Knees (WIAS Berlin) Schedule<br />
A global higher differentiability result in Besov spaces is proved for the displacement fields <strong>of</strong><br />
linear elastic models with self contact. In particular, domains with cracks are studied, where<br />
nonpenetration conditions/Signorini conditions are imposed on the crack faces. It is shown that<br />
in a neighborhood <strong>of</strong> crack tips (in 2d) or crack fronts (3d) the displacement fields are B 3<br />
2<br />
2,∞regular.<br />
The pro<strong>of</strong> relies on a difference quotient argument for the directions tangential to the<br />
crack. In order to obtain the regularity estimates also in the normal direction, an argument due<br />
to Ebmeyer/Frehse/Kassmann is modified. The methods used here will also be applied to further<br />
examples like contact problems with nonsmooth rigid foundations or to energies with nonsmooth<br />
constraints as they occur for instance in the modeling <strong>of</strong> shape memory alloys. Numerical examples<br />
will illustrate the proved results.<br />
This is joint work with Andreas Schröder (HU Berlin).<br />
The Loves problem for hyperbolic thermoelasticity.<br />
Jerzy Gawinecki, Józef Rafa, Jarosław Łazuka (Military University <strong>of</strong> Technology, Warsaw) Schedule<br />
In our presentation we investigated the initial-boundary value problem for elastic layer situated<br />
on half space <strong>of</strong> another elastic medium. In this medium the thermomechanical interactions were<br />
taken into consideration. The system <strong>of</strong> equations with initial-boundary conditions describes the<br />
phenomenon <strong>of</strong> wave propagation with finite speed. In our problem there are two surfaces i.e.<br />
free surface and contact surface between layer and half space. On the free surface are setting<br />
boundary conditions for normal and tangential surface force. We consider two types <strong>of</strong> contact<br />
between layer and half space: rigid contact and slip contact. The initial-boundary value problem<br />
was solved by using integral transformation and Cagniard- de Hoope methods. From the solution<br />
<strong>of</strong> this problem follows that in layer and half space exist some kind <strong>of</strong> thermoelastic waves. We<br />
investigated moreover the conditions which should be fullfiled for propagation <strong>of</strong> Raylaighs and<br />
Loves type waves on the contact surface between layers and half space. Our results can be used<br />
in technical applications especially engineering design and diagnostics <strong>of</strong> roads and airfields.<br />
Delamination in visco-elastic materials with thermal effects<br />
Marita Thomas (WIAS Berlin), Riccarda Rossi (Università di Brescia) Schedule<br />
This contribution deals with the analysis <strong>of</strong> a model describing a rate-independent delamination<br />
process along a prescribed interface. The material properties in the bulk are considered to be viscoelastic<br />
and temperature-dependent. In the spirit <strong>of</strong> continuum damage mechanics the delamination
Section 14: Applied analysis 277<br />
process is modeled with the aid <strong>of</strong> an internal delamination variable z. The related PDE system,<br />
which couples the displacements, the absolute temperature and the delamination variable, has<br />
a highly nonlinear character and features nonpenetration conditions. The goal is to obtain the<br />
existence <strong>of</strong> weak solutions in the setting <strong>of</strong> brittle delamination, where the delamination variable<br />
takes the values 0 or 1, only, and where the crack is described in terms <strong>of</strong> a transmission condition<br />
being a local, nonconvex constraint, which links the displacements and the delamination variable<br />
in a very rigid manner. In order to deduce this existence result the brittle model is consecutively<br />
approximated by suitably regularized problems: On the one hand, the brittle constraint z ∈<br />
{0, 1} is gained from a Modica-Mortola functional; on the other hand, the brittle transmission<br />
condition is approximated by a surface energy term for so-called adhesive contact, which penalizes<br />
displacement jumps outside the crack set but does not rigidly exclude them.<br />
S14.2: Applied analysis, Session A Tue, 16:00–18:00<br />
Chair: Alexander Mielke S1|03–113<br />
Analytical model for deformable roll coating with nip feed<br />
Bettina Willinger (<strong>Universität</strong> Erlangen-Nürnberg), Philipp Epple (Hochschule Coburg), Antonio<br />
Delgado (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
Nowadays roll coating is a common technique for applying thin coating films on continuous<br />
substrates, e.g. paper and foils. Roll coating are operated either with co-rotating or counterrotating<br />
rolls and the field <strong>of</strong> applications ranges from printable solar cells via composites to<br />
adhesive labels. Key advantages are the comparatively simple technology and the possibility <strong>of</strong><br />
coating thin films using highly viscous fluids. On the other hand, the probably most important<br />
disadvantage <strong>of</strong> roll coating systems compared to other coating technologies like curtain, spray or<br />
slot coating is the self-metered coating process. A lot <strong>of</strong> experience and experiments are necessary<br />
to find the proper parameters to coat a defined film thickness. Analytical solutions <strong>of</strong>fer a good<br />
possibility to find predictions for the necessary set-up parameters.<br />
The presented work deals therefore with an analytical solution for a roll coater with deformable<br />
rolls, as commonly used in industry. In this coating technique <strong>of</strong>ten a pair <strong>of</strong> a rigid (steel) roll<br />
and a deformable roll is used. The deformable roll is in most cases a steel roll wrapped with an<br />
elastic rubber layer. The focus is on the calculation <strong>of</strong> the nip feed system in a forward coating<br />
mode.<br />
The calculation is done with thin film theory, as it is an useful simplification <strong>of</strong> Navier-Stokes-<br />
Equations for the presented case. For including the elasticity <strong>of</strong> the deformable roll Hooks law<br />
for elasticity <strong>of</strong> the deformable roll are used. Pressure boundary conditions are introduced in the<br />
calculation for getting a closed solution. The film splitting <strong>of</strong> the coating film is described by<br />
a commonly used relation based on the calculations <strong>of</strong> Landau and Levich and experimentally<br />
validated in literature.<br />
The new model has been validated by experiments with an industrial roll coater. The analytical<br />
prediction and the experimental data are in good agreement.<br />
Estimations on Thermo-mechanical Dynamics <strong>of</strong> Vibration Elastomeric Isolators<br />
Silviu Nastac, Carmen Debeleac (Dunarea de Jos University <strong>of</strong> Galati, Braila) Schedule<br />
This analysis deals with one <strong>of</strong> the basic problem category <strong>of</strong> vibratory systems, means the complete<br />
and complex characterization <strong>of</strong> elastic and viscous isolators behaviour under dynamic loads<br />
such as vibrations, seismic waves, shocks, etc. Usually, the dynamic characteristics <strong>of</strong> vibration<br />
isolators made by elastomeric materials are considered to have a constant shape for a certain<br />
practical case. It is ignored the thermal phenomenon inside the isolator block during the exploita-
278 Section 14: Applied analysis<br />
tion cycles and its influences on the proper characteristic parameters. This usual approximation<br />
leads to more or less significant differences between simulation and practical evolution <strong>of</strong> a vibration<br />
isolator subjected to the same dynamic load. Continuous changes <strong>of</strong> rigidity modulus and/or<br />
dissipative characteristics due to internal thermal effects imply aleatory evolution <strong>of</strong> the isolated<br />
system, unstable movements and resonance imminence danger. The partial results <strong>of</strong> this analysis<br />
dignify the linkage between thermal effects into the elastomeric isolator and its essential dynamic<br />
parameters. Using <strong>of</strong> these correlations frames the seismic shock and vibration protective devices<br />
designing and deployment areas.<br />
On Non-linear Characteristics Evaluation <strong>of</strong> Vibratory Tool and Terrain Interaction<br />
for Embankment Works<br />
Carmen Debeleac, Silviu Nastac (Dunarea de Jos University <strong>of</strong> Galati, Braila) Schedule<br />
The complete and correct identification and evaluation <strong>of</strong> proper characteristics <strong>of</strong> terrain for embankment<br />
works is the frame idea <strong>of</strong> this analysis. The study began from the necessity <strong>of</strong> vibratory<br />
working tools utilization for different construction jobs. Mainly, the simple dynamic calculus is<br />
used for estimation <strong>of</strong> proper parameters values for this kind <strong>of</strong> works. It supposes a linear characteristic<br />
<strong>of</strong> the material in interaction with vibrating tool and it estimates the domain <strong>of</strong> working<br />
parameters. But instrumental tests reveal that the terrain has a non-linear characteristic and the<br />
dynamic behaviour acquires deviation from theoretical estimations. An identification procedure<br />
followed by a correct and complete evaluation <strong>of</strong> the non-linear parameters gives the necessary<br />
information for a practical case. Available mathematical models require a lot <strong>of</strong> initial values<br />
for characteristic parameters, but changing the case changes the values. A complex model which<br />
needs only initial tuning <strong>of</strong>fers a proper solution to simulate, estimate, evaluate and analyze the<br />
interactions between the vibratory tools <strong>of</strong> construction equipments and the terrain. Non-linear<br />
static and dynamic characteristics are the basic model defined properties. Elastic, dissipative and<br />
plastic rheological components were included into the main model. Partial concluding remarks<br />
have shown a good approximation between numerical results and experiments. The results <strong>of</strong><br />
this study are very useful for vibratory equipment designing and correct exploitation, check <strong>of</strong><br />
Regulations conformity for construction technologies, and oldies equipments maintenance.<br />
On the modeling <strong>of</strong> slender heat sources<br />
Thomas Martin Cibis, Nicole Marheineke (<strong>Universität</strong> Erlangen-Nürnberg), Raimund Wegener<br />
(Fraunh<strong>of</strong>er-ITWM Kaiserslautern) Schedule<br />
In the production process <strong>of</strong> nonwoven materials thousands <strong>of</strong> long slender fibers are spun and<br />
entangled by fast air streams before they are fall down onto a conveyor belt where they form<br />
a nonwoven texture (web). The quality <strong>of</strong> the fabric is crucially determined by the fiber-flowinteractions.<br />
Since the direct numerical simulation <strong>of</strong> this two-phase multi-scale problem is impossible,<br />
we intend to model the two-way coupling on basis <strong>of</strong> slender-body theory and drag<br />
sources that satisfy the actio-reactio principle in the balance laws <strong>of</strong> momentum and energy with<br />
respect to flow and fibers. In this talk, we focus on the aspect <strong>of</strong> heat exchange treating the<br />
fibers as long and slender heat sources. We introduce an asymptotic surrogate model in which<br />
the three-dimensional objects are replaced by line sources. To evaluate this approach, a simplified<br />
model scenario is investigated and solved analytically.<br />
S14.3: Applied analysis, Session B Wed, 13:30–15:30<br />
Chair: Robert Denk S1|03–113
Section 14: Applied analysis 279<br />
A free boundary problem related to the spin-coating process<br />
Matthias Geissert (TU Darmstart) Schedule<br />
We consider the spin-coating process which is described by the Navier-Stokes equations in a layerlike<br />
domain in 3 in the rotating setting. Our model takes into account Coriolis forces, centrifugal<br />
forces as well as surface tension on the free boundary. On the fixed boundary we prescribe Robin<br />
boundary conditions.<br />
Our aim is to show local existence and uniqueness <strong>of</strong> strong solutions. In order to do so, we<br />
transform this problem to a fixed layer by the Hanzawa transform and show maximal regularity<br />
estimates for a suitable linearized problem.<br />
Helically symmetric flows: Conservation laws using Lie symmetries<br />
Olga Kelbin (TU <strong>Darmstadt</strong>), Alexei F. Cheviakov (University <strong>of</strong> Saskatchewan, Saskatoon), Martin<br />
Oberlack (TU <strong>Darmstadt</strong>) Schedule<br />
A new theoretical approach for helical flows using Lie symmetries is presented. By introducing<br />
the helical variable ξ = az + bϕ, in which ϕ, z are cylindrical coordinates, we are able to derive<br />
the Euler and Navier-Stokes equations for helically symmetrical flows in primitive variables as<br />
well as in vorticity formulation. The obtained systems <strong>of</strong> equations unify the equations <strong>of</strong> planar<br />
and axially symmetrical flows as being the natural limits characterized by two parameters a and<br />
b.<br />
Conservation laws are constructed using the direct method [1] . This method is based on the idea to<br />
use the Euler operator to obtain the divergence expressions that comes originally from the ideas<br />
related to famous Noether’s theorem, but is applicalbe to a much wider class <strong>of</strong> PDE systems.<br />
In addition to classical well known conservation laws like conservation <strong>of</strong> mass, momentum, energy,<br />
new infinite families <strong>of</strong> conservation laws are discovered.<br />
[1] S. Anco, G. Bluman, A.F. Cheviakov. Applications <strong>of</strong> Symmetry Methods to Partial Differential<br />
Equations, vol. 168. Springer: Applied Mathematical Sciences, 2010<br />
On the ultra relativistic Euler equations<br />
Mahmoud Abdelrahman, Matthias Kunik, Gerald Warnecke (<strong>Universität</strong> Magdeburg) Schedule<br />
In this paper we study the relativistic Euler equations in isentropic fluids with the equation <strong>of</strong><br />
state p = ρ<br />
, which is the ultra-relativistic limit. We first analyze the single shocks and rarefaction<br />
3<br />
curves. Then the Riemann problem is solved constructively. We derive sharp estimates for the<br />
strength <strong>of</strong> the waves in the Riemann solution and prove uniqueness for the Riemann problem.<br />
Finally we study explicit examples for the irreversibilty <strong>of</strong> the ultra relativistic Euler equations.<br />
The exterior Dirichlet and the interior Neumann boundary value problems for the<br />
scalar Oseen equation<br />
Emma Skopin (<strong>Universität</strong> Kassel) Schedule<br />
The scalar Oseen equation represents a linearized form <strong>of</strong> the Navier Stokes equations. We present<br />
an explicit potential theory for this equation and solve the exterior Dirichlet and interior Neumann<br />
boundary value problems via a boundary integral equations method in spaces <strong>of</strong> continuous<br />
functions on a C 2 -boundary, extending the classical approach for the isotropic selfadjoint Laplace<br />
operator to the anisotropic non-selfadjoint scalar Oseen operator.
280 Section 14: Applied analysis<br />
Sufficient conditions for second order L 2 -convergence <strong>of</strong> the fractional step theta<br />
method<br />
Florian Zanger (<strong>Universität</strong> Kassel) Schedule<br />
We consider the fractional step theta time stepping procedure for the non-stationary incompressible<br />
linear Stokes equations in a cylindrical domain (0, T ) × G, where G is a bounded domain<br />
in R n . Using energy estimates and assuming a certain degree <strong>of</strong> regularity for the data, we show<br />
second order L 2 -convergence.<br />
On Sharp Interface Limits <strong>of</strong> Diffuse Interface Models for Viscous Incompressible<br />
Fluids<br />
Helmut Abels (<strong>Universität</strong> Regensburg) Schedule<br />
We present recent results on the sharp interface limits <strong>of</strong> a new diffuse interface model for two<br />
viscous incompressible fluids with different densities. We will discuss how the sharp interface limit<br />
depends on the choice <strong>of</strong> the mobility. The sharp interface limit is determined with the aid <strong>of</strong> the<br />
method <strong>of</strong> formally matched asymptotics. Moreover, in some cases we can perform the limit on<br />
the level <strong>of</strong> so-called varifold solutions rigorously.<br />
S14.4: Applied analysis, Session B Wed, 16:00–18:00<br />
Chair: Matthias Geissert S1|03–113<br />
Convergence properties <strong>of</strong> weak solutions <strong>of</strong> the Boussinesq equations in domains<br />
with rough boundaries<br />
Christian Komo (TU <strong>Darmstadt</strong>) Schedule<br />
We act on the assumption that the boundary <strong>of</strong> every ’physical’ domain Ω has microscopic asperities<br />
which influence the boundary behaviour <strong>of</strong> weak solutions <strong>of</strong> the Boussinesq equations. Let<br />
(Ωn)n∈N ⊆ R3 be domains with rough boundaries and let Ωn ’converge to’ Ω. Consider a sequence<br />
(un, θn)n∈N <strong>of</strong> weak solutions <strong>of</strong> the Boussinesq equations with un fulfilling the impermeability<br />
condition un · N = 0 on ∂Ωn and θn fulfilling the Robin boundary condition ∂θn<br />
∂N + α(θn − h0) = 0<br />
on ∂Ωn. In this talk the boundary conditions and limit equations <strong>of</strong> weak limits <strong>of</strong> (un, θn) on Ω<br />
under certain assumptions <strong>of</strong> the rugosity <strong>of</strong> the boundaries will be determined.<br />
Exponential stability for a general model in electrophoresis<br />
Jürgen Saal, André Fischer, Dieter Bothe (TU <strong>Darmstadt</strong>) Schedule<br />
We present a thorough analysis <strong>of</strong> the Navier-Stokes-Nernst-Planck-Poisson equations. This system<br />
describes the dynamics <strong>of</strong> charged particles dispersed in an incompressible fluid. In contrast<br />
to existing literature and in view <strong>of</strong> its physical relevance, we also allow for different diffusion coefficients<br />
<strong>of</strong> the charged species. In addition, the commonly assumed electro-neutrality condition<br />
is not required by our approach. Our aim is to present results on local and global well-posedness<br />
as well as exponential stability <strong>of</strong> equilibria. The results are obtained jointly with Dieter Bothe<br />
and Andre Fischer at the Center <strong>of</strong> Smart Interfaces at TU <strong>Darmstadt</strong>.<br />
Validity <strong>of</strong> the Korteweg-de Vries Approximation for the Two-Dimensional Water<br />
Wave Problem in the Arc Length Formulation<br />
Wolf-Patrick Düll Schedule<br />
We consider the two–dimensional water wave problem in an infinite long canal <strong>of</strong> finite depth both<br />
with and without surface tension. It has been proven by several authors that long–wavelength<br />
solutions to this problem can be approximated over a physically relevant timespan by solutions<br />
<strong>of</strong> the Korteweg–de Vries equation or, for certain values <strong>of</strong> the surface tension, by solutions <strong>of</strong> the
Section 14: Applied analysis 281<br />
Kawahara equation. These pro<strong>of</strong>s are formulated either in Langrangian or in Eulerian coordinates.<br />
In this talk, we provide a new pro<strong>of</strong>, which is simpler, more elementary and shorter. Moreover,<br />
the rigorous justification <strong>of</strong> the KdV approximation can be given for the cases with and without<br />
surface tension together by one pro<strong>of</strong>. In our pro<strong>of</strong>, we parametrize the free surface by arc length<br />
and use some geometrically and physically motivated variables with good regularity properties.<br />
This formulation <strong>of</strong> the water wave problem has already been <strong>of</strong> great usefulness for Ambrose and<br />
Masmoudi to simplify the pro<strong>of</strong> <strong>of</strong> the local well–posedness <strong>of</strong> the water wave problem in Sobolev<br />
spaces.<br />
Cosymmetric problems and bifurcations without parameter<br />
Andrey Afendikov (Keldysh Institute <strong>of</strong> Applied Mathematics, Moscow) Schedule<br />
In the early 1990s V.Yudovich introduced the notion <strong>of</strong> cosymmetry. He discovered that steady<br />
states are generically non-isolated in such problems and investigated the loss <strong>of</strong> stability and<br />
the bifurcation <strong>of</strong> cycle generation. We consider several hydrodynamic problems in unbounded<br />
domains where in a vicinity <strong>of</strong> the instability threshold the dynamics is governed by generalized<br />
Cahn-Hilliard equation. For the time independent solutions <strong>of</strong> this equation we recover<br />
Bogdanov-Takens bifurcation without parameter in the 3-dimensional reversible system with a<br />
line <strong>of</strong> equilibria. This line <strong>of</strong> equilibria is neither induced by symmetries, nor by first integrals.<br />
At isolated points, normal hyperbolicity <strong>of</strong> the line fails due to a transverse double eigenvalue<br />
zero. The bi-reversible problem and its small perturbation where only one symmetry is left was<br />
studied in [1],[2]. Our aim is to relate Yudovich theory to our results and to discuss hydrodynamic<br />
problems, where the reversibility breaking perturbation can not be considered as small.<br />
[1] A. Afendikov, B. Fiedler, and S. Liebscher. Plane Kolmogorov flows and Takens-Bogdanov<br />
bifurcation without parameters: The doubly reversible case.Asymptotic Analysis, 60 (3,4),<br />
(2008), 185–211.<br />
[2] A. Afendikov, B. Fiedler, and S. Liebscher. Plane Kolmogorov flows and Takens-Bogdanov<br />
bifurcation without parameters: The singly reversible case. Asymptotic Analysis, 72, n. 1-2<br />
, (2011), 31–76<br />
On a one-dimensional upper-convected Maxwell model for a viscoelastic fiber jet –<br />
asymptotic derivation and numerical simulations<br />
Maike Lorenz (TU Kaiserslautern), Nicole Marheineke (<strong>Universität</strong> Erlangen-Nürnberg), Raimund<br />
Wegener (Fraunh<strong>of</strong>er ITWM) Schedule<br />
In this talk we present a strict systematic derivation <strong>of</strong> a one-dimensional model for the dynamics<br />
<strong>of</strong> a viscoelastic jet using asymptotic analysis in the slenderness ratio <strong>of</strong> the jet. The model is<br />
obtained from the three-dimensional free boundary value problem <strong>of</strong> the upper-convected Maxwell<br />
equations describing the flow <strong>of</strong> a viscoelastic fluid. It also covers the purely viscous case. The<br />
model system has a hyperbolic character and contains several parameters that determine the<br />
solvability <strong>of</strong> the equations and hence the applicability range <strong>of</strong> the model. For a stationary<br />
uniaxial gravitational spinning process we show numerical simulations and investigate the effect<br />
<strong>of</strong> a die swell, i.e. an increase in the jet diameter which is larger than the diameter <strong>of</strong> the nozzle<br />
where the fluid is extruded.<br />
S14.5: Applied analysis, Session C Thu, 13:30–15:30<br />
Chair: Helmut Abels S1|03–113
282 Section 14: Applied analysis<br />
On the Riesz minimal energy problem<br />
Wolfgang L. Wendland (<strong>Universität</strong> Stuttgart) Schedule<br />
This is on joint work with H. Harbrecht, G. Of and N. Zorii.<br />
In Rn ≥ 2, we study the constructive and numerical solution <strong>of</strong> minimizing the Riesz energy<br />
relative to the Riesz kernel |x − y| α−n , where 1 < α < n, for the Gauss variational problem. which<br />
is considered for two compact, disjoint closed manifolds Γj ⊂ Rn , j = 1, 2, charged with Borel<br />
measures <strong>of</strong> opposite sign. Since this minimizing problem over an affine cone <strong>of</strong> Borel measures<br />
with finite Riesz energy can also be formulated as the minimum problem over an affine cone <strong>of</strong><br />
ε<br />
− surface distributions belonging to a Sobolev–Slobodetski space H 2 (Γ), 0 < ε = α−1, Γ := Γ1∪Γ2,<br />
the application <strong>of</strong> simple layer boundary integral operators on Γ can be used. The numerical<br />
approximation is based on a Galerkin–Bubnov discretization with piecewise constant boundary<br />
elements. For n = 3 and n = 2 multipole approximation and for 1 < α < 3 = n wavelet matrix<br />
compression is applied. The minimizing procedure is executed with an active set strategy. We<br />
finally present some numerical results.<br />
Maximum modulus estimates for the linear steady Stokes system<br />
Werner Varnhorn (<strong>Universität</strong> Kassel) Schedule<br />
In the theory <strong>of</strong> partial differential equations the classical maximum principle is well-known.<br />
It states that any non-constant harmonic function u takes its maximum (and minimum) values<br />
always at the boundary ∂G <strong>of</strong> the corresponding domain G. For higher order differential equations<br />
as well as for systems <strong>of</strong> differential equations such a principle does not hold in general. In these<br />
cases, however, there is some hope for a so-called maximum modulus estimate <strong>of</strong> the form<br />
max |u(x)| ≤ c max<br />
G ∂G |u(x)|,<br />
where c denotes some constant. We prove the validity <strong>of</strong> such an estimate for the linear Stokes<br />
system via the method <strong>of</strong> boundary integral equations. Here G ⊂ R n (n ≥ 2) is some bounded<br />
or unbounded open set having a compact boundary ∂G <strong>of</strong> class C 1,α (0 < α ≤ 1).<br />
Blow-up <strong>of</strong> solutions to a p-Laplace equation<br />
Yuliya Gorb (University <strong>of</strong> Houston) Schedule<br />
The problem considered in this talk describes two perfectly conducting spheres in a homogeneous<br />
medium where the current-electric field relation is the power law. Electric field E blows up in the<br />
L ∞ -norm as δ, the distance between the conductors, tends to zero. A concise rigorous justification<br />
<strong>of</strong> the rate <strong>of</strong> this blow-up in terms <strong>of</strong> δ will be given.<br />
On asymptotic behavior <strong>of</strong> 1-dimensional functional <strong>of</strong> Ginzburg-Landau type with<br />
internally-externally created oscillations <strong>of</strong> minimizers<br />
Andrija Raguz (Zagreb School <strong>of</strong> Economics and Management, Department <strong>of</strong> Mathematics and<br />
Statistics, Zagreb) Schedule<br />
In this note we provide a kind <strong>of</strong> generalization <strong>of</strong> the well-known notion <strong>of</strong> internally (externally,<br />
resp.) created oscillations <strong>of</strong> minimizers <strong>of</strong> non-convex integrands in the calculus <strong>of</strong> variations. As<br />
an example, we consider a class <strong>of</strong> 1-dimensional Ginzburg-Landau functionals (the simplest case<br />
being considered in the paper G. Alberti, S. Muller: A new approach to variational problems with<br />
multiple scales, Comm. Pure Appl. Math. 54, 761-825 (2001)). We describe asymptotic behavior<br />
leading to multiple small scale separation as parameter epsilon tends to zero.
Section 14: Applied analysis 283<br />
Analysis and simulations <strong>of</strong> data based PDE-models in intracellular signaling<br />
Elfriede Friedmann (<strong>Universität</strong> Heidelberg) Schedule<br />
Complex biological processes in systems biology are usually reduced to a system <strong>of</strong> chemical<br />
reactions taking place in a fluid medium. Rate equations link the reaction rate or velocity <strong>of</strong><br />
the reaction to the concentration <strong>of</strong> the reactants according to a specific law. With resulting<br />
differential equations we obtain the evolution <strong>of</strong> signaling pathways over time and space. They<br />
help to understand underlying mechanisms, explain certain characteristic behavior, or predict<br />
the outcome <strong>of</strong> experiments. For intracellular systems, such as signaling pathways, most existing<br />
models are based on ordinary differential equations. These models describe temporal processes,<br />
while they neglect spatial aspects. In [9] and [10] experimental evidence was given that cell size<br />
and shape can influence intracellular signaling. Basic theoretical work concerning this aspect can<br />
be found in [2] and [7].<br />
We will compare data-based (non)linear PDE models on the basis <strong>of</strong> reaction diffusion equations<br />
with the corresponding ODE model <strong>of</strong> the JAK2/STAT5 and SMAD signaling pathway, to<br />
analyze whether the cell geometry plays a significant role to its fate or not. It is an interesting<br />
biological question, if the diffusion <strong>of</strong> signaling molecules leads to a roughly homogeneous distribution<br />
or if we can observe a significant gradient <strong>of</strong> proteins in the cell. Such a gradient might affect<br />
the signaling pathway and constitute a regulatory mechanism. In the cytoplasm, signaling may<br />
be localized to certain areas. In addition, the signal to the nucleus may be delayed or modulated<br />
by diffusive processes.<br />
We present numerical simulations <strong>of</strong> these data-based models performed with the s<strong>of</strong>tware<br />
Gascoigne [6] developed in Rolf Rannachers group based on Finite Elements. With the high<br />
quality numerical methods implemented in this s<strong>of</strong>tware like adaptive mesh refinement, multigrid<br />
algorithms and error control [1], [11], we are able to handle even more complex shapes within a<br />
suitable computing time. We used different diffusion coefficients and calculated the spatial average<br />
<strong>of</strong> each species’ concentration as the integral over the cytoplasmic domain divided by the volume<br />
<strong>of</strong> the cytoplasm, i.e. uaverage(t) = 1<br />
�<br />
u(x, t). These average concentrations were plotted as<br />
vcyt<br />
Ωcyt<br />
time courses and compared to the results <strong>of</strong> the pure ODE system.<br />
Nevertheless, the outcome <strong>of</strong> our simulations can be significant only if we use as model input<br />
high-quality quantitative data (provided by our collaboration partner from the German Cancer<br />
Research Center [8]), and if we are able to establish some theoretical results to guarantee the<br />
existence and uniqueness <strong>of</strong> solutions <strong>of</strong> our differential equation system.<br />
We will present our analytical and numerical results and will show that diffusion in the model<br />
can lead to significant intracellular gradients <strong>of</strong> signaling molecules and changes the level <strong>of</strong><br />
response to the signal transduced by the signaling pathway. In particular, the extend <strong>of</strong> these<br />
observations will depend on the geometry <strong>of</strong> the cell.<br />
[1] Becker, R., Rannacher, R., An optimal control approach to a posteriori error estimation in<br />
finite element methods, Acta Numerica 10, 1-102, 2001.<br />
[2] Brown, G. C., Kholodenko, B. N., Spatial gradients <strong>of</strong> cellular phospho-proteins, FEBS Letters,<br />
457:452-454, 1999.<br />
[3] Friedmann, E., Pfeifer, A. C., Neumann, R., Klingmüller, U., Rannacher, R., Interaction between<br />
Experiment, Modeling and Simulation <strong>of</strong> Spatial Aspects in the Jak2/Stat5 Signaling<br />
Pathway, Modellgestuetzte Parameterschaetzung - Theorie und Anwendungen, Springer, in<br />
print.
284 Section 14: Applied analysis<br />
[4] Friedmann, E., Neumann, R., Rannacher, R., Well-posedness for a spatio-temporal model <strong>of</strong><br />
the JAK2/STAT5 signaling pathway, submitted 2011.<br />
[5] Friedmann, E., Claus, J., Rannacher, R., Spatial aspects in the SMAD signaling pathway,<br />
submitted 2011.<br />
[6] GASCOIGNE, High Performance Adaptive Finite Element Toolkit, URL: http://www.<br />
numerik.uni-kiel.de/~mabr/gascoigne/.<br />
[7] Kholodenko, B. N. Cell signalling dynamics in time and space, Nat. Rev. Mol. Cell Biol.,<br />
7:3:165-176, 2006.<br />
[8] Klingmüller, U., Bauer, A., Bohl, S., Nickel, P. J., Breitkopf, K., Dooley, S., Zellmer, S.,<br />
Kern, C., Merfort, I., Sparna, T., Donauer, J., Walz, G., Geyer, M., Kreutz, C., Hermes,<br />
M., Götschel, F., Hecht, A., Walter, D., Egger, K. Neubert, C. Borner M. Brulport, W.<br />
Schormann, C. Sauer, F. Baumann, R. Preiss, L., MacNelly, S., Godoy, P., Wiercinska,<br />
E., Cuiclan, L., Edelmann, J., Zeilinger, K., Heinrich, M., Zanger, U. M., Gebhardt, R.,<br />
Maiwald, T., Heinrich, R., Timmer, J., von Weizsäcker, F., Hengstler, J. G., Primary mouse<br />
hepatocytes for systems biology approaches: a standardized in vitro system for modelling<br />
<strong>of</strong> signal transduction pathways, Syst Biol (Stevenage), 153:433-47, 2006.<br />
[9] Meyers, J., Craig, J., Odde, D. J., Potential for Control <strong>of</strong> Signaling Pathways via Cell Size<br />
and Shape, Current Biology, 16:17:1685-1693, 2006.<br />
[10] Neves, S. R., Tsokas, P., Sarkar, A., Grace, E. A., Rangamani, P., Taubenfeld, S. M., Alberini,<br />
C. M., Schaff, J. C., Blitzer, R. D., Moraru, I. I., Iyengar, R., Cell Shape and Negative Links<br />
in Regulatory Motifs Together Control Spatial Information Flow in Signaling Networks, Cell,<br />
133:4:666-680, 2008.<br />
[11] Rannacher, R., Adaptive finite element discretization <strong>of</strong> flow problems for goal-oriented<br />
model reduction, Computational Fluid Dynamics Review 2010, (M. M. Hafez, K. Oshima,<br />
D. Kwak, eds), 51-70, World Scientific, 2010.<br />
S14.6: Applied analysis, Session C Thu, 16:00–18:00<br />
Chair: Robert Denk S1|03–113<br />
Homogenization on Nonflat Surfaces and Applications<br />
Sören Dobberschütz (<strong>Universität</strong> Bremen) Schedule<br />
The notion <strong>of</strong> periodic unfolding has become a standard tool in the theory <strong>of</strong> periodic homogenization,<br />
which has been applied to many problems. However, all the results obtained so far deal<br />
only with domains or boundaries <strong>of</strong> domains in the flat Euclidean space R n for some n ∈ N. In<br />
the talk, we present a generalization <strong>of</strong> the method <strong>of</strong> periodic unfolding which is applicable to<br />
certain classes <strong>of</strong> compact Riemannian manifolds. The method is then applied to a simple elliptic<br />
model-problem for illustration.<br />
Covering Surfaces with Noncommutative Monodromy Groups and their Industrial<br />
Applications<br />
Irina Dmitrieva (Odessa National Academy <strong>of</strong> Telecommunications, Odessa) Schedule
Section 14: Applied analysis 285<br />
Let an arbitrary algebraic (compact) Riemann surface R be given, and its finite genus ρ ≥ 0. We<br />
are looking for the function f(z, u), (z, u) ∈ R, that is analytic everywhere on R except the finite<br />
set <strong>of</strong> ramification points, has a finite order at infinity and its values undergo the m-dimensional<br />
permutations when come around these ramification points.<br />
The search <strong>of</strong> such multi-valued (here is m-valued) function by its monodromy group that<br />
is described by the ramification points and respective permutations, leads to the solution <strong>of</strong> the<br />
corresponding homogeneous vector Riemann problem with the boundary condition:<br />
F + (t, v) = M(t, v)F − (t, v), (t, v) ∈ L =<br />
M(t, v) =<br />
n�<br />
Miδ(t, v; Li), D −1 |(F ).<br />
i=1<br />
n�<br />
i=1<br />
Li, Lj<br />
� Lk = ∅, (j �= k);<br />
Here: F = F (z, u) = {Fj(z, u)} m j=1 is the class <strong>of</strong> unknown m-dimensional vector-valued functions<br />
that are analytic everywhere on surface R outside the finite system <strong>of</strong> open contours L whose<br />
endpoints are the original ramification points; F are bounded at the endpoints <strong>of</strong> L, extend to<br />
it H-continuously from the left and right, have the finite order at infinity and F ± (t, v) are the<br />
limited values <strong>of</strong> F at L from the left and right respectively; Mi(i = 1, n) is the so called m × m<br />
permutation matrix that is raised by the appropriate permutation from the aforesaid monodromy<br />
group and δ is the Kronecker symbol; D is the m-dimensional vector-valued divisor <strong>of</strong> infinities<br />
and F is divisible by it. Each the sought for scalar component Fj(z, u) (j = 1, n) is the jth branch<br />
<strong>of</strong> the initially wanted multi-valued function f(z, u).<br />
The explicit solution <strong>of</strong> the given problem generates the construction <strong>of</strong> the relevant algebraic<br />
equation <strong>of</strong> the covering with respect to the surface R. The last fact and the corresponding matrix<br />
Riemann problem have the majority <strong>of</strong> industrial applications in technical electrodynamics, optics,<br />
acoustics, various wave propagation, etc., and are interesting mostly in the noncommutative case<br />
that is studied here.<br />
We suggest also some illustrative examples <strong>of</strong> the covering surfaces’ construction with noncommutative<br />
monodromy groups, and whose corresponding algebraic equations have direct industrial<br />
applications.<br />
Backscatter data in electric impedance tomography<br />
Stefanie Hollborn, Martin Hanke (<strong>Universität</strong> Mainz), Nuutti Hyvönen (Aalto University) Schedule<br />
This talk presents the concept <strong>of</strong> backscatter data in electric impedance tomography. These sparse<br />
data are the analogue to so-called backscattering data in inverse scattering. They arise in practice<br />
if the same single pair <strong>of</strong> electrodes is used to drive currents and measure voltage differences<br />
subsequently at various locations on the boundary <strong>of</strong> the object to be imaged. A single insulating<br />
cavity within an otherwise homogeneous object is uniquely determined by its backscatter data.<br />
However, this is in general not true for a perfectly conducting inclusion. The talk presents the<br />
uniqueness pro<strong>of</strong> for an insulating cavity, and it outlines a reconstruction algorithm based thereon.<br />
Furthermore, the non-uniqueness for perfect conductors is illustrated by an example. The<br />
results presented here arise from joint research with Martin Hanke and Nuutti Hyvönen.
286 Section 15: Applied stochastics<br />
Section 15: Applied stochastics<br />
Organizers: Steffen Dereich (<strong>Universität</strong> Marburg), Hanno Gottschalk (Bergische <strong>Universität</strong><br />
Wuppertal)<br />
S15.1: Applied Stochastics Wed, 13:30–15:30<br />
Chair: Hanno Gottschalk S1|02–344<br />
Almost Sure Stability Criterion for Parametric Roll in Random Seas Based on Top<br />
Lyapunov Exponent<br />
Leo Dostal, Edwin Kreuzer (TU Hamburg-Harburg), Navaratnam Sri Namachchivaya (University<br />
<strong>of</strong> Illinois at Urbana-Champaign) Schedule<br />
A criterion for the stability <strong>of</strong> the upright position <strong>of</strong> a ship in random head or following waves<br />
is presented. Such waves lead to parametric excitation <strong>of</strong> roll motion due to periodic variations<br />
<strong>of</strong> righting lever. The development <strong>of</strong> simple criteria for occurrence <strong>of</strong> parametric induced roll<br />
motion in random seas is <strong>of</strong> major interest for improvement <strong>of</strong> the international code on intact<br />
stability provided by the International Maritime Organization. The criterion is based on calculation<br />
<strong>of</strong> the top Lyapunov exponent using the fact, that a negative top Lyapunov exponent yields<br />
no roll motion. With this criterion, roll motion is excluded for specific sea states.<br />
The Analysis <strong>of</strong> Stochastic Fiber Lay-Down Models: Geometric Formulation, Operator<br />
Semigroups and Convergence to Equilibrium<br />
Patrik Stilgenbauer, Martin Grothaus (TU Kaiserslautern) Schedule<br />
The so called fiber lay-down models arise in the production process <strong>of</strong> nonwovens. These new<br />
mathematical models have been developed in recent years and provide an interesting interplay<br />
between functional analysis, stochastics and differential geometry. The models are <strong>of</strong> stochastic<br />
nature and can precisely be formulated in a geometric language as stochastic differential equations<br />
on manifolds. An important criterion for the quality <strong>of</strong> the nonwoven material is how the solution<br />
to the associated Fokker-Planck equations converges towards its stationary state. Especially, one<br />
is interested in determining the speed <strong>of</strong> convergence. Thus the analytic study <strong>of</strong> the models<br />
yields to the investigation <strong>of</strong> their corresponding Kolmogorov- and Fokker-Planck operators. To<br />
solve the Cauchy problems we make use <strong>of</strong> the theory <strong>of</strong> operator semigroups. Techniques from<br />
the theory <strong>of</strong> Dirichlet forms as well as hypocoercivity are used for analyzing the convergence<br />
to equilibrium. Summarizing, the models show up a fascinating interaction between applied and<br />
pure mathematics.<br />
A Smooth 3D Model for Fiber Lay-down Processes<br />
Johannes Maringer, Axel Klar, Patrik Stilgenbauer (<strong>Technische</strong> <strong>Universität</strong> Kaiserslautern), Raimund<br />
Wegener (Fraunh<strong>of</strong>er ITWM Kaiserslautern) Schedule<br />
We present an improved three dimensional stochastic model concerning the fiber lay-down in the<br />
production process <strong>of</strong> nonwoven materials. The model describes the position <strong>of</strong> the deposited fibers<br />
on a conveyor belt, which is determined by a system <strong>of</strong> stochastic differential equations. Here<br />
we remove a drawback <strong>of</strong> a previous 3D model, that is the non-smoothness <strong>of</strong> the fiber paths.<br />
Besides the derivation <strong>of</strong> the smooth 3D model we show its connection to the non-smooth model<br />
in a white noise limit.<br />
Brownian Dynamics <strong>of</strong> Rigid Body by Fluctuating Hydrodynamic Equations<br />
Anamika Pandey, Axel Klar, Sudarshan Tiwari (TU Kaiserslautern) Schedule
Section 15: Applied stochastics 287<br />
The current work focuses on a meshfree simulation for the Brownian dynamics <strong>of</strong> rigid body in<br />
an incompressible viscous fluid. The Brownian dynamics <strong>of</strong> rigid body is demonstrated by fluctuating<br />
hydrodynamic equations coupled with the equation <strong>of</strong> motion for rigid body. The rigid<br />
body accomplishes random motion through the hydrodynamic force acting on its surface from<br />
the surrounding fluid. Fluctuation is incorporated in fluid equation via random stress.<br />
The used meshfree method is a promising numerical approach to simulate multiphase flow and<br />
irregular geometries. Though, it is challenging to work in a meshfree framework with stochastic<br />
partial differential equations(SPDEs) but it has advantage to deal interface boundary in fluid-solid<br />
interaction and in many future application such as study <strong>of</strong> complex fluid. A successful meshfree<br />
scheme for the simulation <strong>of</strong> fluctuating hydrodynamic equations in the case <strong>of</strong> compressible<br />
flow has been presented by Pandey et al. [2]. The previous study by Sharma and Patankar [1]<br />
for investigating Brownian dynamics by fluctuating hydrodynamic equations neglects the inertia<br />
term and focuses on resultant Stokes problem. Furthermore, the fluid-solid domain is considered<br />
to be a fluid and fixed grid method is employed for spatial discretization.<br />
The mathematical formulation in present study can be described as:<br />
• The fluid flow is modeled by Landau-Lifshitz-Navier-Stokes equation.<br />
• No body force was applied either in the particle domain or the fluid domain. However,<br />
the force due to random stress induces fluctuation in fluid, which will lead to Brownian<br />
dynamics <strong>of</strong> rigid body.<br />
• Compute forces on the surface <strong>of</strong> rigid body due to surrounding fluid.<br />
• Newton-Euler equations modeled the motion <strong>of</strong> rigid body.<br />
Unlike the conventional Brownian dynamics type approaches, the random term is incorporated<br />
in fluid equation to capture the Brownian dynamics <strong>of</strong> rigid body.<br />
[1] N. Sharma and N. A. Patankar. Direct numerical simulation <strong>of</strong> the Brownian motion <strong>of</strong><br />
particles by using fluctuating hydrodynamics equations. J. Comput. Phys. 201(2) : 466-<br />
486, 2004.<br />
[2] A. Pandey, A. Klar and S. Tiwari. Meshfree Method for the Stochastic Landau-Lifshitz<br />
Navier-Stokes Equations. Proc. II International Conference on Particle-based Methods Fundamentals<br />
and Applications (2011).<br />
Strong approximation <strong>of</strong> the Cox-Ingersoll-Ross process<br />
S. Dereich (<strong>Universität</strong> Marburg/<strong>Universität</strong> Münster), A. Neuenkirch (TU Kaiserslautern), L.<br />
Szpruch (Oxford University) Schedule<br />
We analyze strong approximation <strong>of</strong> the Cox-Ingersoll-Ross (CIR) process in the regime where<br />
the process does not hit zero by a positivity preserving drift-implicit Euler-type method. As an<br />
error criterion we use the p-th mean <strong>of</strong> the maximum distance between the CIR process and its<br />
approximation on a finite time interval. We show that under mild assumptions on the parameters<br />
<strong>of</strong> the CIR process the proposed method attains, up to a logarithmic term, convergence <strong>of</strong> order<br />
1/2.
288 Section 15: Applied stochastics<br />
S15.2: Applied Stochastics Wed, 16:00–18:00<br />
Chair: Steffen Dereich S1|02–344<br />
Fixed design regression estimation based on experimental and artificially generated<br />
data.<br />
Dmytro Furer, Michael Kohler (TU <strong>Darmstadt</strong>) Schedule<br />
In this article we study least squares estimates based on experimental and artificially generated<br />
data. The artificially generated data comes from already undertaken estimates on the basis <strong>of</strong><br />
similar experiments. It is investigated under which condition the rate <strong>of</strong> convergence <strong>of</strong> least<br />
squares estimates applied to this data is better then the rate <strong>of</strong> convergence <strong>of</strong> least squares<br />
estimates applied to the experimental data.<br />
Estimation <strong>of</strong> the optimal design <strong>of</strong> a nonlinear parametric regression problem via<br />
Monte Carlo experiments<br />
Ida Hertel, Michael Kohler (TU <strong>Darmstadt</strong>) Schedule<br />
A Monte Carlo method for estimation <strong>of</strong> the optimal design <strong>of</strong> a nonlinear parametric regression<br />
problem is presented. The basic idea is to produce via Monte Carlo values <strong>of</strong> the error <strong>of</strong> a<br />
parametric regression estimate for randomly chosen designs and randomly chosen parameters and<br />
to use nonparametric regression to estimate from this data the design for which the maximal<br />
error with respect to all possible parameter values is minimal. A theoretical result concerning<br />
consistency <strong>of</strong> this estimate <strong>of</strong> the optimal design is presented and the method is used to find an<br />
optimal design for an experimental fatigue test.<br />
Keywords and phrases: Optimal design, nonparametric regression, consistency.<br />
On the statistical performance <strong>of</strong> optimizers applied to random processes and fields<br />
Hanno Gottschalk (<strong>Universität</strong> Wuppertal) Schedule<br />
As a mean to measure and compare performance and robustness <strong>of</strong> optimization algorithms, we<br />
apply them to Gaussian random fields in d=1,2.
Section 16: Optimization 289<br />
Section 16: Optimization<br />
Organizers: Florian Jarre (<strong>Universität</strong> Düsseldorf), Arnd Rösch (<strong>Universität</strong> Duisburg-Essen)<br />
S16.1: Shape optimization and forming processes Tue, 13:30–15:30<br />
Chair: Arnd Rösch S1|01–A3<br />
A second order approximation technique for robust shape optimization<br />
Adrian Sichau, Stefan Ulbrich (TU <strong>Darmstadt</strong>) Schedule<br />
We present a second order approximation for the robust counterpart <strong>of</strong> general uncertain nonlinear<br />
programs with state equation given by a partial differential equation. We show how the approximated<br />
worst-case functions, which are the essential part <strong>of</strong> the approximated robust counterpart,<br />
can be formulated as trust-region problems that can be solved efficiently. Also, the gradients <strong>of</strong><br />
the approximated worst-case functions can be computed efficiently combining a sensitivity and<br />
an adjoint approach. However, there might be points where the approximated worst-case functions<br />
are nondifferentiable. This is referred to as the hard case. Hence, we introduce an equivalent<br />
formulation <strong>of</strong> the approximated robust counterpart, in which the objective and all constraints<br />
are differentiable functions. This method is applied to shape optimization in structural mechanics<br />
in order to obtain optimal solutions that are robust with respect to uncertainties in acting forces<br />
and other quantities. Numerical results are presented.<br />
Mesh Regularization in parameter-free Shape Optimization<br />
E. Stavropoulou, M. Hojjat, R. Wüchner, K.-U. Bletzinger (TU München) Schedule<br />
In parameter-free shape optimization, no relation between the different degrees <strong>of</strong> freedom is established<br />
and the design variables are the position <strong>of</strong> the finite element nodes. This gives a great<br />
flexibility in exploring the design space. However, special care has to be given in preventing the<br />
quality <strong>of</strong> the surface mesh. For this, an in-plane-regularization method is established. Moreover,<br />
the computed gradients are usually noisy and contain spurious modes which have to be removed<br />
for several reasons such as mesh dependency and manufacturing limits. To remove this problem,<br />
an out <strong>of</strong> plane regularization method is integrated in the optimization process.<br />
More precisely, the in-plane regularization is a global method which regularizes the finite element<br />
mesh to a desired condition [1],[2]. In this method, an artificial stress field is applied on the surface<br />
or on the volume mesh and a global linear system <strong>of</strong> equations is solved. The applied stress adapts<br />
each element towards a desired predefined template geometry and at the end a globally smooth<br />
mesh is achieved. In this way both the shape and the size <strong>of</strong> each element is effectively controlled.<br />
On the other hand, in out <strong>of</strong> plane regularization the sensitivity field is smoothened with a local<br />
method. Here, non-parametric regression is used and the continuous sensitivity field is established<br />
by convolving the gradients with a kernel function.<br />
The optimization framework as well as the position <strong>of</strong> these modules in the optimization chain<br />
is presented. Various examples which motivate the use <strong>of</strong> the aforementioned methods are shown<br />
and the application <strong>of</strong> the overall methods in fluid and fluid-structure interaction problems is<br />
demonstrated.<br />
[1] K.-U. Bletzinger, R. Wüchner, F. Daoud and N. Camprubi, Computational methods for form<br />
finding and optimization <strong>of</strong> shells and membranes, Computer Methods in Applied Mechanics<br />
and Engineering 194(30-33) (2005), 3438-3452.<br />
[2] R. Wüchner, K.-U. Bletzinger, Stress-adapted numerical form finding <strong>of</strong> pre-stressed surfaces<br />
by the updated reference strateg, International journal for numerical methods in engineering
290 Section 16: Optimization<br />
64(2) (2005), 143-166.<br />
Multipoint Aerodynamical Global Shape Optimization <strong>of</strong> the Flying Configurations<br />
with Spanwise Movable Leading Edge Flaps, in Supersonic Flow<br />
Adriana Nastase (RWTH Aachen) Schedule<br />
The aerodynamical multipoint global optimization (GO) <strong>of</strong> the shape <strong>of</strong> a flying configuration<br />
(FC), fitted with leading edge flaps movable in spanwise direction, leads to two enlarged variational<br />
problems at two different cruising Mach numbers.Let us further suppose that the surfaces<br />
<strong>of</strong> the wing, <strong>of</strong> the fuselage and <strong>of</strong> the flaps <strong>of</strong> FC in open position are approximated in form <strong>of</strong><br />
different superpositions <strong>of</strong> homogeneous polynomes in two variables.The coefficients <strong>of</strong> these polynomes<br />
and the similarity parameters <strong>of</strong> the planforms <strong>of</strong> the FC, flying with movable leading edge<br />
flaps in closed and, respectively, in open position, are the parameters <strong>of</strong> optimization. Meshless<br />
discontinuous hybrid numerical solutions for the full Navier-Stokes layer (NSL) are used here as<br />
start solutions for the GO shape <strong>of</strong> FC. These NSL’s solutions use own analytical hyperbolic potential<br />
solutions <strong>of</strong> the flow over the same FC twice. Firstly, as outer flow, at the NSL’s edge and,<br />
secondly, the velocity’s components are products between the corresponding potential velocities<br />
and polynomial expansions with arbitrary coefficients, which are used to satisfy the NSL’s PDEs.<br />
The first enlarged variational problem consists in the determination <strong>of</strong> the GO shape <strong>of</strong> the surface<br />
and <strong>of</strong> the similarity parameters <strong>of</strong> the planform <strong>of</strong> FC, flying with the flaps in retracted position,<br />
which is <strong>of</strong> minimum drag, at the higher supersonic cruising Mach number. The constraints are:<br />
the lift and the pitching moment coefficients <strong>of</strong> FC are given, the Kutta condition on the subsonic<br />
leading edges <strong>of</strong> the wing is fulfilled, the relative volumes <strong>of</strong> the wing and <strong>of</strong> the fuselage are given,<br />
the leading edges are sharp and the integration conditions along the junction lines wing/fuselage<br />
are fulfilled (i.e. the wing and the fuselage have same tangent planes along their junction lines).<br />
The second variational problem consists in the determination <strong>of</strong> the shape <strong>of</strong> the surface and <strong>of</strong><br />
the planform <strong>of</strong> the leading edge flaps, in such a manner that the entire FC, with the flaps in open<br />
position, is <strong>of</strong> minimum drag at the second, lower supersonic cruising Mach number. The value<br />
<strong>of</strong> the lift and pitching moment coefficients <strong>of</strong> the FC and the relative volume <strong>of</strong> the flaps are<br />
given. The iterative optimum-optimorum theory <strong>of</strong> the author is used for the multipoint global<br />
optimization <strong>of</strong> the FC’s surface and <strong>of</strong> the similarity parameters <strong>of</strong> the planforms <strong>of</strong> the FC with<br />
flaps in open and in retracted position.<br />
Keywords: 76N25 Flow control and optimization, 76D05 Navier-Stokes equations,76J20 Supersonic<br />
flow. (2010 MSC)<br />
Optimal control <strong>of</strong> hydr<strong>of</strong>orming processes<br />
Daniela Koller, Stefan Ulbrich (TU <strong>Darmstadt</strong>) Schedule<br />
The sheet metal hydr<strong>of</strong>orming process is a complex forming process, which involves contact, friction<br />
and plasticity to manufacture complex curved sheet metals with bifurcated cross section.<br />
These sheet metals are examined within the framework <strong>of</strong> the Collaborative Research Centre<br />
(CRC) 666. Mathematically, the sheet metal hydr<strong>of</strong>orming process leads to a quasi-variational<br />
inequality. We seek for optimal controls for typical control variables, e.g. the time dependent<br />
blank holder force and the fluid pressure.<br />
As a first step derivative-free optimization algorithms were used to control the hydr<strong>of</strong>orming<br />
process. The commercial FEM-s<strong>of</strong>tware ABAQUS is invoked for the simulations. Numerical examples<br />
with appropriate objective functions for this new kind <strong>of</strong> manufacturing process for sheet<br />
metals will be presented.
Section 16: Optimization 291<br />
To reduce the runtime <strong>of</strong> the optimization process, algorithms based on reduced models are<br />
under investigation. In this context we want to use a POD Galerkin approach. Preliminary numerical<br />
results for the reduced order model approach will be presented.<br />
Numerical optimization <strong>of</strong> process parameters for combined quasi-static and impulse<br />
forming<br />
Marco Rozgic (<strong>Universität</strong> der Bundeswehr Hamburg), Farhad Taebi (TU Dortmund), Marcus<br />
Stiemer (<strong>Universität</strong> der Bundeswehr Hamburg) Schedule<br />
Recent results in forming technology indicate that forming limits <strong>of</strong> classical quasi-static forming<br />
processes can be extended by combining them with fast impulse forming. However, in such combined<br />
processes, process parameters have to be chosen carefully, to eventually achieve an increase<br />
in formability. In this work a numerical optimization method is presented to identify process parameters<br />
<strong>of</strong> combined deep drawing and electromagnetic forming. This leads to an extension <strong>of</strong><br />
classical quasi-static forming limits. The parameter space comprises contributions <strong>of</strong> the triggering<br />
current (e.g. frequency, amplitude, damping, etc.), geometric descriptions <strong>of</strong> the tool coil as well<br />
as deep drawing parameters (e.g. drawing radii or tribological parameters). The quality <strong>of</strong> a given<br />
parameter set is determined by computing the distance <strong>of</strong> the simulated forming result to the<br />
prescribed ideal shape. A finite element simulation <strong>of</strong> the combined process computes the target<br />
function. To avoid a large number <strong>of</strong> target function evaluations, a gradient-based optimization<br />
scheme is employed. Forming limits have to be incorporated as constraints to the optimization<br />
process, considering rate dependence and prestrain in the second impulse forming step.<br />
Geometry Optimization <strong>of</strong> Branched Sheet Metal Products<br />
Thea Göllner, Wolfgang Hess, Stefan Ulbrich (TU <strong>Darmstadt</strong>) Schedule<br />
We consider the geometry optimization <strong>of</strong> hydr<strong>of</strong>ormed branched sheet metal products, which<br />
can be produced integrally and continuously using the new technologies <strong>of</strong> linear flow splitting<br />
and linear bend splitting. These are explored within the framework <strong>of</strong> the Collaborative Research<br />
Centre (CRC) 666.<br />
The geometry <strong>of</strong> such products can be parameterized by means <strong>of</strong> free form surfaces whereas their<br />
mechanical behaviour is described by the three dimensional linear elasticity equations.<br />
The associated PDE-constrained problem for optimizing the stiffness <strong>of</strong> the structure is formulated.<br />
An algorithm for solving this problem using exact constraints and a globalization strategy<br />
based on adaptive cubic regularization is presented. Numerical results for an example are given.<br />
S16.2: Applied optimization Tue, 16:00–18:00<br />
Chair: Arnd Rösch S1|01–A3<br />
Parameter identification based on multiple inhomogeneous experiments <strong>of</strong> practical<br />
relevance<br />
D. Schellenberg (Deutsches Institut für Kautschuktechnologie), J. Ihlemann (TU Chemnitz),<br />
D. Juhre (Deutsches Institut für Kautschuktechnologie) Schedule<br />
The quality and validity <strong>of</strong> FEM simulations is limited by the suitability <strong>of</strong> the used material model<br />
and its related material parameters. Especially in the field <strong>of</strong> rubber materials high advanced<br />
material models have been developed. Therefore, disadvantages <strong>of</strong> current standard procedures<br />
to identify material parameters have gained in importance.
292 Section 16: Optimization<br />
Usually, current available procedures are based on experiments with simple test specimens.<br />
Furthermore, the load distribution is approximately homogeneous. Of course, this results in low<br />
computational costs and allows to directly characterize the material behaviour. Unfortunately,<br />
the restriction to homogenous experiments leads to losses in the reliability <strong>of</strong> the identified parameters.<br />
On the one hand, there are only few feasible experiments, which produce homogeneous<br />
or almost homogeneous load distributions. On the other hand, deviations from homogeneity and<br />
their consequences cannot be avoided and are <strong>of</strong>ten ignored.<br />
In this work, we present a solution algorithm, which takes several different experimental results<br />
into account. Thereby, the experiments are performed on specimens which respond with<br />
inhomogeneous distributions <strong>of</strong> strains and stresses. The restriction to homogeneous loads is not<br />
necessary. Thus, it is possible to use different measurement results <strong>of</strong> multiple load cases on one<br />
and the same test specimen. The intentional design <strong>of</strong> the specimen permits to consider the specific<br />
properties <strong>of</strong> product groups and load types already during the identification process. In<br />
addition, the effect <strong>of</strong> the manufacturing process on the final material properties can be incorporated.<br />
Reducing the Model-Data Misfit in a Marine Ecosystem Model Using Periodic Parameters<br />
and Linear Quadratic Optimal Control<br />
Mustapha El Jarbi, Thomas Slawig (<strong>Universität</strong> Kiel), Andreas Oschlies (Leibniz-Institut für<br />
Meereswissenschaften) Schedule<br />
This paper presents the application <strong>of</strong> the Linear Quadratic Optimal Control (LQOC) method for<br />
a parameter optimization problem in a marine ecosystem model. The ecosystem model simulates<br />
the distribution <strong>of</strong> nitrogen, phytoplankton, zooplankton and detritus in a water column with<br />
temperature and turbulent diffusivity pr<strong>of</strong>iles taken from a three-dimensional ocean circulation<br />
model. Marine ecosystem models are coupled systems <strong>of</strong> partial differential equations (PDEs) consisting<br />
<strong>of</strong> time-dependent advection-diffusion-reaction equations with nonlinear coupling terms.<br />
The turbulent diffusivity, temperature and salinity fields are either computed simultaneously or<br />
in advance by a physical ocean model. Clearly, the second variant is computationally cheaper but<br />
neglects the biology’s feedback effects via impacts on the absorption <strong>of</strong> solar radiation, generally<br />
assumed to be small relative to uncertainties in the boundary conditions such as surface heat<br />
fluxes. The model uses the ocean circulation and temperature field in an <strong>of</strong>f-line mode, i.e. these<br />
are used only as forcing, but no feedback on them is modeled. The model simulates one water<br />
column at a given horizontal position, which is motivated by the fact that there have been special<br />
time series studies at fixed locations, one <strong>of</strong> which was used here. We present a linearization<br />
method which is based on the available observations. The linearization is necessary to apply the<br />
LQOC method on the nonlinear system <strong>of</strong> state equations. We derive the linearized time-variant<br />
problems and two algebraic Riccati Equations. By using the LQOC method, we are able to introduce<br />
temporally varying periodic model parameters and to significantly improve – compared<br />
to the use <strong>of</strong> constant parameters – the fit <strong>of</strong> the model output to given observational data.<br />
An Approach to Incremental Support Vector Machine Learning Algorithm for Classification<br />
Kaboon Thongtha (King Mongkut’s Institute <strong>of</strong> Technology Ladkrabang, Thailand) Schedule<br />
Incremental learning techniques are important tools to operate information data from internet<br />
updating achieves faster. Support Vector Machine (SVM) duties well for incremental learning<br />
model with impressive performance for its prominent power to summarize the data space in a<br />
short way. This research proposes a heuristic algorithm to incremental learning with SVM taking
Section 16: Optimization 293<br />
the possible effect <strong>of</strong> new training data to history data into account. The partition different set<br />
has fewer elements, and existing hyperplane is closer to the optimal one is used in the algorithm.<br />
The modified support vectors in the algorithm comprise <strong>of</strong> existing support vector, partition<br />
difference set <strong>of</strong> new training data and history data by adding partition difference sets and reduce<br />
the computation process by creating new classification <strong>of</strong> hyperplane on support vector set. The<br />
examples show that algorithm is effective to develop the classification precision.<br />
Son<strong>of</strong>usion: EA optimisation <strong>of</strong> acoustic resonator<br />
Markus J. Stokmaier, Andreas G. Class, Thomas Schulenberg (KIT), Richard T. Lahey Jr. (Rensselaer<br />
Polytechnic Institute) Schedule<br />
Describing imploding cavitation bubbles in a liquid excited by standing sound waves in terms <strong>of</strong><br />
continuum mechanics allows the formation <strong>of</strong> concentric supersonic shock fronts in the vapourfilled<br />
bubble’s inside and represents a mathematical singularity. This implies extreme pressures<br />
and temperatures when the shock reaches the center. The energy-focussing capability <strong>of</strong> the<br />
singularity is confirmed through experimental observation <strong>of</strong> accompanying sonoluminescence<br />
(SL) flashes with spectra corresponding to black body radiation <strong>of</strong> up to 2 · 10 4 K [1]. However,<br />
due to the plasma’s opaqueness and small mass, experiment-based estimation <strong>of</strong> peak plasma<br />
conditions is extremely difficult. Estimations from first principles have substantial difficulties in<br />
modeling the extreme equations <strong>of</strong> state and with simulations <strong>of</strong> molecular dynamics they share<br />
the problem <strong>of</strong> quantifying the multi-scale energy transport phenomena based on particle collision<br />
and radiation.<br />
Both, theory and experiment suggest the potential <strong>of</strong> reaching fusion conditions at the singularity.<br />
That motivated son<strong>of</strong>usion experiments, i.e. the attempt to detect 2.45 MeV neutrons<br />
and tritium production accompanying SL in deuterated liquids as tracers <strong>of</strong> D-D fusion. These<br />
comprise publications by Taleyarkhan et al. [2,3] starting in 2002 claiming successful experimental<br />
son<strong>of</strong>usion detection, but they are so far lacking independent verification.<br />
The current work is based on 2D-axisymmetric harmonic structural FE simulations <strong>of</strong> the<br />
liquid-filled acoustic resonators used for son<strong>of</strong>usion experiments. We determine a substantial sensitivity<br />
<strong>of</strong> the sound pressure amplitude performance <strong>of</strong> the resonators to a majority <strong>of</strong> the design<br />
parameters. We claim that son<strong>of</strong>usion experiments based on manually manufactured resonators<br />
<strong>of</strong> the current design are not reproducible. Thus they can neither verify nor falsify Taleyarkhan’s<br />
findings.<br />
Our contribution to make son<strong>of</strong>usion experiments reproducible, is the development <strong>of</strong> novel<br />
resonator designs consisting <strong>of</strong> CAD-machinable parts. We present the application <strong>of</strong> evolutionary<br />
algorithms (EA) to the resonator design optimisation problem, which is a high-dimensional multimodal<br />
search task. An own EA approach is presented and compared to the evolution strategy<br />
with covariance matrix adaption (CMA-ES) [4]. For a population size <strong>of</strong> 80 and for the total<br />
number <strong>of</strong> evaluation calls limited to less than 10 4 the own algorithm yields acceptable results<br />
with much higher probability.<br />
[1] K.S. Suslick, D.J. Flannigan, Inside a Collapsing Bubble: Sonoluminescence and the Conditions<br />
During Cavitation, Annu. Rev. Phys. Chem. 59 (2008), 659 – 683.<br />
[2] R.P. Taleyarkhan, C.D. West, J.S. Cho, R.T. Lahey Jr., R.I. Nigmatulin, R.C. Block, Evidence<br />
for Nuclear Emissions During Acoustic Cavitation, Science 295 (2002), 1868.<br />
[3] R.P. Taleyarkhan, J.S. Cho, C.D. West, R.T. Lahey Jr., R.I. Nigmatulin, R.C. Block, Additional<br />
evidence <strong>of</strong> nuclear emissions during acoustic cavitation, Phys. Rev. E 69 (2004),<br />
036109.
294 Section 16: Optimization<br />
[4] N. Hansen, A. Ostermeier, Completely Derandomized Self-Adaptation in Evolution Strategies,<br />
Evolutionary Computation 9 (2001), 159 – 195.<br />
Fuzzy-stochastic models for solving CVRPFD<br />
Yuriy P. Kondratenko, Leonid P. Klymenko, Galyna V. Kondratenko (Petro Mohyla Black Sea<br />
State University, Mykolaiv, Ukraine), Igor P. Atamanyuk (Mykolaiv State Agrarian University,<br />
Mykolaiv, Ukraine) Schedule<br />
In many cases the Vehicle Routing Problem (VRP) can be solved using corresponding mathematical<br />
models, exect optimisation algorithms, operations research methods and mathematical<br />
programming. Problem statement, size <strong>of</strong> set <strong>of</strong> nodes, existing restricitions and assumptions are<br />
main factors which have significant impact to a choise <strong>of</strong> solving heuristic.<br />
The CVRP (Capacitated Vehicle Routing Problem) is considered with focus to VRP for tankerrefuellers<br />
which should provide bunkering operations (BO) for various ships. These ordered ships<br />
may be located in different ports or in different sea points. The efficiency <strong>of</strong> BO is evaluated<br />
by possibility to serve all ordered ships with minimum total length <strong>of</strong> tankers routes and with<br />
maximum possible quantity <strong>of</strong> unloaded fuel.<br />
Comparing modelling results for CVRP with crisp demands based on different heuristic (genetic<br />
algorithm, ant colony models, saving algorithm, sweeping algorithm and other) are under<br />
discussion.<br />
Marine practice shows that very <strong>of</strong>ten the information about fuel demands is uncertain. The<br />
fuzzy logic algorithms (FLA) are designed by authors for solving CVRP with fuzzy demands<br />
(CVRPFD) and for special sets <strong>of</strong> input data. For testing and verification <strong>of</strong> proposed models<br />
authors use fuzzy-stochastic approach.<br />
Among finding <strong>of</strong> this research are: classification <strong>of</strong> conflict situations in CVRPFD, stochastic<br />
simulation models <strong>of</strong> prognoses and real demands for modeling and optimization in uncertainty;<br />
methods for increasing efficiency <strong>of</strong> CVRPFD solving by adjusting critical value <strong>of</strong> satisfaction<br />
level for node-applicant in conflict situations.<br />
Average value <strong>of</strong> critical parameter (desired satisfaction level or preference level) is determined<br />
as 0.5 based on the 10000 fuzzy-stochastic models <strong>of</strong> uncertain demands in one program for each<br />
port (CVRPFD with 32 ports and 8 marine bunkering programs).<br />
Modelling results confirm the efficiency <strong>of</strong> suggested intelligent models and fuzzy-stochastic<br />
approach for solving CVRPFD in marine environment.<br />
The main contribution <strong>of</strong> this research deals with development <strong>of</strong> intelligent models and algorithms<br />
for solving CVRPFD and design <strong>of</strong> fuzzy decision support system (DSS) which suggests<br />
alternative decisions to decision-maker.<br />
Using the Elements <strong>of</strong> Manufacturing Systems Management in the Calculation <strong>of</strong> the<br />
Implementation <strong>of</strong> a Serial-Modular Industrial Robot within a Flexible Work Cell<br />
Designed for Special Applications<br />
Marius Alexandru Rizescu, Silviu Mihai Petrisor (Nicolae Balcescu Land Forces Academy, Sibiu,<br />
Romania) Schedule<br />
Organizing the manufacturing activity with industrial robots is a design activity based on the<br />
synthetic analysis <strong>of</strong> the type <strong>of</strong> production, the type <strong>of</strong> equipments used and the products obtained<br />
within those processes. As part <strong>of</strong> the flexible work cell (F.W.C.), the technological flow<br />
may maintain a certain feature dictated by the operations plan, a situation in which the part<br />
moves either successively from one equipment to another, or randomly, depending on the type <strong>of</strong><br />
parts processed within the cell. The flexibility <strong>of</strong> the work cell serviced by the robot is not given
Section 16: Optimization 295<br />
by the very presence <strong>of</strong> the robot within the work cell, but by the type <strong>of</strong> equipments within the<br />
cell. The flexible work cell stands as a developed manufacturing system, and not only because <strong>of</strong><br />
the fact it is the most recent concept in the field <strong>of</strong> material goods manufacturing, but mostly<br />
because it triggers a significant improvement in the economy <strong>of</strong> the manufacturing process, given<br />
that it is focused on the needs for real and prevailing goods <strong>of</strong> the human society, that is, widely<br />
diversified goods in terms <strong>of</strong> typology which are produced in small quantities. In this paper,<br />
the authors propose a basic design <strong>of</strong> a flexible work cell with a parallel organization, destined<br />
for the spot welding <strong>of</strong> AAV carcasses. The cell is serviced by three industrial TTR robots that<br />
perform spot welding operations on the carcasses flowing on the conveyor belt to each <strong>of</strong> the<br />
robots performing this operation. This paper presents economic issues on the value <strong>of</strong> the robots<br />
comprised by the system, the calculus <strong>of</strong> the entire F.W.C. value, the determination <strong>of</strong> the FWC<br />
static configuration, and evaluates the overall pr<strong>of</strong>itability <strong>of</strong> the cell using elements pertaining<br />
to the mathematical game theory and the graph theory, as well.<br />
S16.3: Semidefinite programs and structural optimization Wed, 13:30–15:30<br />
Chair: Florian Jarre S1|01–A3<br />
Data reduction in magnetic resonance imaging by vector and semidefinite optimization<br />
Gabriele Eichfelder (<strong>Universität</strong> Erlangen-Nürnberg), Matthias Gebhardt (Siemens Healthcare,<br />
Erlangen) Schedule<br />
In parallel transmission applications in magnetic resonance imaging the supervision <strong>of</strong> local specific<br />
absorption rate (SAR), which is a measure <strong>of</strong> the rate at which energy is absorbed by the<br />
body, is crucial. One existing approach is to use electromagnetic simulations including human<br />
anatomical models and to precalculate the electric field distributions <strong>of</strong> each individual channel.<br />
These can be superposed later with respect to certain combined excitations under investigation,<br />
and the local SAR distribution can be evaluated. Local SAR maxima can be obtained by<br />
exhaustive search over all investigated subvolumes <strong>of</strong> the body model.<br />
However, optimizing local SAR in radi<strong>of</strong>requency pulse design using constraints for each subvolume<br />
is impractical due to the large number <strong>of</strong> subvolumes (300 000 up to 1 000 000 subvolumes).<br />
We present in this talk a method for reducing this complexity significantly. From a mathematical<br />
point <strong>of</strong> view the subvolumes are represented by a set <strong>of</strong> matrices and we are interested in the<br />
maximal elements <strong>of</strong> this set with respect to the partial ordering defined by the cone <strong>of</strong> positive<br />
semidefinite matrices, i.e. we have to solve a discrete vector optimization problem.<br />
For a larger effect on the data reduction new matrices are constructed which serve as such<br />
maximal elements and which are then called Virtual Observation Points. For that, the matrices<br />
representing the subvolumes are clustered iteratively by a similarity measure and for each cluster a<br />
new matrix is determined by a linear semidefinite optimization problem. By allowing a predefined<br />
overestimation we reach a significant reduction <strong>of</strong> the number <strong>of</strong> matrices which have to be<br />
considered for a supervision <strong>of</strong> the local SAR maxima.<br />
On the solution <strong>of</strong> the Roothaan equations by nonlinear semidefinite programming<br />
Michael Stingl, Tim Clark (<strong>Universität</strong> Erlangen-Nürnberg), Michal Kocvara (University <strong>of</strong> Birmingham)<br />
Schedule<br />
The Roothaan equations are finite dimensional representations <strong>of</strong> the Hartree-Fock equation, a<br />
well established approximation <strong>of</strong> the time-independent electric Schrödinger equation. It is shown
296 Section 16: Optimization<br />
that introducing the so called density matrix P ∈ S n + with properties<br />
P 2 = 2P, tr(P ) = N<br />
for a given integer N < n, the Roothaan equation can be turned into a nonlinear program <strong>of</strong> the<br />
type<br />
min E(P ) (1)<br />
P ∈Sn tr(P ) = N<br />
P 2 = 2P<br />
where E : S n → R is a non-convex quadratic energy function <strong>of</strong> P . The projection type constraint<br />
P 2 = 2P forces the eigenvalues <strong>of</strong> P to 0 or 2. In order to get rid <strong>of</strong> this integer character <strong>of</strong><br />
the problem, the projection constraint is relaxed and one obtains the nonlinear (non-convex)<br />
semidefinite program<br />
min E(P ) (2)<br />
P ∈Sn tr(P ) = N<br />
0 � P � 2P<br />
which can be solved efficiently by the nonlinear SDP algorithm Pennon. It is shown that due to<br />
properties <strong>of</strong> the energy function E the relaxation (2) is exact under reasonable assumptions and<br />
further that each KKT-point <strong>of</strong> (2) is indeed a solution <strong>of</strong> the Roothaan equations.<br />
The presentation is concluded by discussing a series <strong>of</strong> numerical experiments. It is demonstrated<br />
that instances <strong>of</strong> the Roothaan equations can be successfully treated by the nonlinear SDP<br />
approach, which due to the best knowledge <strong>of</strong> the authors have not been solved in the literature<br />
before by the ’standard’ SCF approach.<br />
Robust Design <strong>of</strong> active trusses via Mixed Integer Semidefinite Programming<br />
Kai Habermehl, Stefan Ulbrich (TU <strong>Darmstadt</strong>) Schedule<br />
This work is an extension <strong>of</strong> Ben-Tal and Nemirovskis approach on Robust Truss Topology Design<br />
to active trusses. Active trusses may use active components (e.g. piezo-actuators) to react on<br />
uncertain loads. We present the implementation <strong>of</strong> optimal positioning <strong>of</strong> active components<br />
within a truss.<br />
The approach is based on a semidefinite programming problem, which is a well-known optimization<br />
approach for robust truss topology design. By introducing actors into the model, it<br />
becomes a nonlinear semidefinite program with binary variables. Discrete-continuous mathematical<br />
optimization problems arise and no state-<strong>of</strong>-the-art solver is known that delivers an efficient<br />
solution method to solve these problems. We use a sequential semidefinite programming approach<br />
within a branch-and-bound-framework to solve the problems.<br />
Different uncertainty sets are analyzed for the robust optimization approach mainly polyhedral<br />
and ellipsoidal uncertainty sets. These different approaches have their specific advantages and<br />
disadvantages. A combined approach seems to be the best way to deal with active elements in<br />
robust truss topology design.<br />
Several solution methods (e.g. Cascading techniques, projection approaches) and numerical<br />
results will be presented.
Section 16: Optimization 297<br />
Improvement <strong>of</strong> classical first-order adjoint sensitivity relations<br />
Daniel Materna, Franz-Joseph Barthold (TU Dortmund) Schedule<br />
Sensitivity analysis plays an important role in structural optimization. Of interest are the changes<br />
in the state variable and a chosen objective functional due to perturbations in the design variables.<br />
In the most cases, only first-order sensitivity relations are considered and higher-order terms are<br />
ignored. Such sensitivity relations yield for large design perturbations just a rough approximation<br />
<strong>of</strong> the true change in the state and objective functionals.<br />
This contribution is concerned with a novel approach for the improvement <strong>of</strong> classical firstorder<br />
sensitivity relations <strong>of</strong> general objective functionals or quantities <strong>of</strong> interest. The improvement<br />
approach is based on an exact variational formulation for the change in the quantity <strong>of</strong><br />
interest due to finite design perturbations. The exact change in the quantity <strong>of</strong> interest can be<br />
expressed in a closed variational form. This formulation is used in order to predict the change in<br />
the quantity <strong>of</strong> interest and yields an improved solution in comparison to the results <strong>of</strong> classical<br />
first-order approximations. We consider a general variational framework and present the application<br />
<strong>of</strong> the proposed approach to shape sensitivity for the model problem <strong>of</strong> nonlinear elasticity.<br />
The capability <strong>of</strong> the proposed framework is demonstrated by means <strong>of</strong> selected computational<br />
examples.<br />
S16.4: Modifications <strong>of</strong> Newton’s method Wed, 16:00–18:00<br />
Chair: Florian Jarre S1|01–A3<br />
On limited memory BFGS with cubic overestimation<br />
Andreas Griewank, Jonathan Fischer, Torsten Bosse (HU Berlin) Schedule<br />
We consider the classical problem <strong>of</strong> minimizing a smooth objective by gradient based variable<br />
metric methods. Assuming Lipschitz-continuity <strong>of</strong> the Hessian on an open neighborhood <strong>of</strong> a<br />
bounded level set we employ the cubic overestimation approach recently (re)developed by Toint<br />
and his collaborators. We establish local and global convergence results. The linear algebra implementation<br />
is based on an iteratively updated eigenvalue decomposition <strong>of</strong> variable rank.<br />
On a two-step method for solving nonlinear equations with nondifferentiable operator<br />
Stepan Shakhno, Halyna Yarmola (Ivan Franko National University <strong>of</strong> L’viv, Ukraine ) Schedule<br />
We consider the problem <strong>of</strong> finding an approximation solution <strong>of</strong> the nonlinear equation<br />
H(x) = F (x) + G(x) = 0, (1)<br />
where F, G : D ⊆ X → Y , F is a Fréchet differentiable operator and G is a continuous operator.<br />
In works [1, 2] the authors considered the one-step iterative method for solving (1) given by<br />
xn+1 = xn − A(xn−1, xn) −1 H(xn), x−1, x0 ∈ D, n = 0, 1, . . . .<br />
Here A(xn−1, xn) = F ′ (xn), A(xn−1, xn) = F ′ (xn) + [xn−1, xn; G], A(xn−1, xn) = [xn−1, xn; H].<br />
In this work we propose the two-step method based on methods with order <strong>of</strong> convergence<br />
1 + √ 2 [3, 4]<br />
xn+1 = xn − A(xn, yn) −1 H(xn),<br />
yn+1 = xn+1 − A(xn, yn) −1 H(xn+1), n = 0, 1, . . . ,<br />
where A(xn, yn) = F ′<br />
� �<br />
xn + yn<br />
+ [xn, yn; G]. A local and semilocal convergence <strong>of</strong> the method<br />
2<br />
(2) in Banach spaces is investigated and an order <strong>of</strong> convergence is obtained. In the semilocal case<br />
(2)
298 Section 16: Optimization<br />
we assume that the divided difference <strong>of</strong> the first order <strong>of</strong> the operator G and the first Frećhetderivative<br />
<strong>of</strong> the operator F satisfy Lipschitz conditions. Additionally, we assume that the second<br />
Fréchet-derivative is Lipschitz continuous in the local case.<br />
[1] I.K. Argyros, A unifying local-semilocal convergence analysis and applications for two-point<br />
Newton-like methods in Banach space, J. Math. Anal. Appl. 298 (2004), 374 – 397.<br />
[2] M.A. Hernandez, M.J. Rubio, The secant method for nondifferentiable operators, Appl. Math.<br />
Lett. 15 (2002), 395 – 399.<br />
[3] S.M. Shakhno, On an iterative algorithm with superquadratic convergence for solving nonlinear<br />
operator equations, J. Comp. Appl. Math. 231 (2009), 222 – 235.<br />
[4] W. Werner, Über ein Verfarhren der Ordnung 1 + √ 2 zur Nullstellenbestimmung, Numer.<br />
Math. 32 (1979), 333 - 342.<br />
An Optimisation Method for Nonsmooth Ojective Functions based on Algorithmic<br />
Differentiation<br />
Sabrina Fiege (<strong>Universität</strong> Paderborn), Andreas Griewank (HU Berlin), Andrea Walther (<strong>Universität</strong><br />
Paderborn) Schedule<br />
Nonsmoothness is a typical characteristic <strong>of</strong> numerous objective function in optimisation that arises<br />
from various applications. The standard approach in algorithmic or automatic differentiation<br />
(AD) is to consider only differentiable functions that are defined by an evaluation program. We<br />
extend this functionality by allowing also the functions abs(), min() and max() during the function<br />
evaluation yielding piecewise differential nonlinear functions. It is shown how these functions<br />
can be approximated locally by a piecewise-linear models. These models will have at most a finite<br />
number <strong>of</strong> kinks between open polyhedra decomposing the function domain. The piecewise linear<br />
model can easily be generated by minor modification <strong>of</strong> the ADOL-C and other standard AD<br />
tools. We will employ it in an adapted gradient based optimisation method was adjusted to the<br />
special properties. This talk presents this nonsmooth optimisation method and first numerical<br />
results.
Section 17: Applied and numerical linear algebra 299<br />
Section 17: Applied and numerical linear algebra<br />
Organizers: Thomas Huckle (TU München), Miroslav Rozloznik (Czech Academy <strong>of</strong> Sciences,<br />
Prague)<br />
S17.1: Tensor methods Tue, 13:30–15:30<br />
Chair: Huckle S1|01–A5<br />
Tensor Network States for the study <strong>of</strong> quantum many-body systems: ground states<br />
and time evolution<br />
Maria Carmen Banuls (MPI Garching) Schedule<br />
The term Tensor Network States has become common in the context <strong>of</strong> numerical studies <strong>of</strong> quantum<br />
many-body problems. It refers to a number <strong>of</strong> families that represent different ansatzes for the<br />
efficient description <strong>of</strong> the state <strong>of</strong> a quantum many-body system. The first <strong>of</strong> these families, Matrix<br />
Product States (MPS), lies at the basis <strong>of</strong> Density Matrix Renormalization Group methods,<br />
which have become the most precise tool for the study <strong>of</strong> one dimensional quantum many-body<br />
systems. Their natural generalization to two or higher dimensions, the Projected Entanglement<br />
Pair States (PEPS) are good candidates to describe the physics <strong>of</strong> higher dimensional lattices.<br />
Other families, like Tree Tensor States can also be understood in terms <strong>of</strong> renormalization procedures.<br />
Quantum information gives us some tools to understand why these families are expected to<br />
be good ansatzes for the physically relevant states, and some <strong>of</strong> the limitations connected to the<br />
simulation algorithms.<br />
In this talk I will introduce some <strong>of</strong> these families from the physical point <strong>of</strong> view. I will also<br />
describe the existing algorithms that make use them to study quantum many-body problems.<br />
Low-rank tensor structure <strong>of</strong> elliptic operators in the TT and QTT formats<br />
Vladimir Kazeev, Oleg Reichmann, Christoph Schwab (ETH Zürich) Schedule<br />
We present recent results on the low-rank tensor structure <strong>of</strong> discretized elliptic operators in the<br />
Tensor Train (TT) and Quantized Tensor Train (QTT) representations. These formats have been<br />
proposed recently for the low-parametric structured representation <strong>of</strong> large-scale tensors. In a<br />
remarkable number <strong>of</strong> problems involving d-dimensional n × . . . × n-vectors they have already<br />
demonstrated the reduction <strong>of</strong> the computational complexity to O � d α n β log γ n � and O � d α log δ n �<br />
with sufficiently small exponents α, β, γ and δ.<br />
We consider a linear elliptic second-order differential operator <strong>of</strong> the form<br />
L = −∇ ⊤ a∇ + b ⊤ ∇ + c,<br />
where a is a diffusion tensor, b is a velocity field and c is a reaction coefficient, in a d-dimensional<br />
hypercube with the homogeneous Dirichlet boundary conditions. We discretize L with the use<br />
<strong>of</strong> the standard multi-linear finite elements with n degrees <strong>of</strong> freedom in each dimension and<br />
study the TT and QTT structure <strong>of</strong> the obtained n d × n d -matrix Lh. For this matrix, under<br />
certain reasonable requirements on coefficients a, b and c, we construct explicit TT and QTT<br />
representations <strong>of</strong> ranks which grow linearly with respect to d and, in some important cases,<br />
are also independent <strong>of</strong> n. This implies that the storage cost <strong>of</strong> Lh is respectively O (d 3 n 2 ) and<br />
O (d 3 log n) in the TT and QTT formats.<br />
The result can be applied to the tensor-structured spatial discretization <strong>of</strong> high-dimensional<br />
problems, such as the Fokker-Planck equation or the Black-Scholes equation in finance.
300 Section 17: Applied and numerical linear algebra<br />
Numerical Methods in Tensor Format Representations<br />
Mike Espig (MPI Leipzig) Schedule<br />
We discuss numerical methods and there convergence in tensor representations with a special<br />
focus on tensor networks. The survey provides all necessary ingredients for applying minimization<br />
methods in a general setting. The important cases <strong>of</strong> target functionals which are linear and<br />
quadratic with respect to the tensor product are discussed in detail. As an example, we consider<br />
the representation rank compression in tensor networks. For the numerical treatment, we use<br />
nonlinear block Gauss-Seidel methods and demonstrate the rate <strong>of</strong> convergence in numerical<br />
tests.<br />
Tensor calculus <strong>of</strong> the Fock operator and associated integrals<br />
Venera Khoromskaia (MPI Leipzig) Schedule<br />
The Hartree-Fock equation is one <strong>of</strong> the basic ab initio models is electronic structure calculations.<br />
Traditional approximation <strong>of</strong> the Fock operator is based on a rigorous analytical precomputation<br />
<strong>of</strong> the two-electron convolution integrals in R 3 in a naturally separable Gaussian orbital basis.<br />
We discuss the novel tensor-structured methods for the numerical solution <strong>of</strong> the Hartree-Fock<br />
equation [3], which can be used as well in other quantum chemistry simulations. These methods<br />
include efficient algorithms for separable representation and calculation <strong>of</strong> the discretized functions<br />
and integral operators in R 3 using the canonical, Tucker and mixed tensor formats. The core <strong>of</strong> our<br />
“black-box” solver is the rank-structured computation <strong>of</strong> the Laplace, nuclear potential, nonlinear<br />
Hartree and the (nonlocal) exchange parts <strong>of</strong> the Fock operator in R 3 , discretized on a sequence<br />
<strong>of</strong> n × n × n Cartesian grids [1,2,5]. The arising 3D and 6D convolution integrals are replaced<br />
by 1D algebraic operations implemented with O(n log n) complexity. The robust rank reduction<br />
algorithm [1] enables usage <strong>of</strong> fine Cartesian grids, yielding high resolution in tensor calculations<br />
which allows arbitrary location <strong>of</strong> atoms in a molecule as in the conventional mesh-free analyticalbased<br />
solution <strong>of</strong> the Hartree-Fock equation.<br />
We demonstrate that tensor methods are as well advantageous in calculation <strong>of</strong> the two-electron<br />
integrals, giving a choice to use the generic set <strong>of</strong> basis functions, including even simple combinations<br />
<strong>of</strong> Slater-type and local finite element basis functions [5]. Based on the quantized tensor<br />
multilinear algebra, our approach reduces the numerical costs to O(N 2 log N) with the storage<br />
size O(N 2 ). Thus, the complexity <strong>of</strong> the calculation <strong>of</strong> the two-electron integrals and <strong>of</strong> the Hartree<br />
and exchange operators is bounded only by the unreducible number <strong>of</strong> coupling parameters,<br />
that is, by the entanglement <strong>of</strong> a molecular system [4]. Numerical results for several moderate<br />
size molecules demonstrate efficiency <strong>of</strong> the tensor-structured methods in electronic structure<br />
calculations.<br />
[1] B.N. Khoromskij and V. Khoromskaia. Multigrid Tensor Approximation <strong>of</strong> Function Related<br />
Arrays. SIAM J Sci. Comp., 31(4), 3002-3026 (2009).<br />
[2] V. Khoromskaia. Computation <strong>of</strong> the Hartree-Fock Exchange in the Tensor-structured Format.<br />
Comp. Meth. in Appl. Math., Vol. 10(2010), No 2, pp.204-218.<br />
[3] B.N. Khoromskij, V. Khoromskaia and H.-J. Flad. Numerical solution <strong>of</strong> the Hartree-Fock<br />
equation in multilevel tensor-structured format. SIAM J Sci. Comp., 33(1), 45-65 (2011).<br />
[4] V. Khoromskaia, B.N. Khoromskij and R. Schneider. Grid-based tensor calculus <strong>of</strong> the twoelectron<br />
integrals with entanglement based complexity, in preparation, <strong>2012</strong>.<br />
[5] V. Khoromskaia, D Andrae and B.N. Khoromskij. Tensor Representation <strong>of</strong> the Fock Operator<br />
in a General Basis, in preparation, 2011.
Section 17: Applied and numerical linear algebra 301<br />
Dynamical low rank approximation in hierarchical tensor formats<br />
Reinhold Schneider, Thorsten Rohwedder (TU Berlin) Schedule<br />
Already known in many body quantum physics the introduction <strong>of</strong> hierarchical tensor formats<br />
as the HT (hierarchical Tucker) format and TT (tensor train) format can be considered as a<br />
significant progress in tensor product approximation and the numerical treatment <strong>of</strong> high dimensional<br />
problems. We will present an analytical framework <strong>of</strong> dynamical low rank approximation<br />
in these formats. This can be directly turned into numerical schemes. We emphasize further on<br />
the space �d i=1 C2 which covers e.g. many body Schrödinger equations and numerical homogenization.<br />
Examples for the computation <strong>of</strong> open shell molecules and high dimensional PDE’s e.g.<br />
Focker Planck equations will be presented.<br />
S17.2: Tensor methods/ Eigenvalues Tue, 16:00–18:00<br />
Chair: Kressner S1|01–A5<br />
Tensorization and Multiscale Problems<br />
Lars Grasedyck (RWTH Aachen) Schedule<br />
We will present our recent findings on the relation between hierarchical tensor representations —<br />
which is basically a multilinear data model — and the multiscale nature <strong>of</strong> problems. As it turns<br />
out, the tensorization <strong>of</strong> a periodic multiscale problem leads trivially to a data-sparse low rank<br />
representation and thus efficient computational techniques. However, even in the non-periodic setting<br />
the model still works and thus gives an algebraic generalisation <strong>of</strong> the periodic case to other,<br />
entirely non-periodic cases. However, the low rank condition — which makes the computations in<br />
the hierarchical format efficient — restricts the applicability to special multiscale problems. It is<br />
thus a technique between the periodic and the non-periodic case. Due to black-box approximation<br />
techniques being available for tensors in the hierarchical format, one can exploit the structure also<br />
in cases where it is not directly visible and analytically hard to derive.<br />
Subspace iteration methods in terms <strong>of</strong> MPS<br />
Konrad Waldherr, Thomas Huckle (TU München) Schedule<br />
In the simulation <strong>of</strong> quantum many-body systems an important task is the computation <strong>of</strong> ground<br />
states (i.e. the eigenvector related to the smallest eigenvalue) As the dimension <strong>of</strong> the underlying<br />
vector space grows exponentially in the number <strong>of</strong> physical sites, one has to consider appropriate<br />
subsets promising both convenient approximation properties and efficient computations. For<br />
1D systems, Matrix Product States (MPS) are in use. Algorithms based on MPS only scale polynomially<br />
in the size <strong>of</strong> the physical system, but still guarantee to approximate ground states<br />
faithfully.<br />
In this talk we consider Krylov-based subspace iteration methods for finding ground states.<br />
These methods are formulated in terms <strong>of</strong> MPS. As the set <strong>of</strong> Matrix product states is not closed<br />
under linear combinations, we need techniques that allow us to project a sum <strong>of</strong> MPS back onto<br />
the MPS space, a highly nonlinear approximation problem. We will show and analyze techniques<br />
to solve such projection problems and apply them to construct iteration methods working on the<br />
MPS space.<br />
Solving nonlinear eigenvalue problems via contour integrals<br />
Wolf-Jürgen Beyn (<strong>Universität</strong> Bielefeld) Schedule<br />
In this talk we report on a numerical method that allows to compute eigenvalues (and associated
302 Section 17: Applied and numerical linear algebra<br />
eigenvectors) <strong>of</strong> a nonlinear eigenvalue problem<br />
A(λ)v = 0, v ∈ C m ,<br />
where the matrix family A(λ) ∈ Cm×m depends analytically on the eigenvalue parameter λ in<br />
some domain Ω ⊂ C.<br />
The method determines all eigenvalues inside a prescribed contour Γ in Ω by evaluating two<br />
integrals<br />
�<br />
1<br />
λ<br />
2πi Γ<br />
j A(λ) −1 rdλ, j = 0, 1<br />
for a number <strong>of</strong> right hand sides r ∈ Cm that exceeds the number <strong>of</strong> eigenvalues inside the contour.<br />
The idea <strong>of</strong> the method results from an application <strong>of</strong> Keldysh’s theorem.<br />
We show how the errors <strong>of</strong> the method depend on the number <strong>of</strong> quadrature points and on<br />
the distance <strong>of</strong> the contour to the spectrum. Several applications are presented to the stability<br />
analysis <strong>of</strong> nonlinear waves in PDEs, where the typical problem is to separate a few isolated<br />
eigenvalues from large eigenvalue clusters related to essential spectrum.<br />
Hierarchically enhanced adaptive finite element methods for PDE eigenvalue/eigenvector<br />
approximations<br />
Agnieszka Miedlar (TU Berlin), Luka Grubišić (University <strong>of</strong> Zagreb), Jeffrey S. Ovall (University<br />
<strong>of</strong> Kentucky ) Schedule<br />
Although adaptive approximation methods have gained a recognition and are well-established,<br />
they frequently do not meet the needs <strong>of</strong> real world applications. In this talk we present a hierarchically<br />
enhanced adaptive finite element method for PDE eigenvalue problems. Starting from the<br />
results <strong>of</strong> Grubišić and Ovall on the reliable and efficient asymptotically exact a posteriori hierarchical<br />
error estimators in the self-adjoint case, we explore the possibility to use the enhanced Ritz<br />
values and vectors to restart the iterative algebraic procedures within the adaptive algorithm.<br />
Using higher order hierarchical polynomial finite element bases, as indicated by Bank and by<br />
Ovall and Le Borne, our method generates discretization matrices whose compressions onto the<br />
complement <strong>of</strong> piecewise linear finite element subspace (in the higher order finite element space)<br />
are almost diagonal. This construction can be repeated for the complements <strong>of</strong> higher (even)<br />
order polynomials and yields a structure which is particularly suitable for designing computational<br />
algorithms with low complexity. We present some preliminary numerical results for both the<br />
symmetric as well as the nonsymmetric eigenvalue problems.<br />
Preconditioning for Allen-Cahn variational inequalities with non-local constraints<br />
Martin Stoll (MPI Magdeburg), Luise Blank (<strong>Universität</strong> Regensburg), Lavinia Sarbu (University<br />
<strong>of</strong> Sussex) Schedule<br />
The solution <strong>of</strong> Allen-Cahn variational inequalities with mass constraints is <strong>of</strong> interest in many<br />
applications. This problem can be solved both in its scalar and vector-valued form as a PDEconstrained<br />
optimization problem by means <strong>of</strong> a primal-dual active set method. At the heart <strong>of</strong><br />
this method lies the solution <strong>of</strong> linear systems in saddle point form. In this talk we propose the use<br />
<strong>of</strong> Krylov-subspace solvers and suitable preconditioners for the saddle point systems. Numerical<br />
results illustrate the competitiveness <strong>of</strong> this approach.<br />
Subspace acceleration for pseudospectral computations<br />
Daniel Kressner (EPF Lausanne) Schedule<br />
The computation <strong>of</strong> pseudospectra and associated quantities (pseudospectral abscissa, H∞ norm)<br />
for large-scale matrices is a computationally challenging task. In this talk, we present a new class
Section 17: Applied and numerical linear algebra 303<br />
<strong>of</strong> algorithms, which employ reduced basis techniques to reduce the computational cost, sometimes<br />
dramatically. If time permits, an application <strong>of</strong> these techniques to parameter-dependent<br />
eigenvalue problems is given.<br />
S17.3: HPC / General Wed, 13:30–15:30<br />
Chair: Rozloznik S1|01–A5<br />
An introduction to Compressed Sensing with an application to low-rank matrix recovery<br />
Massimo Fornasier (TU München), Holger Rauhut (<strong>Universität</strong> Bonn), Rachel Ward (University<br />
<strong>of</strong> Texas, Austin) Schedule<br />
In this talk we illustrate the main principles <strong>of</strong> Compressed Sensing by presenting an iteratively<br />
reweighted least squares algorithm for low-rank matrix recovery from few linear measurements.<br />
Calculation <strong>of</strong> invariant subspaces <strong>of</strong> general matrices using a modified Newton method<br />
Ute Kandler (TU Berlin), Pr<strong>of</strong>. Hubert Schwetlick (TU Dresden) Schedule<br />
We consider a modified Block Newton Method for approximating an invariant subspace X and<br />
the corresponding eigenvalues <strong>of</strong> an arbitrary complex matrix A ∈ C n×n . The method generates<br />
a sequence <strong>of</strong> bases Uk <strong>of</strong> the subspaces (Uk), which approximate the target subspace X . We<br />
show that for a sufficiently good initial approximation U0 the method converges in the sense<br />
that sin(ξk), with ξk = ∡((Uk), X ), converges Q-quadratically to zero under the condition that<br />
the subspace X is simple, i.e., that the eigenvalues which belong to it are separated from the<br />
rest <strong>of</strong> the spectrum. In contrast to the established approach by Beyn, Kless and Thümmler<br />
[2001] we only use the U-update from the Newton method but approximate the eigenvalues by a<br />
generalized Rayleigh quotient matrix so the method can be considered as a Block Rayleigh Quotient<br />
Iteration. Moreover we are able to pro<strong>of</strong> the convergence results direct and without using<br />
standard Newton convergence results by using the angles between the corresponding subspaces<br />
instead <strong>of</strong> their norm differences analogously to the real symmetric case considered in Lösche,<br />
Schwetlick and Timmermann [1998].<br />
On the stability <strong>of</strong> neural networks<br />
Vladimir Kostic, Ljiljana Cvetkovic (University Novi Sad) Schedule<br />
Neural networks relevant to biology represent large and multi-time-scale nonlinear dynamical<br />
systems that contain both the activity and synaptic changes. Such systems form the foundation<br />
for every cognitive task and their complex dynamical behavior has to be very thoroughly<br />
mathematically analyzed.<br />
Inherently, biological networks undergo many parametric perturbations. Thus, it is <strong>of</strong> high importance<br />
to understand their dynamical behavior which, due to activation functions and synaptic<br />
weights, has instabilities.<br />
In this talk we will address the stability conditions that applicable to such large scale problems<br />
that can be obtained through the theory <strong>of</strong> diagonally dominant matrices.<br />
Generalized Least-Squares for Genome-Wide Association Studies<br />
Diego Fabregat-Traver, Paolo Bientinesi (RWTH-Aachen) Schedule<br />
In recent years, genome-wide association studies (GWAS) have become ubiquitous in genomics<br />
and medical genetics. A common approach to perform such studies is the use <strong>of</strong> mixed-effects<br />
models, which involve the solution <strong>of</strong> very large sequences <strong>of</strong> generalized least-squares (GLS)
304 Section 17: Applied and numerical linear algebra<br />
problems. This method requires processing from terabytes up to petabytes <strong>of</strong> data; it is therefore<br />
imperative to design routines capable <strong>of</strong> processing very large sets <strong>of</strong> data while attaining the<br />
highest possible performance.<br />
For multi-core systems, generalized least-squares problems may, for instance, be directly solved<br />
using MATLAB or reduced to a form accepted by LAPACK. Unfortunately, in the context <strong>of</strong><br />
GWAS, these approaches present two critical limitations: 1) they do not exploit the specific<br />
structure <strong>of</strong> GWAS; and 2) they are in-core routines, i.e., they expect data to fit in main memory,<br />
being therefore constrained by the amount <strong>of</strong> available memory. To address the first limitation,<br />
there is the need to carefully design algorithms that exploit the domain-specific properties <strong>of</strong> the<br />
problem; while to overcome the second limitation, a common approach for multi-core systems is<br />
to develop out-<strong>of</strong>-core routines, i.e., routines capable <strong>of</strong> dealing with data stored in disk while still<br />
delivering high performance.<br />
We introduce an algorithm, and the corresponding out-<strong>of</strong>-core routine, that address both shortcomings.<br />
On the one hand, the algorithm takes advantage <strong>of</strong> the specific structure <strong>of</strong> GWAS, a<br />
parametric sequence <strong>of</strong> GLS problems, and doing so it greatly reduces redundant computations.<br />
On the other hand, the out-<strong>of</strong>-core routine is able to deal with very large sets <strong>of</strong> data residing<br />
on disk. As a result, our implementation outperforms existing naive approaches by a factor <strong>of</strong> 5,<br />
being able to sustain such high performance for data sets up to the hard-drive size.<br />
Parallel Computing for Long-Time Simulations <strong>of</strong> Calcium Waves in a Heart Cell<br />
Matthias K. Gobbert (University <strong>of</strong> Maryland, Baltimore) Schedule<br />
The flow <strong>of</strong> calcium ions in a heart cell is modeled by a system <strong>of</strong> time-dependent reaction-diffusion<br />
equations. The highly non-smooth nature <strong>of</strong> the source terms, the large number <strong>of</strong> calcium release<br />
sites requiring high-resolution meshes, and the need for long-time simulations up to large final<br />
times are among the challenges for convergent and efficient numerical methods for this problem.<br />
We will describe the techniques used for long-time simulations <strong>of</strong> this model using sophisticated<br />
time-stepping and a Jacobian-Free Newton-Krylov method. Recent work provides a rigorous<br />
pro<strong>of</strong> for the convergence <strong>of</strong> the finite element method used and demonstrates that the simulator<br />
can produce physiologically correct behavior such as experimentally observed spontaneous spiral<br />
waves. To further improve the ability <strong>of</strong> the simulator, we are leveraging the GPGPUs in each<br />
hybrid node for the Newton-Krylov method in the computational kernel <strong>of</strong> the simulator. GPG-<br />
PUs are ideally suited for this type <strong>of</strong> application, since they can dramatically speed up studies<br />
for long-time simulations, which would take the parallelism <strong>of</strong> several compute nodes to achieve<br />
the same run times.<br />
Parallel Fast Computation <strong>of</strong> Coulomb Interactions Based on Nonequispaced Fourier<br />
Methods<br />
Michael Pippig (TU Chemnitz) Schedule<br />
The evolution <strong>of</strong> charged particle systems is determined by classical Coulomb interactions. Since<br />
the Coulomb potential is long ranged, the number <strong>of</strong> interactions increases quadratically with<br />
the number <strong>of</strong> particles. This makes it impossible to use the direct calculation for large particle<br />
numbers.<br />
Instead, an acceleration can be achieved using fast Fourier transforms at nonequispaced nodes.<br />
For periodic boundary conditions the resulting algorithm is identically to the widely known<br />
particle-particle particle-mesh (P3M) algorithm. Nevertheless, reasonable particle simulations are<br />
still a computationally demanding problem, which can only be tackled with the computing power<br />
<strong>of</strong> massively parallel architectures. Therefore, the algorithm <strong>of</strong> choice must not only be fast but<br />
also massively parallel.
Section 17: Applied and numerical linear algebra 305<br />
During this talk, we give an overview <strong>of</strong> the Fourier based fast calculation <strong>of</strong> Coulomb interactions.<br />
We introduce a s<strong>of</strong>tware library for the massively parallel computation <strong>of</strong> fast Fourier<br />
transforms at nonequispaced nodes. This library forms the key component <strong>of</strong> our algorithm for<br />
the fast and parallel computation <strong>of</strong> Coulomb interactions in particle systems.<br />
S17.4: Matrix Functions / General Wed, 16:00–18:00<br />
Chair: Frommer S1|01–A5<br />
On optimality <strong>of</strong> interpolation-based low-rank approximations <strong>of</strong> large-scale matrix<br />
equations<br />
Tobias Breiten, Peter Benner (MPI Magdeburg) Schedule<br />
In this talk, we will discuss projection-based approximations for the solution <strong>of</strong> Lyapunov equations<br />
<strong>of</strong> the form<br />
AXE T + EXA T + BB T = 0,<br />
with A = A T , E = E T ∈ R n×n and B ∈ R n×m . Recently, in [1] a relation between minimizing the<br />
objective function<br />
f : M → R, X ↦→ XAXE + BB T<br />
on the manifold M <strong>of</strong> symmetric positive semi-definite matrices <strong>of</strong> rank k and the L−norm defined<br />
by the operator<br />
L := E ⊗ A + A ⊗ E<br />
together with the inner product 〈u, v〉L = 〈u, Lv〉 has been shown. While there the minimization<br />
problem was solved by means <strong>of</strong> a Riemannian optimization approach, here we will discuss an<br />
interpolation-based method which leads to the same results but relies on projecting the original<br />
Lyapunov equation onto a smaller subspace. It will turn out that this can be achieved by the<br />
iterative rational Krylov algorithm (IRKA) or, alternatively, by the alternating direction implicit<br />
iteration (ADI) if appropriate shifts are used. Besides a generalization for the case <strong>of</strong> A �= A T , we<br />
will also discuss an extension for more general Sylvester equations <strong>of</strong> the form<br />
AXE + F XB + CD = 0,<br />
with A = A T , F = F T ∈ R n×n , B = B T , E = E T ∈ R m×m , C ∈ R n×p and D ∈ R p×m .<br />
[1] B. Vandereycken and S. Vandewalle, A Riemannian optimization approach for computing<br />
low-rank solutions <strong>of</strong> Lyapunov equations, SIAM J. Matrix Anal. Appl. 31(5) (2010), 2553–<br />
2579.<br />
A completely real way <strong>of</strong> dealing efficiently with complex shifts in the low-rank ADI<br />
method<br />
Patrick Kürschner, Peter Benner, Jens Saak (MPI Magdeburg) Schedule<br />
Solving large-scale Lyapunov equations defined by an unsymmetric matrix with the low-rank ADI<br />
method might require complex shift parameters to achieve fast convergence. One <strong>of</strong> our recent<br />
contributions to the low-rank ADI method proposed an efficient way for handling these complex
306 Section 17: Applied and numerical linear algebra<br />
shift parameters. There, the amount <strong>of</strong> complex arithmetic operations corresponding to pairs <strong>of</strong><br />
complex conjugate shift parameters is roughly halved, which also leads to a drastic reduction <strong>of</strong><br />
the required complex storage. The solution <strong>of</strong> onecomplex linear system per complex pair <strong>of</strong> shifts<br />
is the essential remaining task requiring complex computations. This is the starting point <strong>of</strong> this<br />
work, where we investigate an approach to get rid <strong>of</strong> all <strong>of</strong> these remaining complex arithmetic<br />
operations. This makes the method applicable on computing environments where complex computations<br />
and storage are not supported or not efficiently available.<br />
ADI for Tensor Structured Equation<br />
Thomas Mach (MPI Magdeburg ), Jens Saak (MPI Magdeburg and TU Chemnitz) Schedule<br />
We will present an extension <strong>of</strong> the well known ADI method for the solution <strong>of</strong> Lyapunov equations<br />
F X + XF T = −GG T<br />
to higher dimensional problems. The vectorized form <strong>of</strong> the Lyapunov equation is<br />
(I ⊗ F + F ⊗ I)vec(X) = vec(B).<br />
We consider the generalization <strong>of</strong> this equation <strong>of</strong> the form<br />
Avec(X) = (I ⊗ · · · ⊗ I ⊗ A1 + . . . + Ad ⊗ I ⊗ · · · ⊗ I) vec(X) = vec(B).<br />
The tensor train structure is one possible generalization <strong>of</strong> the low rank factorization we find in<br />
the right hand side <strong>of</strong> (1). Therefore we assume B to be <strong>of</strong> tensor train structure. We show that in<br />
analogy to the low rank ADI case the solution X can be generated in tensor train structure, too.<br />
Further we provide an algorithm that computes X using a generalization <strong>of</strong> the ADI method.<br />
FFT-based Finite Element Method for homogenization<br />
Jaroslav Vondřejc, Jan Zeman, Ivo Marek (Czech Technical University Prague) Schedule<br />
We present a mathematical analysis on an FFT-based homogenization algorithm introduced by<br />
Moulinec and Suquet in [1]. This approach is based on the Lippmann-Schwinger type <strong>of</strong> integral<br />
equation including the Green function for some reference homogeneous conductivity being<br />
a parameter <strong>of</strong> the method. We show that this equation is equivalent to weak formulation <strong>of</strong><br />
the unit cell problem in the sense that the solution <strong>of</strong> both formulations is identical. Moreover,<br />
we describe the discretization using Galerkin approximation and numerical integration with the<br />
trigonometric polynomials used as basis functions. The convergence <strong>of</strong> discrete solutions to the<br />
solution <strong>of</strong> weak formulation is presented. The solution <strong>of</strong> resulting non-symmetric linear system<br />
by conjugate gradients is discussed, and it is shown that it results in substantial acceleration <strong>of</strong><br />
the original Moulinec-Suquet scheme, cf. [2].<br />
[1] H. Moulinec and P. Suquet, A fast numerical method for computing the linear and nonlinear<br />
mechanical properties <strong>of</strong> composites, Comptes rendus de l’Académie des sciences. Série II,<br />
Mécanique, physique, chimie, astronomie 318 (1994), no. 11, 1417–1423.<br />
[2] J. Zeman, J. Vondřejc, J. Novák, and I. Marek, Accelerating a FFT-based solver for numerical<br />
homogenization <strong>of</strong> periodic media by conjugate gradients, Journal <strong>of</strong> Computational Physics<br />
229 (2010), no. 21, 8065–8071.<br />
Application <strong>of</strong> Buckingham Pi-theorem to asymmetric plate rolling processes<br />
Tobias Münker, Denis Anders, Kerstin Weinberg (<strong>Universität</strong> Siegen) Schedule<br />
(1)
Section 17: Applied and numerical linear algebra 307<br />
Rolling under asymmetrical conditions such as temperature gradients within the material, difference<br />
<strong>of</strong> the circumferential velocity <strong>of</strong> the rolls and different friction coefficients cause the<br />
rolled slab to bend towards the direction <strong>of</strong> one <strong>of</strong> the rolls. In general this effect is undesired,<br />
since it hinders the further material transport and is a potential danger for the machine components<br />
in the proceeding processes. Unfortunately the essential mechanisms and the sensitivity<br />
<strong>of</strong> the influencing parameters in asymmetric rolling are still not comprehended sufficiently. Here<br />
a novel approach is presented in order to gain an enhanced insight into the front-end bending<br />
phenomenon. To this end Buckingham Pi-theorem is applied to recover dimensionless coefficients<br />
describing the state <strong>of</strong> the roll gap and enable a reduction <strong>of</strong> the number <strong>of</strong> calculations in the<br />
required parametric studies. These parametric studies have been performed applying a finite element<br />
model considering elasto-plastic material behaviour and the boundary conditions applied to<br />
the slab in the roll gap. The dimensionless quantity considering the slab’s curvature is thoroughly<br />
investigated in terms <strong>of</strong> the other dimensionless system parameters.<br />
Error bounds for functions <strong>of</strong> matrices<br />
Andreas Frommer, Karsten Kahl, H. Rittich (<strong>Universität</strong> Wuppertal) Schedule<br />
We consider the task <strong>of</strong> computing f(A)b, where A is a (complex) n × n matrix, f a sufficiently<br />
smooth function defined on an open set containing the spectrum <strong>of</strong> A and b a vector. As it is<br />
common in applications, we assume that A is large and sparse, so that f(A) cannot be computed<br />
directly. Instead we consider the approach to approximate f with a rational function r and to<br />
then use the Lanczos process to iteratively approximate r(A)b. This is a computationally viable<br />
approach, since it relies on short recurrencies.<br />
An important aspect is to obtain reliable stopping criteria for this Lanczos iteration. We show<br />
how to obtain precise stopping criteria, <strong>of</strong>ten yielding to upper bounds on the exact error, by<br />
running a secondary, restarted Lanczos process which can be retrieved very efficiently from the<br />
primary Lanczos iteration. We illustrate the quality <strong>of</strong> our approach with a number <strong>of</strong> examples,<br />
including the matrix exponential and the matrix sign function.<br />
S17.5: Iterative Solvers Thu, 13:30–15:30<br />
Chair: Huckle S1|01–A5<br />
A Deflated Conjugate Gradient Method for Multiple Right Hand Sides and Multiple<br />
Shifts<br />
Sebastian Birk, Andreas Frommer (<strong>Universität</strong> Wuppertal) Schedule<br />
Computations in QCD simulations <strong>of</strong>ten require the solution <strong>of</strong> linear systems that only differ by a<br />
shift with the identity matrix as well as solutions for several different right hand sides. In the past<br />
Krylov subspace methods have been developed which try to exploit either the need for solutions<br />
to multiple right hand sides (e.g. deflation type methods and block methods) or multiple shifts<br />
(e.g. shifted CG) with some success. Though, in some instances (e.g. the Rational Hybrid Monte<br />
Carlo algorithm) the computations even require solutions to linear systems for both multiple<br />
right hand sides and multiple shifts at the same time. In this talk we present a Krylov subspace<br />
method DSBlockCG that, based on a block Lanczos process, exploits both features at once. We<br />
give numerical evidence that our method is superior to applying other iterative methods to each<br />
<strong>of</strong> the systems individually as well as in some cases to shifted or block Krylov subspace methods.<br />
Recycling Krylov subspace information in sequences <strong>of</strong> linear systems<br />
Nemanja Božović (<strong>Universität</strong> Wuppertal) Schedule
308 Section 17: Applied and numerical linear algebra<br />
Many problems in numerical simulations in physics require the solution <strong>of</strong> long sequences <strong>of</strong> slowly<br />
changing linear systems. One problem that is <strong>of</strong> interest to us arises in Lattice QCD simulations,<br />
e.g., while computing masses <strong>of</strong> elementary particles. In each time step, we have to solve a linear<br />
system with a Dirac operator which changes slightly from time step to time step. Based on the<br />
work <strong>of</strong> M. Parks and E. de Sturler [1] we will show how the cost <strong>of</strong> solving subsequent systems<br />
is reduced by recycling selected subspaces generated for previous systems. Furthermore, we have<br />
investigated how the algorithm behaves when we use the solution <strong>of</strong> the previous system as an<br />
initial guess and also, when we use different kinds <strong>of</strong> extrapolations <strong>of</strong> the previous solutions as<br />
an initial guess. We will show these results and the effectiveness <strong>of</strong> the algorithm in comparison<br />
to the algorithm that solves each system separately.<br />
[1] Michael L. Parks, Eric de Sturler, Greg Mackey, Duane D. Johnson and Spandan Maiti,<br />
Recycling Krylov subspaces for sequences <strong>of</strong> linear systems, SIAM Journal on Scientific<br />
Computing, 28(2006), 1651 − 1674<br />
Deflation and Projector Preconditioning in iterative substructuring methods:<br />
Connections and new results<br />
Axel Klawonn, Oliver Rheinbach (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
In this talk, projector preconditioning, also known as the deflation method, is applied to the<br />
FETI-DP iterative substructuring method in order to create a second, independent coarse problem.<br />
This may help to extend the parallel scalability <strong>of</strong> classical FETI-DP methods without<br />
the use <strong>of</strong> inexact solvers and may also be used to improve the robustness, e.g., for almost incompressible<br />
elasticity problems. Connections <strong>of</strong> FETI-DP methods applying a transformation <strong>of</strong><br />
basis using a larger coarse space with a corresponding FETI-DP method using projector preconditioning<br />
are pointed out. It can be shown that the methods have essentially the same spectrum.<br />
Numerical results confirming our theoretical findings are provided.<br />
Exact and Block Factorized Sparse Approximate Inverses based on Kaporin functional<br />
minimization<br />
Matous Sedlacek, Thomas Huckle, Jürgen Bräckle (TU München) Schedule<br />
The talk is concerned with the factorized sparse approximate inverse (FSPAI) preconditioning<br />
technique for symmetric positive definite systems Ax = b. Based on an arbitrary sparsity pattern,<br />
FSPAI automatically captures most pr<strong>of</strong>itable indices to improve on a current approximation<br />
L which satisfies L T L ≈ A −1 . The computation <strong>of</strong> the preconditioner is favorable for high performance<br />
clusters as it can be done column-wise in parallel. A detailed analysis <strong>of</strong> the FSPAI<br />
provides theoretical properties and makes it possible to derive the Exact FSPAI (EFSPAI). This<br />
exact version <strong>of</strong> FSPAI updates its sparsity pattern by indices yielding optimal improvement for<br />
the current approximation. In the second part <strong>of</strong> the talk, we derive the block version <strong>of</strong> FSPAI<br />
(BFSPAI) which allows parallel preconditioning <strong>of</strong> block SPD systems. The presented modifications<br />
inherit the main advantages <strong>of</strong> FSPAI: the computation <strong>of</strong> the preconditioner remains<br />
inherently parallel and no a priori knowledge on the (block) sparsity pattern is required. Finally,<br />
we present a first scalable implementation <strong>of</strong> FSPAI which forms the basis for a future parallel<br />
EFSPAI and BFSPAI implementation.<br />
A GPU implementation <strong>of</strong> the SPAI preconditioner for cardiovascular simulation<br />
William Sawyer, Gilles Fourestey (Swiss National Supercomputing Centre), Radu Popescu (EPL<br />
Lausanne), Carlo Vanini (University <strong>of</strong> Lugano) Schedule
Section 17: Applied and numerical linear algebra 309<br />
It is well known that the sparse approximate inverse preconditioner (SPAI) [1] has particular potential<br />
for high performance computing. Briefly, given a large, sparse system <strong>of</strong> equations Ax = b,<br />
this technique minimizes the Frobenius norm,<br />
�<br />
�<br />
�<br />
�AM − I�F = � n �<br />
�(AM − I)k�2 , (1)<br />
which entails solving n decoupled least squares minimization problems,<br />
k=1<br />
min �<br />
ˆmk<br />
 ˆmk − êk�, (2)<br />
where  is formed by taking only the non-zero entries <strong>of</strong> a A which are relevant for a given<br />
sparsity pattern <strong>of</strong> M. The solution to this minimization is:<br />
ˆmk = R −1 ˜ Q T êk,<br />
with  = QR, the QR decomposition.<br />
We have ported this calculation to graphical processing units (GPUs) within NVIDIA’s CUSP<br />
library [2] for sparse linear algebra. GPUs perform well on dense problems such as QR where data<br />
resides for long periods on the device. Since the minimization problems (2) are independent, they<br />
are mapped to separate thread-blocks. A highly optimized QR algorithm from the MAGMA<br />
library [3] is employed on each.<br />
Traditionally the challenge has been to determine a sparsity pattern for M which reduces the<br />
norm to a degree where M can be successfully applied in an iterative solver such as GMRES.<br />
Due to the extremely high performance <strong>of</strong> the GPU, it is possible to consider initially sparsity<br />
patterns for M much denser than have been previously considered.<br />
Utilizing techniques discussed in [4], we evaluate the resulting preconditioner on Stokes problems<br />
arising from the LifeV s<strong>of</strong>tware [5] for cardiovascular research, and present results for the<br />
time to solution compared with existing preconditioners, as well as the absolute performance in<br />
GFlop/s.<br />
[1] M. J. Grote, T. Huckle, Parallel Preconditioning with Sparse Approximate Inverses, SIAM<br />
Journal on Scientific Computing, 18 (1997), 838–853.<br />
[2] W. N. Bell, M. J. Garland, CUSP: CUDA Sparse linear algebra,<br />
http://code.google.com/p/cusp-library/, 2011.<br />
[3] A. Tomov, J. Dongarra, MAGMA: Matrix Algebra on GPU and Multicore Architectures<br />
http://icl.cs.utk.edu/magma/, 2011.<br />
[4] T. Huckle, A. Kallischko, Frobenius Norm Minimization and Probing for Preconditioning Int.<br />
J. Comp. Math 84(8) (2007), 1225–1248.<br />
[5] A. Crosetto, S. Deparis, G. Fourestey, A. Quarteroni, Parallel Algorithms for Fluid-Structure<br />
Interaction Problems, SIAM Journal on Scientific Computing 33(4) (2011), 1598–1622.<br />
Constructing Sparse Approximate Inverse Block Preconditioner<br />
Thomas Huckle (TU München) Schedule
310 Section 17: Applied and numerical linear algebra<br />
In many applications the matrices related to a linear system <strong>of</strong> equations exhibit a - maybe hidden<br />
- block structure. This block structure should therefore also show up in the preconditioner in order<br />
to derive better approximations. Additionally, in order to reduce the number <strong>of</strong> rather expensive<br />
Least Squares problems that appear in the Frobenius norm minimization minM �AM − I�F , a<br />
blocking <strong>of</strong> column indices related to nearly the same normal equations can save computing time.<br />
Furthermore, blocking allows BLAS3 operations resulting in an additional speedup.<br />
In this talk we will dicussion different blocking strategies und related algorithms in order to<br />
derive improved sparse approximate inverse preconditioners.<br />
S17.6: Iterative Solvers Thu, 16:00–18:00<br />
Chair: Rozloznik S1|01–A5<br />
Stability and Sparsity <strong>of</strong> Frames<br />
Gitta Kutyniok (TU Berlin) Schedule<br />
Frames in finite dimensional spaces have established themselves as a means to derive redundant,<br />
yet stable decompositions <strong>of</strong> a signal for analysis or transmission, while also promoting sparse<br />
expansions. The reconstruction procedure is then based on one <strong>of</strong> the associated dual frames,<br />
which – in the case <strong>of</strong> a tight frame – can be chosen to be the frame itself.<br />
In this talk, we focus on two structural properties <strong>of</strong> frames and their associated sets <strong>of</strong> dual<br />
frames, namely their condition number and the sparsity <strong>of</strong> their vectors. While the first property<br />
is related to stability, the second property ensures low-complexity computations and enables high<br />
compressibility. We will discuss optimality results, provide algorithmic constructions, and finish<br />
with some numerical experiments.<br />
This is joint work with Krahmer (U. Göttingen) and Lemvig (TU Danmark).<br />
Bounds on the range <strong>of</strong> multivariate rational functions by Bernstein expansion with<br />
application to the enclosure <strong>of</strong> the solution set <strong>of</strong> parametric linear systems<br />
Jürgen Garl<strong>of</strong>f, Andrew P. Smith (Hochschule Konstanz) Schedule<br />
The expansion <strong>of</strong> a given n-variate polynomial p into Bernstein polynomials can be used to tightly<br />
bound the range <strong>of</strong> p over an n-dimensional box, see [1, 4]. The interval spanned by the minimum<br />
and the maximum <strong>of</strong> the coefficients <strong>of</strong> this expansion encloses the range. A disadvantage <strong>of</strong> this<br />
approach is that the number <strong>of</strong> the coefficients to be computed explicitly grows exponentially with<br />
the number <strong>of</strong> variables n. In [3] a method was presented by which the number <strong>of</strong> coefficients<br />
which are needed for the enclosure is only approximately linear in the number <strong>of</strong> the terms <strong>of</strong> the<br />
polynomial.<br />
The talk addresses the question <strong>of</strong> the way in which the tight bounds on the range <strong>of</strong> a<br />
polynomial can be employed to construct bounds on the range <strong>of</strong> the ratio <strong>of</strong> two multivariate<br />
polynomials. The naive method <strong>of</strong> bounding the ranges <strong>of</strong> the two polynomials independently<br />
and dividing the two resulting intervals neglects the dependency between the variables <strong>of</strong> the<br />
polynomials and may result in gross overestimation <strong>of</strong> the range.<br />
In our talk, a linearisation technique is presented which leads to much tighter enclosures for<br />
the ranges <strong>of</strong> rational functions.<br />
In the second part <strong>of</strong> our talk, we apply these bounds to the enclosure <strong>of</strong> the solution set <strong>of</strong> a<br />
parametric system <strong>of</strong> linear equations. This is a system <strong>of</strong> linear equations where the coefficients<br />
<strong>of</strong> the matrix and the right hand side depend on parameters which vary within given intervals. We<br />
employ a parametric residual iteration based on interval arithmetic [2] which requires bounding<br />
the range <strong>of</strong> a multivariate rational function over a box. Applications to the verified solution <strong>of</strong>
Section 17: Applied and numerical linear algebra 311<br />
some simple finite element models for truss structures are also presented.<br />
[1] J. Garl<strong>of</strong>f, Convergent bounds for the range <strong>of</strong> multivariate polynomials, in K. Nickel, ed.,<br />
Interval Mathematics 1985, Lecture Notes in Computer Science vol. 212, 37–56. Springer,<br />
Berlin, Heidelberg, New York (1986).<br />
[2] J. Garl<strong>of</strong>f, E. D, Popova, and A. P. Smith, Solving linear systems with polynomial parameter<br />
dependency with application to the verified solution <strong>of</strong> problems in structural mechanics,<br />
in A. Chinchuluun, P. M. Pardalos, R. Enkhbat, and E. N. Pistikopoulos, eds., Proceedings<br />
<strong>of</strong> the International Conference on Optimization, Simulation and Control, Ulaanbaatar,<br />
Mongolia (2010), Series Springer Optimization and Its Applications, Springer-Verlag (to<br />
appear).<br />
[3] A. P. Smith, Fast construction <strong>of</strong> constant bound functions for sparse polynomials, J. Global<br />
Optimization 43 (2–3), 445–458 (2009).<br />
[4] M. Zettler and J. Garl<strong>of</strong>f, Robustness analysis <strong>of</strong> polynomials with polynomial parameter<br />
dependency using Bernstein expansion, IEEE Trans. Automat. Contr. 43, 425–431 (1998).<br />
Using block smoothers in multigrid methods<br />
Matthias Bolten, Karsten Kahl (<strong>Universität</strong> Wuppertal) Schedule<br />
In the context <strong>of</strong> domain decomposition methods usually block smoothers with or without overlap<br />
are used. On parallel computers and nowadays computer architectures block smoothers possess<br />
the advantage <strong>of</strong> a high computation/communication and/or a computation/memory access ratio,<br />
especially when compared to traditional point smoothers. Therefore, multigrid methods should<br />
benefit from the use <strong>of</strong> block smoothers. Nevertheless, numerical results show that block smoothers<br />
are not as efficient as expected when standard coarsening procedures are in effect. We propose<br />
a different coarsening scheme and a new local interpolation for the usage <strong>of</strong> block smoothers in<br />
multigrid methods. Using this scheme, we obtain textbook multigrid efficiency with fast convergence<br />
rate and can thus benefit from the higher amount <strong>of</strong> work that is carried out locally. In this<br />
talk, we will present the resulting method, give an overview over the theoretical foundations and<br />
show numerical results.<br />
Aggregation-based Multilevel Methods for Lattice QCD<br />
Matthias Rottmann, Karsten Kahl (<strong>Universität</strong> Wuppertal) Schedule<br />
In this talk, we present a multigrid solver for application in Quantum Chromodynamics (QCD),<br />
a theory that describes the strong interaction between subatomic particles. In QCD simulations<br />
a substantial amount <strong>of</strong> work is spent in solving Dirac equations on regular grids. These large<br />
sparse linear systems are <strong>of</strong>ten ill conditioned and typical Krylov subspace methods (e.g. CGN,<br />
GCR, BiCGStab) tend to be slow. As a solution to their bad scaling behavior we present an<br />
aggregation based multigrid method with a domain decomposition smoother and show numerical<br />
results for systems up to the size <strong>of</strong> 450 million <strong>of</strong> unknowns.<br />
Adaptive algebraic multigrid methods for Markov chains<br />
Sonja Sokolovic (<strong>Universität</strong> Wuppertal) Schedule<br />
We present an algebraic multigrid approach for computing the state vector <strong>of</strong> an irreducible Markov<br />
chain. The presented method consists <strong>of</strong> two parts: In a multiplicative setup phase based on<br />
the recently introduced bootstrap algebraic multigrid (BAMG) framework, a multigrid hierarchy
312 Section 17: Applied and numerical linear algebra<br />
is developed in an adaptive fashion and a first approximation to the desired state vector is computed.<br />
In the second part <strong>of</strong> the method, the multigrid hierarchy is used for preconditioning a<br />
Krylov subspace iteration that further improves the approximation to the state vector. In our<br />
approach, we propose some modifications to the basic BAMG framework, in particular to the<br />
least squares based computation <strong>of</strong> the interpolation operator, which in some cases, especially for<br />
large, unstructured problems, seem to be advantageous. In addition, new results concerning the<br />
convergence <strong>of</strong> the preconditioned Krylov subspace iteration (which is not guaranteed because<br />
the system to be solved is singular) are presented.<br />
Adaptive smoothed aggregation multigrid<br />
Marcel Schweitzer (<strong>Universität</strong> Wuppertal) Schedule<br />
We investigate algebraic multigrid (AMG) methods, in particular those based on the smoothed<br />
aggregation approach, for solving linear systems Ax = b with a general, nonsymmetric matrix A.<br />
Recent results show that in this case it is reasonable to demand that the interpolation operator<br />
is able to accurately approximate singular vectors corresponding to the smallest singular values<br />
<strong>of</strong> A. Therefore, we present an extension <strong>of</strong> the bootstrap AMG setup, which is geared towards<br />
the singular vectors <strong>of</strong> A instead <strong>of</strong> the eigenvectors as in the original approach. Numerical experiments<br />
with systems from the discretization <strong>of</strong> convection diffusion equations show that this<br />
new setup approach performs very well when compared to established methods. In addition, we<br />
present results that show that our method can also be used as a very efficient preconditioner for<br />
the generalized minimal residual (GMRES) method.
Section 18: Numerical methods <strong>of</strong> differential equations 313<br />
Section 18: Numerical methods <strong>of</strong> differential equations<br />
Organizers: Etienne Emmrich (<strong>Universität</strong> Bielefeld), Andreas Prohl (<strong>Universität</strong> Tübingen)<br />
S18.1: Computational Fluid Dynamics Tue, 13:30–15:30<br />
Chair: Bürger S1|03–221<br />
Fully conservative time integrators for skew-symmetric compressible flow schemes<br />
Jens Brouwer, Julius Reiss, Jörn Sesterhenn (TU Berlin) Schedule<br />
Fully conservative finite difference schemes for the compressible Navier-Stokes equations can be<br />
constructed by discretizing the skew-symmetric form <strong>of</strong> the analytic equations and keeping the<br />
skew-symmetry in their respective discrete forms. For example, the momentum equation takes<br />
the form<br />
� �<br />
1 ∂ρ · u<br />
+ ρ∂u +<br />
2 ∂t ∂t<br />
1<br />
� �<br />
∂ρu · u<br />
+ ρu∂u +<br />
2 ∂x ∂x<br />
∂p<br />
∂x<br />
= 0, (1)<br />
where both the convective and temporal differentiation operators are skew symmetric. While conservative<br />
semi-discrete schemes are easily constructed the unusual form <strong>of</strong> the temporal derivative<br />
poses additional challenges which dictate the use <strong>of</strong> multistep methods. A promising ansatz is to<br />
rewrite the time derivative as<br />
� �<br />
1 ∂ρ · u<br />
+ ρ∂u<br />
2 ∂t ∂t<br />
= √ ρ ∂√ρu , (2)<br />
∂t<br />
which is based on the work <strong>of</strong> Morinishi, [1],and leads to fully conservative one-step schemes<br />
with better stability properties and easier implementation. Implicit and explicit integrators for<br />
both formulations are presented and discussed with respect to there applicability for practical<br />
computations and extension to higher order schemes.<br />
[1] Y. Morinishi, Skew-symmetric form <strong>of</strong> convective terms and fully conservative finite difference<br />
schemes for variable density low-Mach number flows,<br />
Journal <strong>of</strong> Computational Physics 229 (2010), 276 – 300.<br />
Kinetic Models and the Finite Pointset Method (FPM)<br />
Maria Kobert, Jörg Kuhnert (ITWM Kaiserslautern), Axel Klar (TU Kaiserslautern) Schedule<br />
The overall goal is to simulate rarefied flows inside vacuum pumps. The behavior <strong>of</strong> a flow in a<br />
vacuum pump is defined through the Knudsen number Kn, which can be very small (Kn < 0.01<br />
continuum flow) or larger (Kn > 0.5 molecular flow).<br />
Continuum flows are mainly simulated by using commercial CFD methods, which solve the<br />
Navier-Stokes equations. In the case <strong>of</strong> molecular flows one uses statistical methods, such as the<br />
Direct Simulation Monte Carlo (DSMC).<br />
We want to develop a deterministic method for flows near continuum (Kn ≈ 0.01, ...0.1), since<br />
the DSMC method fails in those regions due to rapid increase <strong>of</strong> particles. The deterministic<br />
method we intend to use is the Finite-Pointset-Method (FPM) [1], which is a meshfree numerical<br />
method developed at the ITWM Kaiserslautern and is mainly used to solve fluid dynamical problems.<br />
The method is superior to the classical methods in the case <strong>of</strong> problems with complicated<br />
geometries and/or moving boundaries, which is appropriate in models <strong>of</strong> vacuum pump systems.<br />
As Boltzmann collision model we use the BGK-model [2].
314 Section 18: Numerical methods <strong>of</strong> differential equations<br />
Two attempts <strong>of</strong> implementing the BGK-equation in FPM are presented. The first one is to<br />
discretize the BGK-model using the IMEX-Runge Kutta scheme [3] and the second one is dealing<br />
with the moments <strong>of</strong> the BGK-equation and the so called 13 Moment equations [4]. Numerical<br />
examples for both methods are shown for different ranges <strong>of</strong> the Knudsen number.<br />
[1] Tiwari, S., Kuhnert, J., Finite pointset method based on the projection method for simulations<br />
<strong>of</strong> the incompressible Navier-Stokes equations Meshfree methods for partial differential<br />
equations Band 1 (2004)<br />
[2] P.L. Bhatnagar, E. P. G., Krook, M., A model for collision processes in gases. Small amplitude<br />
processes in charged and neutral one-component systems Physical Reviews 1954 (94), 511-<br />
525.<br />
[3] Pieraccini, S., Puppo, G., Implicit - Explicit schemes for BGK kinetic equations<br />
[4] Struchtrup, H., Derivation <strong>of</strong> 13 Moment equations for rarefied gas flow to second order<br />
accuracy for arbitrary interaction potentials Multiscale Model Simul. 3 (2005) 221-243<br />
Subspace Projection Method for Particulate Flows<br />
Rodolphe Prignitz, Eberhard Bänsch (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
A method is presented for the simulation <strong>of</strong> viscous incompressible flow with many suspended<br />
solid particles. This method uses a finite-element discretisation in space and an operator-splitting<br />
technique for discretisation in time and has its basis in work by Glowinski et al.. However, a<br />
subspace projection rather than a Lagrange multiplier is used to couple the particle motion with<br />
the fluid motion. Combined with local mesh refinement the method results in a fast and accurate<br />
algorithm for the simulation <strong>of</strong> a huge number <strong>of</strong> particles in a flow field. Validation is achieved<br />
using the sedimentation <strong>of</strong> one particle and comparing the resulting drag coefficient with theoretical<br />
and experimental results.<br />
Solving Kaup-Kupershmidt equation by using iterative methods<br />
Shadan Sadigh Behzadi, Armin Sadigh Behzadi (Islamic Azad University Tehran) Schedule<br />
In this paper, a nonlinear Kaup-Kupershmidt equation is solved by using the Adomian decomposition<br />
method (ADM),modified Adomian decomposition method (MADM), variational iteration<br />
method (VIM), modified variational iteration method (MVIM), homotopy perturnbation method<br />
(HPM), modified homotopy perturbation method (MHPM) and homotopy analysis method<br />
(HAM) numerically. For each method, the approximate solution <strong>of</strong> this equation is calculated<br />
based on a recursive relation which its components are computed easily. The existence and uniqueness<br />
<strong>of</strong> the solution and the convergence <strong>of</strong> the proposed methods are proved. Numerical<br />
examples are studied to demonstrate the accuracy <strong>of</strong> the given algorithms.<br />
A Stabilized Finite Element Method for Convection-Diffusion Problems using Boundary<br />
Integral Operators<br />
Clemens H<strong>of</strong>reither, Ulrich Langer (<strong>Universität</strong> Linz) Schedule<br />
We present a non-standard stabilized finite element method where stabilization is done using<br />
element-local boundary integral operators. This approach requires the explicit knowledge <strong>of</strong> a<br />
local fundamental solution, but permits the use <strong>of</strong> general polygonal or polyhedral meshes. Some<br />
numerical examples confirm the stabilizing effect.
Section 18: Numerical methods <strong>of</strong> differential equations 315<br />
A-priori error analysis for finite element approximations <strong>of</strong> Stokes problem on dynamic<br />
meshes<br />
Andreas Brenner, Eberhard Bänsch (<strong>Universität</strong> Erlangen-Nürnberg), Markus Bause (<strong>Universität</strong><br />
der Bundeswehr Hamburg) Schedule<br />
We study finite element approximations <strong>of</strong> the time dependent Stokes system on dynamically<br />
changing meshes. Applying the backward Euler method for time discretization we use the discrete<br />
Helmholtz or Stokes projection to evaluate the solution at time tn−1 on the new spatial<br />
mesh at time tn. The theoretical results consist <strong>of</strong> a priori error estimates that show a dependence<br />
on the time step size not better than O(1/∆t). These surprisingly pessimistic upper bounds are<br />
complemented by numerical examples giving evidence that our error estimates are sharp. These<br />
observations imply that using adaptive meshes for flow problems is delicate and requires further<br />
investigations.<br />
S18.2: Applications Tue, 16:00–18:00<br />
Chair: Banas S1|03–221<br />
A stabilized finite volume element method for sedimentation-consolidation processes<br />
Raimund Bürger (Universidad de Concepción, Chile), Ricardo Ruiz-Baier (EPFL Lausanne),<br />
Héctor Torres (Universidad de La Serena, Chile) Schedule<br />
A model <strong>of</strong> sedimentation-consolidation processes in so-called clarifier-thickener units is given by<br />
a parabolic equation describing the evolution <strong>of</strong> the local solids concentration coupled with a<br />
version <strong>of</strong> the Stokes system for an incompressible fluid describing the motion <strong>of</strong> the mixture.<br />
In cylindrical coordinates, and if an axially symmetric solution is assumed, the original problem<br />
reduces to two space dimensions. This poses the difficulty that the subspaces for the construction<br />
<strong>of</strong> a numerical scheme involve weighted Sobolev spaces. A novel finite volume element method<br />
is introduced for the spatial discretization, where the velocity field and the solids concentration<br />
are discretized on two different dual meshes. The method is based on a stabilized discontinuous<br />
Galerkin formulation for the concentration field, and a multiscale stabilized pair <strong>of</strong> P1-P1 elements<br />
for velocity and pressure, respectively. Numerical experiments illustrate properties <strong>of</strong> the model<br />
and the satisfactory performance <strong>of</strong> the proposed method.<br />
On the Coupled Electromechanical Activation <strong>of</strong> the Human Heart<br />
E. Karabelas, O. Steinbach (TU Graz) Schedule<br />
The mathematical modeling <strong>of</strong> electro-mechanical coupled activation <strong>of</strong> the human heart results in<br />
a system <strong>of</strong> highly non-linear time-dependent coupled partial and ordinary differential equations.<br />
In this talk we consider the bidomain equations for modelling the electric activation <strong>of</strong> the human<br />
heart and the quasi-stationary equations <strong>of</strong> non-linear elasticity for describing the deformation <strong>of</strong><br />
the heart. We will present some results on the solvability <strong>of</strong> the coupled system, and we discuss<br />
finite element approximations for the numerical solution.<br />
A Finite Element Approximation <strong>of</strong> Air Flow in the Area under a Platform <strong>of</strong> Bangkok<br />
Sky Train<br />
Nopparat Pochai (King Mongkut’s Institute <strong>of</strong> Technology Ladkrabang, Thailand) Schedule<br />
The air pollution problems arise frequently in Bangkok, Thailand. The consideration area is the<br />
area under Phayathai platform station <strong>of</strong> Bangkok sky train in Bangkok, Thailand. The area has<br />
a problem <strong>of</strong> air pollution control. The Bangkok Mass Transit System Company tries to set up<br />
the misting fans inside the area. The flow <strong>of</strong> the air is still not smooth and the air quality is still<br />
lower than standard. The assumption <strong>of</strong> the research is the flow obstructs by platform structures.
316 Section 18: Numerical methods <strong>of</strong> differential equations<br />
In this research, we will present the finite element method applied to problems <strong>of</strong> two-dimensional<br />
laminar flow <strong>of</strong> incompressible viscous fluid. The governing equations <strong>of</strong> the air flow are expressed<br />
in terms <strong>of</strong> the streamfunction and vorticity.<br />
Basic Modelling for Large Deformation <strong>of</strong> Plates<br />
Jens Rückert, Arnd Meyer (TU Chemnitz) Schedule<br />
In the simulation <strong>of</strong> deformations <strong>of</strong> plates it is well known that we have to use a special treatment<br />
<strong>of</strong> the thickness dependence. Therewith we achieve a reducing <strong>of</strong> dimension from 3D to 2D.<br />
For linear elasticity and small deformations several techniques are well established to handle the<br />
reduction <strong>of</strong> dimension and achieve acceptable numerical results. In the case <strong>of</strong> large deformations<br />
<strong>of</strong> plates with non-linear material behaviour there exist different problems. So, the analytical integration<br />
over the thickness <strong>of</strong> the plate is not possible due to the non-linearities arising from the<br />
material law and the large deformations themselves. There are several possibilities to introduce a<br />
hypothesis for the treatment <strong>of</strong> the plate thickness from the strong Kirchh<strong>of</strong>f assumption on one<br />
hand up to some hierarchical approaches on the other hand. Here we consider a model <strong>of</strong> using<br />
the Kirchh<strong>of</strong>f assumption. Mathematically it means:<br />
x(η 1 , η 2 , η 3 ) : = x m (η 1 , η 2 ) + η 3 f(η 1 , η 2 ) (1)<br />
⎛<br />
= ⎝<br />
η 1<br />
η 2<br />
η 3<br />
⎞<br />
⎠ + U + η 3 (f(U) − e3) (2)<br />
= X(η) + U + η 3 (f(U) − e3), (3)<br />
where X/x are the physical points <strong>of</strong> the undeformed/deformed plate,<br />
η = (η 1 , η 2 , η 3 ) their coordinates, U the deformation vector, depending on (η 1 , η 2 ) only, and f the<br />
normal vector <strong>of</strong> the deformed midsurface, arising from the assumption. In case <strong>of</strong> small strain<br />
this normal direction f is approximated by a linear differential operator. We consider finite strains,<br />
hence f has to have the true nonlinear dependence on U following the differential geometry <strong>of</strong><br />
the deformed midsurface. It is important that we avoid any further simplifications, which could<br />
be crucial for large strains. This way <strong>of</strong> modelling leads to a two-dimensional strain tensor, which<br />
depends essentially on the first two fundamental forms <strong>of</strong> the differential geometry <strong>of</strong> the deformed<br />
midsurface. Outgoing from this new strain tensor we obtain the energy functional. The FEM<br />
ansatz is to find the state <strong>of</strong> the plate, where the deformation energy has its minimum over a<br />
suitable chosen finite element subspace. Therefore the first derivative <strong>of</strong> the energy functional has<br />
to be zero. Whether the energy functional is easily calculated with the new strain tensor, there are<br />
some difficulties in calculating the derivatives <strong>of</strong> the functional. Especially the second derivative<br />
is ambitious to calculate and makes the Newton linearization for computing the solution very<br />
expansive. Nethertheless, due to the fast convergence <strong>of</strong> the Newton linearization, we think that<br />
the effort is worth the trouble. We will present the total theory and give numerical results for<br />
comparisions.<br />
Numerical Simulation <strong>of</strong> Plasmonic Effect at Metallic/Dielectric Interface<br />
Shuai Yan, Christoph Pflaum (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
Plasmonics concern with electromagnetic excitations at the interface between a dielectric and<br />
a conductor, and plasmonic nanostructure is now a promising candidate as a light scattering<br />
and trapping agent for solar cells. We solved Maxwell equation analytically and numerically in a<br />
region with flat interface between a conductor and a dielectric, which is the most simple geometry<br />
sustaining plasmonic effects. The simulation technique is a finite integration technique(FIT)<br />
combined with a time harmonic inverse iteration method(THIIM). Results show the numerical
Section 18: Numerical methods <strong>of</strong> differential equations 317<br />
solution converges to the analytical solution with order around 1.4, which implies our scheme is<br />
well-suited for further simulation involving plasmonics. We then study the convergence behavior<br />
<strong>of</strong> the discretization scheme theoretically, both achievements and difficulties for this analysis will<br />
be presented.<br />
S18.3: Computational Fluid Dynamics Wed, 13:30–15:30<br />
Chair: Siska S1|03–221<br />
A comparison <strong>of</strong> Rosenbrock and ESDIRK schemes for unsteady compressible flow<br />
problems<br />
Hester Bijl (University <strong>of</strong> Delft), Philipp Birken, Andreas Meister (<strong>Universität</strong> Kassel), Alexander<br />
van Zuijlen (University <strong>of</strong> Delft) Schedule<br />
We consider implicit time integration methods for unsteady flow problems. There, it has been<br />
previously demonstrated that ESDIRK schemes are faster than BDF schemes for engineering<br />
accuracies. Here, we compare Rosenbrock schemes to ESDIRK schemes for a model nonlinear<br />
convection-diffusion problem and the 3D unsteady Navier-Stokes equations.<br />
When using Newton’s method in the ESDIRK schemes, we obtain a sequence <strong>of</strong> linear systems.<br />
This is also true <strong>of</strong> Rosenbrock time integration, but there, the system matrix is constant<br />
during a time step. We compare different strategies <strong>of</strong> exploiting this.<br />
The FEM and SDFEM for convection-diffusion problems with low regularity<br />
Lars Ludwig, Hans-Görg Roos (TU Dresden) Schedule<br />
The finite element method is applied to a convection-diffusion problem posed on the unite square<br />
using a tensor product mesh and bilinear elements. The usual pro<strong>of</strong>s that establish superconvergence<br />
for this setting involve a rather high regularity <strong>of</strong> the exact solution - typically u ∈ H 3 (Ω),<br />
which in many cases cannot be taken for granted. In this paper we derive superconvergence results<br />
where the right hand side <strong>of</strong> our a priori estimate no longer depends on the H 3 norm but merely<br />
requires finiteness <strong>of</strong> some weaker functional measuring the regularity. Moreover, we consider the<br />
streamline diffusion stabilization method and how superconvergence is affected by the regularity<br />
<strong>of</strong> the solution. Finally, numerical experiments for both discretizations support and illustrate the<br />
theoretical results.<br />
The influence <strong>of</strong> nonlinear joint characteristics on friction-induced vibrations<br />
Sebastian Kruse (TU Hamburg, Audi AG), Pascal Reuß (<strong>Universität</strong> Stuttgart), Norbert H<strong>of</strong>fmann<br />
(TU Hamburg) Schedule<br />
Friction-induced vibrations and its applications are an everlasting problem in industry and academia<br />
that has been dealt with in many works(e.g. Kinkaid et al.,Ouyang et al.). There are two<br />
aspects in this research field that are mainly discussed. The first aspect is the stability <strong>of</strong> systems<br />
that tend to friction-induced vibrations. Research deals especially with questions <strong>of</strong> modelling,<br />
sensitivity with respect to physical parameters and methods to solve the linearized equations <strong>of</strong><br />
motion (e.g. Sinou et al.,Wagner et al.). The second aspect is the approximation <strong>of</strong> limit cycles<br />
due to the nonlinear terms in the equation <strong>of</strong> motions (e.g. H<strong>of</strong>fmann et al.,Coudeyras et al.).<br />
Well known techniques for limit cycle approximation have been discussed or extended in order to<br />
be able to predict limit cycles and hence the criticality <strong>of</strong> friction-induced vibrations. However,<br />
while the discussion on stability is limited to questions <strong>of</strong> linearized systems and hence fails to<br />
determine the relevance <strong>of</strong> a predicted instability, the methods dealing with limit cycle approximation<br />
are still limited to somewhat small models that fail to predict the reality <strong>of</strong> systems on<br />
an engineering scale.
318 Section 18: Numerical methods <strong>of</strong> differential equations<br />
This research tries to overcome the gap between these two fields. Therefore linear techniques<br />
and the knowledge <strong>of</strong> dominant nonlinearities in a system are employed in order to predict the<br />
criticality <strong>of</strong> a particular system instability.<br />
The research starts with a few degree <strong>of</strong> freedom model that inherits a mechanism for frictioninduced<br />
vibrations. This model includes a joint with nonlinear characteristics. We employ an<br />
extended harmonic balance technique introduced by Coudeyras et al. in order to approximate<br />
limit cycles for unstable regions in the parameter space <strong>of</strong> the small model. The limit cycle<br />
shape and amplitude are analysed and compared to the results <strong>of</strong> the linear stability analysis<br />
with the corresponding eigenvalues and eigenvectors. This analysis shows that the amplitude<br />
or criticality <strong>of</strong> friction-induced vibrations can be predicted based on the linear stability analysis<br />
under the assumptions that the dominant non-linearities <strong>of</strong> the system are known. These dominant<br />
nonlinearities are usually the few joints inheriting dry friction.<br />
Based on these results we discuss the limits <strong>of</strong> todays methods <strong>of</strong> stability analysis in frictioninduced<br />
systems and suggest a way to extend these methods to predict critical regions in the<br />
parameter space that may lead to large limit cycle amplitudes without loosing the possibility to<br />
analyse systems on an engineering scale.<br />
[1] N.M. Kinkaid, O.M. O’Reilly, P. Papadopoulos Automotive disc brake squeal, Journal <strong>of</strong><br />
Sound and Vibration, Volume 267, Issue 1, 9. October 2003, pages 105-166<br />
[2] H. Ouyang, W. Nack, Y. Yuan, F. Chen, Numerical analysis <strong>of</strong> automotive disc brake squeal:<br />
a review, International Journal <strong>of</strong> Vehicle Noise and Vibration, Volume 1, Number 3-4 /<br />
2005 , pages 207 - 231<br />
[3] J.-J. Sinou, L. Jezequel, Mode coupling instability in friction-induced vibrations and its dependency<br />
on system parameters including damping, European Journal <strong>of</strong> Mechanics - A/Solids,<br />
Volume 26, Issue 1, January-February 2007, Pages 106-122<br />
[4] U. v. Wagner, D. Hochlenert, P. Hagedorn, Minimal models for disk brake squeal, Journal <strong>of</strong><br />
Sound and Vibration, Volume 302, Issue 3, 8 May 2007, Pages 527-539<br />
[5] N. H<strong>of</strong>fmann, S. Bieser, L. Gaul, Harmonic Balance and Averaging Techniques for Stick-Slip<br />
Limit-Cycle Determination in Mode-Coupling Friction Self-Excited Systems, TECHNISCHE<br />
MECHANIK, Band 24, Heft 3-4, (2004), 185 197<br />
[6] N. Coudeyras, S. Nacivet, J.-J. Sinou, Periodic and quasi-periodic solutions for multi-instabilities<br />
involved in brake squeal, Journal <strong>of</strong> Sound and Vibration, Volume 328, Issues 4-5, 25<br />
December 2009, Pages 520-540<br />
Application <strong>of</strong> the Method <strong>of</strong> Fundamental Solution for two dimensional steady viscous<br />
fluid flow<br />
Magdalena Mierzwiczak (Poznan University <strong>of</strong> Technology) Schedule<br />
A meshless numerical procedure based on the method <strong>of</strong> fundamental solutions (MFS) and the<br />
Radial Basic Functions (RBF) is proposed to solve the Navier-Stokes equations. For the best<br />
knowledge <strong>of</strong> author, as yet, only in one paper this method was applied to solve <strong>of</strong> Navier–Stokes<br />
equations [1]. The MFS is a meshless method since it is free from the mesh generation and numerical<br />
integration. We will transform the NavierStokes equations into simple inhomogeneous<br />
biharmonic equation for the stream function. The non-linear biharmonic boundary value problem
Section 18: Numerical methods <strong>of</strong> differential equations 319<br />
we solve iteratively. At every step <strong>of</strong> the calculation we use the radial basis functions to interpolation<br />
<strong>of</strong> the right hand side in non-homogeneous governing equation. The proposed meshless<br />
numerical scheme is a first attempt to apply the MFS with RBF for solving the steady NavierStokes<br />
equations in the moderate-Reynolds-number flow regimes. As computational example the flow<br />
in stenosed arteries is considered [2]. From the computational point <strong>of</strong> view, the present numerical<br />
procedure based on the method <strong>of</strong> fundamental solutions is efficient and simple to implement as<br />
compared to the mesh-dependent schemes, which needs complex mesh generation procedure for<br />
the geometrical domains.<br />
[1] Young D.L., Lin Y.C., Fan C.M., Chiu C.L., The method <strong>of</strong> fundamental solutions for solving<br />
incompressible NavierStokes problems, Engineering Analysis with Boundary Elements 33<br />
(2009), 1031–1044.<br />
[2] Zendehbudi G.R., Moayeri M.S., Comparison <strong>of</strong> physiological and simple pulsatile flows<br />
through stenosed arteries, Journal <strong>of</strong> Biomechanics 32 (1999), 959–965.<br />
Convergence <strong>of</strong> Iterative methods applied to Boussinesq equation<br />
Shadan Sadigh Behzadi (Islamic Azad University Qazvin) Schedule<br />
In this paper, a Boussinesq equation is solved by using the Adomain’s decomposition method<br />
(ADM), variational iteration method (VIM),modified Adomian decomposition method (MADM),<br />
modified variational iteration method (MVIM), homotopy analysis method (HAM), homotopy<br />
perturbation method (HPM)and modified homotopy perturbation method (MHPM).The approximate<br />
solution <strong>of</strong> this equation is calculated in the form <strong>of</strong> series which it’s components are<br />
computed by applying a recursive relation The existence and uniqueness <strong>of</strong> the solution and the<br />
convergence <strong>of</strong> the proposed methods are proved.A numerical example is studied to demonstrate<br />
the accuracy <strong>of</strong> the presented methods.<br />
S18.4: Finite Elements Wed, 13:30–15:30<br />
Chair: Steinbach S1|03–223<br />
Generalized Park-Sheen Finite Elements for Adaptivity<br />
Robert Altmann (TU Berlin), Carsten Carstensen (HU Berlin) Schedule<br />
Park and Sheen ([2003]) introduced a basis for nonconforming, piecewise linear finite elements<br />
on triangulations into quadrilaterals <strong>of</strong> simply connected domains. Moreover, adaptive meshrefinement<br />
has recently been proven to be optimal for the related Crouzeix-Raviart nonconforming<br />
FEM on triangles. In order to use adaptive mesh-refinements with the Park-Sheen nonconforming<br />
FEM on quadrilaterals, we introduce the combination <strong>of</strong> Park-Sheen with Crouzeix-Raviart nonconforming<br />
finite elements. This requires the understanding <strong>of</strong> the Park-Sheen FEM on multiple<br />
connected domains.<br />
The proposed combination <strong>of</strong> the Park-Sheen and the Crouzeix-Raviart nonconforming elements<br />
combines the minimal degrees <strong>of</strong> freedom per element domain with the flexibility <strong>of</strong> adaptive<br />
mesh-refinement.<br />
As main result we characterise a basis <strong>of</strong> this nonconforming finite element space with global<br />
edge-connected exceptional basis functions and present a complete a priori error analysis with<br />
explicit constants.<br />
[2003] Park, C. and Sheen, D., P1-nonconforming quadrilateral finite element methods for secondorder<br />
elliptic problems, SIAM J. Numer. Anal. (2003).
320 Section 18: Numerical methods <strong>of</strong> differential equations<br />
FETI-DP for a class <strong>of</strong> linear elasticity problems with varying material coefficients<br />
inside subdomains<br />
Sabrina Gippert, Axel Klawonn, Oliver Rheinbach (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
In this talk, a domain decomposition method for a class <strong>of</strong> linear elasticity problems with varying<br />
material coefficients is considered. In this category <strong>of</strong> problems each subdomain contains<br />
an almost incompressible inclusion surrounded by a compressible hull. The classical FETI-DP<br />
algorithm with primal vertices and primal edge averages is applied, i.e., the coarse space for compressible<br />
linear elasticity is used. The condition number is found to depend only on the material<br />
parameters <strong>of</strong> the hull and also on its thickness, but is otherwise independent <strong>of</strong> coefficient jumps<br />
between subdomains and also between the hull and the inclusion. Thus, the condition number<br />
does not deteriorate when the Poisson ratio <strong>of</strong> the inclusion tends to 0.5. Numerical results confirming<br />
our theoretical findings are presented.<br />
Comparison <strong>of</strong> different methods <strong>of</strong> choice <strong>of</strong> collocation points in boundary collocation<br />
method for 2D harmonic problems with special purpose Trefftz function<br />
Jan Adam Kolodziej, Magdalena Mierzwiczak (Poznan University <strong>of</strong> Technology) Schedule<br />
Based on the special purposed Trefftz functions we present a comparison <strong>of</strong> the different methods<br />
<strong>of</strong> choosing collocation points when boundary collocation method is used to fulfil the boundary<br />
conditions. First, it is shown that for some geometries <strong>of</strong> a region when applying the boundary<br />
collocation method with special purposed Trefftz function, the equidistant collocation points my<br />
give unacceptable results. Next, for four 2-D harmonic boundary values problems: Torsion <strong>of</strong> a<br />
triangular bar with a circular centered hole, Longitudinal laminar flow in a regular array <strong>of</strong> cylindrical<br />
rods, Field temperature in a repeated element <strong>of</strong> regular composite, Potential flow past<br />
a cylinder between parallel walls; four cases <strong>of</strong> different placement <strong>of</strong> the collocation points are<br />
described and compared. Based on the results <strong>of</strong> the comparison <strong>of</strong> the test methods for the location<br />
<strong>of</strong> collocation points it is shown that the our proposed method <strong>of</strong> location <strong>of</strong> the collocation<br />
points which has an iterative and adaptive character is simple to implement and accurate. The<br />
essence <strong>of</strong> this method is an adaptive determination <strong>of</strong> the consequent collocation points.<br />
Coupling Methods for Interior Penalty Discontinuous Galerkin Finite Element Methods<br />
and Boundary Element Methods<br />
Günther Of (TU Graz), G.J. Rodin (The University <strong>of</strong> Texas at Austin), O. Steinbach (TU Graz),<br />
M. Taus (The University <strong>of</strong> Texas at Austin) Schedule<br />
This paper presents three new coupling methods for interior penalty discontinuous Galerkin finite<br />
element methods and boundary element methods. The new methods allow one to use discontinuous<br />
basis functions on the interface between the subdomains represented by the finite element<br />
and boundary element methods. This feature is particularly important when discontinuous Galerkin<br />
finite element methods are used. Error and stability analysis is presented for some <strong>of</strong> the<br />
methods. Numerical examples suggest that all three methods exhibit very similar convergence<br />
properties, consistent with available theoretical results.<br />
Combined boundary element and discrete singularity method<br />
Reshniak Viktor, Kochubey Olexander, Yevdokymov Dmytro (Oles Gonchar Dnipropetrovsk National<br />
University) Schedule<br />
Permanent development and progress in science and technique leads to necessity <strong>of</strong> solving new<br />
problems and taking into account effects, that have never been considered before. Finite element
Section 18: Numerical methods <strong>of</strong> differential equations 321<br />
and finite difference methods are highly developed computational methods <strong>of</strong> solving PDEs problems.<br />
But their usage has some limitation factors. For instance, they are good applicable in case<br />
<strong>of</strong> continuously changing properties <strong>of</strong> solution area. If not, they can become incorrect because<br />
<strong>of</strong> loosing information inside the elements. Another problem is the huge number <strong>of</strong> nodes that<br />
are generated during the meshing procedure. The usage <strong>of</strong> specialized computational methods,<br />
that have been rapidly developed in the last years, can help to solve some <strong>of</strong> these problems.<br />
Among them are lagrangian methods and methods <strong>of</strong> computational potentional theory, based<br />
on integral representations <strong>of</strong> basic PDEs. BEM and discrete singularity method are used in this<br />
work according to this approach. These methods have certain advantages, such as precision <strong>of</strong><br />
BEM and simplicity <strong>of</strong> discrete singularity method. The compilation <strong>of</strong> these features can be very<br />
effective. Besides that, using the BEM for solving elliptical PDEs <strong>of</strong> potentional theory can reduce<br />
the dimension <strong>of</strong> the problem. The considered approach was used to solve the plain boundary<br />
problem <strong>of</strong> vortical motion <strong>of</strong> uncompressible fluid. The boundary was approximated by boundary<br />
elements, while the vortisity was approximated by discrete vortices. Results were visualized with<br />
streamlines and trajectories. The analysis <strong>of</strong> estimated results shows good applicability <strong>of</strong> this<br />
approach.<br />
S18.5: Applications Wed, 16:00–18:00<br />
Chair: Emmrich S1|03–221<br />
Efficient numerical methods for initial-value solid-state laser problems<br />
Fan Feng, Christoph Pflaum (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
The difficulties <strong>of</strong> solving initial-value solid-state laser problems numerically arise from both stiffness<br />
<strong>of</strong> the problems and near-to-zero nonnegative exact solutions.Stability and non-negativity<br />
must be maintained simultaneously in the numerical solutions.Classical schemes unfortunately<br />
suffer from severe time-step restriction because <strong>of</strong> the difficulties.<br />
In this paper,we present an optimized numerical approach with which 3-dimensional laser<br />
problems can be solved faster and much more efficiently.These techniques can not only be used<br />
for solid-state laser system,passively Q-switched laser system, passively Q-switched intracavity<br />
frequency-doubling laser system,but can also be applied to solve other stiff problems which have<br />
near-to-zero nonnegative exact solutions.<br />
To the best <strong>of</strong> our knowledge,efficient numerical approach solving initial-value passively Qswitched<br />
intracavity frequency-doubling solid-state laser problem is introduced for the first time.<br />
An Extrapolation Approach for Iterative Maxwell Solvers Based upon the Prony<br />
Method<br />
Kai Hertel (<strong>Universität</strong> Erlangen-Nürnberg), Christoph Pflaum, Raj Mittra Schedule<br />
We present an adaptation <strong>of</strong> Prony’s extrapolation method for approximating solutions <strong>of</strong> Maxwell’s<br />
equations for large-scale solar cell simulations. The method samples a small number <strong>of</strong><br />
equidistant iterates <strong>of</strong> a finite difference frequency domain (FDFD) solver and extracts the dominating<br />
amplitude-frequency pairs in order to approximate the dominating eigenvectors <strong>of</strong> the<br />
FDFD iteration matrix. The objective is to dampen down the initial transient sufficiently for<br />
the resulting data to allow for a long-term prediction <strong>of</strong> the underlying sinusoidal signals. The<br />
quality <strong>of</strong> the numerical approximation highly depends on both the sample window as well as the<br />
assumed model order.
322 Section 18: Numerical methods <strong>of</strong> differential equations<br />
Reduced Basis Modeling for Parametrized Systems <strong>of</strong> Maxwell’s Equations<br />
Martin Hess, Peter Benner (MPI Magdeburg) Schedule<br />
The Reduced Basis Method [1] generates low-order models to parametrized PDEs to allow for<br />
efficient evaluation <strong>of</strong> parametrized models in many-query and real-time contexts. The Reduced<br />
Basis approach is decomposed into a time-consuming <strong>of</strong>fline phase, which generates a surrogate<br />
model and an online phase, which allows fast parameter evaluations. Rigorous and sharp a posteriori<br />
error estimators play a crucial role in this process, in that they define which snapshots are<br />
to be taken into the reduced space and give bounds to the output quantities during the online<br />
phase.<br />
We apply the Reduced Basis Method to systems <strong>of</strong> Maxwell’s equations arising from electrical<br />
circuits [2]. Using microstrip models as a microscopic view <strong>of</strong> interconnect structures, the<br />
input-output behaviour is approximated with low order reduced basis models for a parametrized<br />
geometry, like distance between microstrips and/or material coefficients, like permittivity and<br />
permeability <strong>of</strong> substrates.<br />
We show the theoretical framework in which the Reduced Basis Method is applied to Maxwell’s<br />
equations and present first numerical results.<br />
[1] G. Rozza, D.B.P. Huynh, A.T. Patera, Reduced Basis Approximation and a Posteriori Error<br />
Estimation for Affinely Parametrized Elliptic Coercive Partial Differential Equations, Arch.<br />
Comput. Methods Eng. 15 (2008), 229 – 275.<br />
[2] R. Hiptmair, Finite Elements in computational electromagnetism, Acta Numerica (2002) 237<br />
– 339.<br />
Consistency Results for a Contact-Stabilized Newmark Method in Time and Space<br />
Corinna Klapproth (Zuse-Institute Berlin) Schedule<br />
The talk is concerned with a contact-stabilized Newmark method for the numerical integration <strong>of</strong><br />
dynamical contact problems formulated on the basis <strong>of</strong> Signorini’s contact conditions. The focus<br />
is on a new variant <strong>of</strong> the original contact-stabilized Newmark method, which is energy dissipative<br />
and avoids artificial oscillations. The new scheme additionally produces velocities equal to zero at<br />
active contact boundaries. The main topic <strong>of</strong> the talk is the investigation <strong>of</strong> the spatio-temporal<br />
discretization error <strong>of</strong> this method in the presence <strong>of</strong> contact. For this aim, the consistency error<br />
is measured in a physical energy norm and the solution is assumed to be <strong>of</strong> bounded total<br />
variation. It turns out that the new contact-stabilization leads to a much better behavior <strong>of</strong> the<br />
discretization error than previous versions <strong>of</strong> the Newmark method.<br />
Phase lag analysis <strong>of</strong> variational integrators using interpolation techniques<br />
O.T. Kosmas, Sigrid Leyendecker (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
In the present work we investigate the construction <strong>of</strong> high order variational integrator methods<br />
[1] combined with phase lag properties [2] for the numerical integration <strong>of</strong> systems with oscillatory<br />
solutions. We first consider physical problems where the corresponding components <strong>of</strong> the<br />
Lagrangian i.e. kinetic and potential energy, depend only on the generalized velocity and the generalized<br />
position respectively (for a generalized coordinate <strong>of</strong> the configuration space). We then<br />
express the action integral at any intermediate points along the curve segment, using a discrete<br />
Lagrangian that depends only from the end points <strong>of</strong> the interval [3]. High order integrators can<br />
be then obtained by defining the discrete Lagrangian in any time segment as a weighted sum on
Section 18: Numerical methods <strong>of</strong> differential equations 323<br />
intermediate points, whose expressions for positions and velocities use cubic spline interpolation<br />
or interpolation using trigonometric functions. The new methods depend now on a frequency,<br />
which needs to be evaluated [4].<br />
For that we adopt a new methodology which improves the phase lag characteristics by vanishing<br />
both the phase lag function and its first derivatives at a specific frequency [2]. Preliminary<br />
results show that sensitivity <strong>of</strong> the integration method is decrised on the estimated frequency<br />
<strong>of</strong> the problem. The efficiency <strong>of</strong> the new methods should be investigated via error analysis and<br />
numerical applications.<br />
[1] J. E. Marsden, M. West, Discrete mechanics and variational integrators. Acta Numerica 10<br />
(2001), 357 – 514.<br />
[2] Z. A Anastassi, D. S. Vlachos, T. E. Simos, The Use <strong>of</strong> Phase-Lag Derivatives in the Numerical<br />
Integration <strong>of</strong> ODEs with Oscillating Solutions. International Conference on Numerical<br />
Analysis and Applied Mathematics 1048 (2008) 1020 – 1025.<br />
[3] S. Leyendecker, J.E. Marsden, M. Ortiz, Variational integrators for constrained dynamical<br />
systems. Journal <strong>of</strong> Applied Mathematics and Mechanics (ZAMM) 88 (2008) 677 – 708.<br />
[4] O. T. Kosmas, D. S. Vlachos, Phase-fitted discrete Lagrangian integrators. Computer Physics<br />
Communications 181 (2010) 562 – 568.<br />
S18.6: Mesh Generation Wed, 16:00–18:00<br />
Chair: Thalhammer S1|03–223<br />
Adaptive anisotropic mesh refinement based on a new adaptivity paradigm<br />
Rene Schneider (TU Dresden) Schedule<br />
We propose a new paradigm for adaptive mesh refinement. Instead <strong>of</strong> considering local mesh<br />
diameters and their adaption to solution features, we propose to evaluate the benefit <strong>of</strong> possible<br />
refinements in a direct fashion, and to select the most pr<strong>of</strong>itable refinements. We demonstrate that<br />
based on this approach a directional refinement <strong>of</strong> triangular elements can be achieved, allowing<br />
arbitrarily high aspect ratios.<br />
However, only with the help <strong>of</strong> edge swapping and/or node removal (directional un-refinement)<br />
near optimal performance can be achieved for strongly anisotropic solution features. With these<br />
ingredients even re-alignment <strong>of</strong> the mesh with arbitrary error directions is achieved. Numerical<br />
experiments demonstrate the utility <strong>of</strong> the proposed anisotropic refinement strategy.<br />
Algebraic graph theory and its applications for mesh generation<br />
Christian Schröppel, Jens Wackerfuß (TU <strong>Darmstadt</strong>) Schedule<br />
Discretization methods are an important aspect <strong>of</strong> finding efficient numerical algorithms for the<br />
solution <strong>of</strong> partial differential equations. Before the advent <strong>of</strong> specialized computer programs,<br />
mesh generation was a tedious and <strong>of</strong>ten time-consuming process. Computer programs can greatly<br />
reduce the effort involved in generating meshes for a known geometry. However, it is generally not<br />
easy to incorporate specific knowledge about the structure, such as symmetries, into the process.<br />
This talk presents algebraic graph theory as an efficient tool for mesh generation. Algebraic<br />
graph theory is based on the mathematical properties <strong>of</strong> graphs itself, rather than on those <strong>of</strong><br />
representations <strong>of</strong> graphs, such as adjacency matrices. Meshes can be generated in a systematic
324 Section 18: Numerical methods <strong>of</strong> differential equations<br />
way, based on the algebraic operations that are available to modify and combine graphs. Specific<br />
features <strong>of</strong> a structure, such as symmetries, can be modeled into the generation <strong>of</strong> a mesh and its<br />
indexing system, allowing for a domain decomposition tailored to those features.<br />
This approach is especially useful for the generation <strong>of</strong> meshes <strong>of</strong> structures <strong>of</strong> a highly symmetric<br />
or fractal nature. Examples <strong>of</strong> such structures include the networks <strong>of</strong> covalent carbon-carbon<br />
bonds present in carbon nanotubes.<br />
Regularization and numerical integration <strong>of</strong> quasi-linear differential-algebraic equations<br />
<strong>of</strong> arbitrary index<br />
Andreas Steinbrecher (TU Berlin) Schedule<br />
Differential-algebraic equations (DAEs) are essential tools in the modeling <strong>of</strong> dynamical processes.<br />
For instance, the dynamical behavior <strong>of</strong> mechanical systems, electrical circuits, chemical reactions<br />
and many other are <strong>of</strong>ten described by DAEs, in particular, <strong>of</strong> quasi-linear structure.<br />
It is well known that the numerical treatment <strong>of</strong> DAEs is nontrivial in general and more complicated<br />
than the one <strong>of</strong> ordinary differential equations (ODEs). The classification <strong>of</strong> different<br />
types <strong>of</strong> DAEs led to the development <strong>of</strong> several (independent) index concepts. Today, the index<br />
concept plays a key role in the numerical analysis <strong>of</strong> DAEs since the index <strong>of</strong> a DAE provides a<br />
measure <strong>of</strong> the difficulty in the analytical as well as in the numerical solution. As a rule <strong>of</strong> thumb,<br />
the higher the index <strong>of</strong> a DAE is, the more complicated is its numerical analysis, and the more<br />
careful one has to be in the numerical solution <strong>of</strong> the problem. In particular, multibody systems<br />
are modeled by DAEs <strong>of</strong> differentiation index (d-index) 3 and circuit equations have a d-index<br />
up to 2. Arising effects in the numerical treatment <strong>of</strong> higher index DAEs are for example drift,<br />
instabilities, convergence problems, or inconsistencies. A way out <strong>of</strong> the dilemma <strong>of</strong> a higher index<br />
is a regularization <strong>of</strong> such classes <strong>of</strong> DAEs.<br />
In this talk we will present two regularization methods and an approach for the numerical integration<br />
<strong>of</strong> quasi-linear DAEs <strong>of</strong> the form<br />
E(x(t), t) ˙x(t) = k(x(t), t), (1)<br />
on the domain I = [t0, tf] with initial values x(t0) = x0 ∈ R n , where E ∈ C(R n × I, R n,n ) is<br />
called the leading matrix <strong>of</strong> the quasi-linear DAE and k ∈ C(R n × I, R n ) its right-hand side.<br />
Furthermore, x : I → R n represent the unknown variables.<br />
We will present two iterative procedures which provide general tools for the regularization and<br />
investigation <strong>of</strong> quasi-linear DAEs <strong>of</strong> an arbitrary index. One <strong>of</strong> this procedures is <strong>of</strong> rank inflation<br />
type while the other one is <strong>of</strong> rank deflation type. Both procedures can be used as basis<br />
for a regularization <strong>of</strong> the quasi-linear DAE and lead to equivalent regularized formulations <strong>of</strong><br />
the DAE, so called projected-strangeness-free formulations. The most important features <strong>of</strong> this<br />
projected-strangeness-free formulations are the lowered index while all constraints, in particular,<br />
the hidden constraints, are preserved. Therefore, projected-strangeness-free formulations can be<br />
used as basis for numerical integration using stiff ODE solvers in an robust and efficient way.<br />
Based on a projected-strangeness-free formulation the basic idea for a robust and efficient numerical<br />
integration will be presented and illustrated by several examples.<br />
Coupled FE-BE eigenvalue problems for fluid-structure interaction <strong>of</strong> submerged<br />
bodies<br />
G. Unger, A. Kimeswenger, O. Steinbach (TU Graz) Schedule<br />
In this talk we present a coupled finite and boundary element eigenvalue problem formulation<br />
for the simulation <strong>of</strong> the vibro-acoustic behavior <strong>of</strong> elastic bodies submerged in unbounded fluid<br />
domains as submarines in the sea. Usually the fluid is assumed to be incompressible and hence
Section 18: Numerical methods <strong>of</strong> differential equations 325<br />
modeled by the Laplace equation. In contrast, we do not neglect the compressibility <strong>of</strong> the fluid<br />
but model it by the Helmholtz equation. The resulting coupled eigenvalue problem for the fluidstructure<br />
interaction is then nonlinear since the frequency parameter appears nonlinearly in the<br />
boundary integral formulation <strong>of</strong> the Helmholtz equation. We analyze this eigenvalue problem and<br />
its discretization in the framework <strong>of</strong> eigenvalue problems for holomorphic Fredholm operator–<br />
valued functions. For the numerical solution <strong>of</strong> the discretized eigenvalue problem we use the<br />
contour integral method which reduces the algebraic nonlinear eigenvalue problem to a linear<br />
one. The method is based on a contour integral representation <strong>of</strong> the resolvent operator and it is<br />
suitable for the extraction <strong>of</strong> all eigenvalues which are enclosed by a given contour. The dimension<br />
<strong>of</strong> the resulting linear eigenvalue problem corresponds to the number <strong>of</strong> eigenvalues inside<br />
the contour. The main computational effort consists in the evaluation <strong>of</strong> the resolvent operator<br />
for the contour integral which requires the solution <strong>of</strong> several linear systems involving finite and<br />
boundary element matrices.<br />
New boundary element algorithm for heat conduction equation<br />
D.V. Yevdokymov (Dniepropetrovsk National University named after O. Honchar) Schedule<br />
Boundary element method has become powerful tool <strong>of</strong> numerical analysis because <strong>of</strong> high accuracy<br />
and unique opportunity <strong>of</strong> effective calculations in complex shape domains, al least, for<br />
linear elliptic boundary-value problems. However, nevertheless all mentioned advantages, general<br />
effectiveness <strong>of</strong> the boundary element method at the moment is very far from the best. Computational<br />
difficulties <strong>of</strong> boundary element applications to inhomogeneous or non-linear problems<br />
are so serious, that the method is practically not used in such field. Beside <strong>of</strong> that, there may<br />
be specific computational difficulties even for linear problems, for example, effectiveness <strong>of</strong> finite<br />
difference method for usual heat conduction equation is sufficiently higher, than boundary element<br />
method effectiveness. As a result, the field <strong>of</strong> effective using <strong>of</strong> boundary element method<br />
is restricted by linear elliptic problems. The aim <strong>of</strong> the present work is to develop such boundary<br />
element algorithm, which provides effectiveness comparable with finite difference method effectiveness<br />
at least for linear parabolic problems. Let us consider a heat conduction problem with<br />
traditional boundary condition and enough smooth initial condition. Thus the problem can be<br />
described by pure boundary integral equation, which provides analysis on boundary alone. Let us<br />
assumed that the problem is solved until n-th time step. To solve the problem on (n+1)-th time<br />
step let us introduce two sets <strong>of</strong> points: observation points, situated on the boundary, and collocation<br />
points, situated on the perpendicular to boundary on enough small (but non-asymptotically<br />
small) distance from correspondent observation points. Let us calculate the temperature values<br />
at collocation points, taking into account influences only previous n time steps. After that, the<br />
boundary thermal flux in observation point can by approximately determined by difference <strong>of</strong><br />
temperatures in observation and collocation points. The boundary condition and the obtained<br />
representation for thermal flux give an opportunity to calculate desired boundary values, thus<br />
the problem is solved on (n+1)-th time step without formulation <strong>of</strong> linear algebraic equation<br />
system and its computer solution. The proposed algorithm is similar to explicit finite difference<br />
and therefore it requires enough small time steps. The time step may be increased under using <strong>of</strong><br />
the simple iterative procedure. The proposed algorithm is illustrated by set <strong>of</strong> test calculations,<br />
which confirm its high effectiveness comparable with finite difference method especially for small<br />
times.<br />
S18.7: Finite Elements Thu, 13:30–15:30<br />
Chair: Otten S1|03–221
326 Section 18: Numerical methods <strong>of</strong> differential equations<br />
Full discretization <strong>of</strong> the porous medium/fast diffusion equation based on its very<br />
weak formulation<br />
Etienne Emmrich, David Šiška (<strong>Universität</strong> Bielefeld) Schedule<br />
The very weak formulation <strong>of</strong> the porous medium/fast diffusion equation yields an evolution problem<br />
in a Gelfand triple with the pivot space H −1 . This allows to employ methods <strong>of</strong> the theory <strong>of</strong><br />
monotone operators in order to study fully discrete approximations combining a Galerkin method<br />
(including conforming finite element methods) with the backward Euler scheme. Convergence is<br />
shown even for rough initial data and right-hand sides. The theoretical results are illustrated,<br />
in the one-dimensional case, for the piecewise constant finite element approximation <strong>of</strong> the porous<br />
medium equation with the δ-distribution as initial value. As a byproduct, L p -stability <strong>of</strong><br />
the H −1 -orthogonal projection onto the space <strong>of</strong> piecewise constant functions is shown for the<br />
one-dimensional case.<br />
Finite Element Approximation <strong>of</strong> the Stochastic Landau-Lifshitz-Gilbert Equation<br />
Lubomir Banas (Heriot-Watt University), Zdzislaw Brzeniak (University <strong>of</strong> York), Andreas Prohl<br />
(<strong>Universität</strong> Tübingen) Schedule<br />
The evolution <strong>of</strong> magnetization in ferromagnetic materials under the influence <strong>of</strong> thermal noise<br />
can be described by the stochastic Landau-Lifshitz-Gilbert (SLLG) equation<br />
�<br />
�<br />
�<br />
�<br />
dm(t, x) = −α m(t, x) × m(t, x) × Heff(t, x) − m(t, x) × Heff(t, x) dt<br />
+ν m(t, x) × ◦dW (t, x) ∀ (t, x) ∈ (0, T ) × D ,<br />
∂nm(t, x) = 0 ∀ (t, x) ∈ (0, T ) × ∂D ,<br />
m(0, x) = m0(x) ∀ x ∈ D ,<br />
where ‘◦’ denotes stochastic integration in the Stratonovich sense, α is a damping constant and<br />
ν is a temperature dependent parameter. The magnetization field m = (m1, m2, m3) satisfies a<br />
sphere constrain |m| = 1. The vector valued Wiener process dW = (W1, W2, W3) models the<br />
effects <strong>of</strong> the thermal noise. The effective field Heff may include a number <strong>of</strong> terms derived from<br />
the free energy, such as, e.g., exchange, anisotropy and magnetic field. We consider two type <strong>of</strong><br />
the noise: a noise uniform in space and a space-time white noise.<br />
We denote by Ik an equi-distant partition <strong>of</strong> [0, T ] into n sub-intervals <strong>of</strong> (local) size k = T/n;<br />
we denote ϕj+1/2 := 1<br />
�<br />
j+1 j ϕ + ϕ 2<br />
� . For simplicity we set Heff = ∆m. A finite-element based<br />
algorithm for the SLLG equation is given below.<br />
Algorithm A. Let Mj ∈ Vh be given for some time level j ≥ 0. The solution Mj+1 ∈ Vh on<br />
the next time level is determined from<br />
(Mj+1 − Mj �<br />
, Φ)h = −αk Mj+1/2 × [Mj+1/2 × � ∆hMj+1 �<br />
], Φ − k<br />
h<br />
� Mj+1/2 × � ∆hMj+1 , Φ �<br />
h<br />
+ν � Mj+1/2 × ∆Wj+1 , Φ �<br />
∀ Φ ∈ Vh ,<br />
where Vh is a finite element space <strong>of</strong> piecewise linear vector fields, (·, ·)h is a discrete (mass<br />
lumped) inner product, and � ∆h is a discrete Laplace operator.<br />
We discuss efficient implementation strategies for Algorithm A and present a number <strong>of</strong> computational<br />
studies including: long-time behaviour <strong>of</strong> finite ensembles <strong>of</strong> magnetic spins, finite-time<br />
finite-energy blow-up behaviour <strong>of</strong> solutions, and thermal fluctuations in magnetic nanoparticles.<br />
[1] Baňas L., and Brzeźniak Z., and Prohl A.: Convergent Finite Element Based Discretization<br />
<strong>of</strong> the Stochastic Landau-Lifshitz-Gilbert Equations. Submitted.<br />
h
Section 18: Numerical methods <strong>of</strong> differential equations 327<br />
Stable coupling <strong>of</strong> finite and boundary element methods<br />
Olaf Steinbach (TU Graz) Schedule<br />
We analyze the one-equation coupling <strong>of</strong> finite and boundary element methods which is very<br />
popular in applications since it requires only single and double layer integral operators, and which<br />
also allows the use <strong>of</strong> simple collocation schemes. We provide necessary and sufficient conditions<br />
to ensure ellipticity <strong>of</strong> the underlying bilinear form. Numerical examples confirm the sharpness<br />
<strong>of</strong> the theoretical estimates.<br />
On the visualization <strong>of</strong> solution <strong>of</strong> fractional differential equations<br />
Djurdjica Takači (University <strong>of</strong> Novi Sad) Schedule<br />
We consider a class <strong>of</strong> fractional differential equations (ordinary and partial) and construct its<br />
exact and approximate solution, The visualizations <strong>of</strong> fractional integral, fractional derivative and<br />
the approximate solution <strong>of</strong> fractional differential equations are presented by using the dynamic<br />
properties <strong>of</strong> package GeoGebra.<br />
On the error estimate for calculating some singular integrals<br />
Alexander V. Vasilyev (Belgorod State University, Russia), Vladimir B. Vasilyev (Lipetsk State<br />
Technical University, Russia) Schedule<br />
We consider multi-dimensional singular integral <strong>of</strong> convolution type<br />
�<br />
K(x − y)u(y)dy (1)<br />
R m<br />
with Calderon-Zygmund kernel K [1], and suggest to replace it by series’ sum over lattice points<br />
from Z m h (the lattice in Rm with step h). Assuming the kernel K has a certain smoothness<br />
property, the function u(y) satisfies the Hölder condition <strong>of</strong> order α, 0 < α < 1, and certain<br />
condition on decay at infinity, we show that the error between (1) and series’ sum is equivalent<br />
h α .<br />
[1] S. G. Mikhlin, S. Prössdorf, Singular Integral Operators, Berlin, Akademie-Verlag, 1986.<br />
S18.8: Theoretical Numerical Analysis Thu, 16:00–18:00<br />
Chair: Prohl S1|03–221<br />
A finite element method for a noncoercive elliptic problem with Neumann boundary<br />
conditions<br />
Klim Kavaliou, Lutz Tobiska (<strong>Universität</strong> Magdeburg) Schedule<br />
We study a noncoercive convection-diffusion problem with Neumann type boundary conditions<br />
appearing in modelling <strong>of</strong> magnetic fluid seals [1,2]. In [3] the existence and uniqueness <strong>of</strong> the<br />
continuous problem has been analyzed. The associated operator has a non-trivial one-dimensional<br />
kernel spanned by a positive function. A finite volume discretization was proposed in [4] which<br />
shows the same properties on the discrete level.<br />
We apply a maximum principle preserving low order finite-element approach developed in<br />
[5,6] for coercive convection-diffusion equations. The properties <strong>of</strong> the discrete problem and its<br />
relationship to the finite volume method in [4] are discussed. Under additional assumptions on<br />
the data both the continuous and discrete problem are coercive. Numerical tests confirm the<br />
theoretical predictions.
328 Section 18: Numerical methods <strong>of</strong> differential equations<br />
[1] S. Beresnev, V. Polevikov, and L. Tobiska, Numerical study <strong>of</strong> the influence <strong>of</strong> diffusion<br />
<strong>of</strong> magnetic particles on equilibrium shapes <strong>of</strong> a free magnetic fluid surface, Commun.<br />
Nonlinear Sci. Numer. Simulat. 14 (2009), 1403–1409<br />
[2] V. Polevikov and L. Tobiska, Influence <strong>of</strong> diffusion <strong>of</strong> magnetic particles on stability <strong>of</strong> a<br />
static magnetic fluid seal under the action <strong>of</strong> external pressure drop, Commun. Nonlinear<br />
Sci. Numer. Simulat. 16 (2011), 4021–4027<br />
[3] J. Droniu and J.-L. Vázquez, Noncoercive convection-diffusion elliptic problems with Neumann<br />
boundary conditions, Calc. Var. 34 (2009), 413–434<br />
[4] C. Chainais-Hillairet and J. Droniou, Finite-volume schemes for noncoercive elliptic problems<br />
with Neumann boundary conditions, IMA J. Numer. Anal. 31 (2011), 61–85<br />
[5] H.-G. Roos, M. Stynes, and L. Tobiska, Robust numerical methods for singularly perturbed<br />
differential equations. Convection-diffusion-reaction and flow problems, volume 24 <strong>of</strong><br />
Springer Series in Computational Mathematics, Springer-Verlag, Berlin (2008)<br />
[6] T. Ikeda, Maximum Principle in Finite Element Models for Convection-Diffusion Phenomena,<br />
North-Holland (1983)<br />
Adaptive exponential operator splitting methods for nonlinear evolution equations<br />
Mechthild Thalhammer (<strong>Universität</strong> der Bundeswehr München, <strong>Universität</strong> Innsbruck) Schedule<br />
In this talk, I shall primarily address the issue <strong>of</strong> efficient numerical methods for the space and<br />
time discretisation <strong>of</strong> nonlinear Schrödinger equations such as systems <strong>of</strong> coupled time-dependent<br />
Gross–Pitaevskii equations arising in quantum physics for the description <strong>of</strong> multi-component<br />
Bose–Einstein condensates. For the considered class <strong>of</strong> problems, a variety <strong>of</strong> contributions confirms<br />
the favourable behaviour <strong>of</strong> pseudo-spectral and exponential operator splitting methods<br />
regarding efficiency and accuracy. However, due to the fact that in the absence <strong>of</strong> an adaptive<br />
local error control in space and time, the reliability <strong>of</strong> the numerical solution and the performance<br />
<strong>of</strong> the space and time discretisation strongly depends on the experienced scientist selecting the<br />
space and time grid in advance, I will exemplify different approaches for the reliable time integration<br />
<strong>of</strong> Gross–Pitaevskii systems on the basis <strong>of</strong> a local error control for splitting methods. The<br />
approach also extends to other problem classes such as parabolic problems.<br />
An adaptive DG space-time method<br />
Martin Neumüller, Olaf Steinbach (TU Graz) Schedule<br />
For evolution equations we present a flexible space-time method based on Discontinuous Galerkin<br />
finite elements. Space-time methods have advantages when we have to deal with moving domains<br />
and if we want to do local refinement in the space-time domain. For this we use a residual based<br />
error estimator. This method will be applied to the heat equation and to the Navier Stokes equations.<br />
Numerical examples and some applications will be given.<br />
Exponential decay <strong>of</strong> two-dimensional rotating waves<br />
Denny Otten (<strong>Universität</strong> Bielefeld) Schedule<br />
In this talk we show exponential decay in space and time for solution kernels <strong>of</strong> complex-valued<br />
parabolic systems in several dimensions with negative absolute term. The convection terms <strong>of</strong><br />
these systems have unbounded coefficients and they are <strong>of</strong> rotational type.
Section 18: Numerical methods <strong>of</strong> differential equations 329<br />
A model equation in R 2 is given by<br />
Ut = A△U + cDφU + B(x)U, x ∈ R 2<br />
where U(x, t) ∈ C N , 0 �= c ∈ R, A ∈ C N,N is positive definite and B(x) ∈ C N,N converges to some<br />
negative definite matrix as |x| → ∞. By Dφ we denote the angular derivative which in Cartesian<br />
coordinates reads Dφ := −x2D1 + x1D2.<br />
For the constant coefficient operator obtained for |x| → ∞ we derive a representation for the<br />
solution kernel from the Feynman-Kac formula. This is used to show exponential decay in time<br />
and space for solutions <strong>of</strong> the variable coefficient inhomogeneous equation. Moreover, this also<br />
leads to exponential decay for the stationary equation.<br />
This study is motivated by the stability problem for rotating waves in several variables.<br />
Adaptive stochastic collocation on sparse grids<br />
Bettina Schieche, Jens Lang (TU <strong>Darmstadt</strong>) Schedule<br />
Keywords: PDEs with random parameters, stochastic collocation, error estimation, adaptivity.<br />
Numerical simulations become more reliable if random effects are taken into account. To this end,<br />
the describing parameters can be expressed by random variables or random fields, which leads to<br />
partial differential equations (PDEs) with random parameters.<br />
Common numerical methods to solve such problems are spectral methods <strong>of</strong> Galerkin type<br />
[1] and stochastic collocation on sparse grids [2,3]. We focus on stochastic collocation, because it<br />
decouples the random PDE into a set <strong>of</strong> deterministic equations that can be solved in parallel.<br />
In order to keep the computational costs at a moderate level, it is inevitable to place the collocation<br />
points adaptively. Therefore, error estimates are required. For spectral methods, adjoint<br />
a posteriori error analysis has been proposed in [4].<br />
We want to combine stochastic collocation with an adjoint approach in order to estimate the<br />
error <strong>of</strong> some stochastic quantity, such as the mean or variance <strong>of</strong> a solution functional. Thereby,<br />
our goal is to develop appropriate error estimates that require less computational effort then the<br />
solution itself.<br />
[1] B. Schieche, Stochastische finite Elemente, diploma thesis, 2009<br />
[2] B. Schieche, Stochastic Analysis <strong>of</strong> Nusselt Numbers for Natural Convection with Uncertain<br />
Boundary Conditions, Preprint, 2010<br />
[3] F. Nobile, R. Tempone, C.G. Webster, An anisotropic sparse grid stochastic collocation method<br />
for partial differential equations with random input data, SIAM J. Numer. Anal., 46, pp<br />
2411–2442, 2008.<br />
[4] L. Mathelin, O.P. Le Maître, Uncertainty quantification in a chemical system using error<br />
estimate-based mesh adaptation, TCFD, (in press)
330 Section 19: Optimization <strong>of</strong> differential equations<br />
Section 19: Optimization <strong>of</strong> differential equations<br />
Organizers: Roland Herzog (TU Chemnitz), Barbara Kaltenbacher (Alpen-Adria <strong>Universität</strong><br />
Klagenfurt)<br />
S19.1: Algorithmic Approaches I Tue, 13:30–15:30<br />
Chair: Roland Herzog S1|03–121<br />
Unified numerical treatment for optimal transport <strong>of</strong> geometric objects<br />
Andreas Günther (Zuse-Institut Berlin) Schedule<br />
An important task in medical imaging is segmentation <strong>of</strong> anatomical objects. Identifying corresponding<br />
points on different shapes is therefore a fundamental prerequisite for quantitative shape<br />
analysis.<br />
Currents provide a unified mathematical description <strong>of</strong> geometrical objects <strong>of</strong> dimension 0<br />
(points), 1 (curves), 2 (surfaces) or 3 (volumes) which are embedded in R 3 . The Large Deformation<br />
Diffeomorphic Metric Mapping framework [Joshi and Miller, IEEE Transactions on Image<br />
Processing, 2000] solves the correspondence problem between them by evolving a displacement<br />
field along a velocity field.<br />
In this talk we develop two innovative aspects for this ode / pde optimization problem: First,<br />
we spatially discretize the velocity field with conforming adaptive finite elements and discuss<br />
advantages <strong>of</strong> this new approach. Second, we directly compute the temporal evolution <strong>of</strong> discrete<br />
m-current attributes. Numerical tests confirm the practicability <strong>of</strong> our findings.<br />
Semismooth Newton for time-optimal control <strong>of</strong> parabolic equations<br />
Konstantin Pieper, Boris Vexler (TU München) Schedule<br />
We consider a time-optimal control problem where the state u is subject to the nonlinear parabolic<br />
equation<br />
∂tu(t) + Au(t) + ϕ(u(t)) = q(t) in Ω for t ∈ (0, T ),<br />
u(0) = u0.<br />
The control q has to be admissible with respect to the pointwise constraints qa ≤ q(t) ≤ qb for all<br />
t ∈ (0, T ). The objective is now to find a control which minimizes the transfer time<br />
min T<br />
such that u is driven sufficiently close to some target condition ud, i.e.,<br />
�u(T ) − ud� L 2 (Ω) ≤ δ.<br />
To derive an efficient numerical algorithm for the time-optimal problem, we consider a Tichonovregularized<br />
version and analyze the influence <strong>of</strong> the regularization parameter on the optimal solutions.<br />
Finally we describe a semismooth Newton method for the regularized problem where<br />
the time T and the control q are updated simultaneously in each iteration. When incorporating<br />
the pointwise control constraints into the Newton method, we also have to be careful to retain<br />
symmetry <strong>of</strong> the linear system which is solved in each step.<br />
An Approach to Shape Optimization with State Constraints<br />
Christian Leithäuser (Fraunh<strong>of</strong>er ITWM, TU Kaiserslautern), Robert Feßler (Fraunh<strong>of</strong>er ITWM)<br />
Schedule
Section 19: Optimization <strong>of</strong> differential equations 331<br />
We study an approach into shape optimization with state constraints by considering flow problems<br />
controlled by the shape <strong>of</strong> the domain with certain constraints on the flow velocity. Especially<br />
this enables us to deal with supremum norm cost functions, but also other state constraints are<br />
possible.<br />
For simplicity we model the domain dependency through conformal metrics, which leads to a<br />
flow problem on a fixed reference domain where the shape dependency is contained in the differential<br />
operators. In order to solve the optimization problem the state equations and constraints<br />
are discretized leading to a nonlinear programming problem which can be solved on the discrete<br />
level.<br />
A Robust Solver for Distributed Optimal Control for Stokes Flow<br />
Markus Kollmann, Walter Zulehner (<strong>Universität</strong> Linz) Schedule<br />
In this talk we consider the following optimal control problem:<br />
subject to<br />
Minimize J(u, f) = 1<br />
2<br />
||u − ud|| L<br />
2 2 α<br />
(Ω) +<br />
2 ||f||2L<br />
2 (Ω)<br />
−∆u + ∇p = f in Ω<br />
div u = 0 in Ω<br />
u = 0 on Γ<br />
+ inequality constraints.<br />
Here Ω is an open and bounded domain in R d (d ∈ {1, 2, 3}), Γ denotes the boundary and α > 0<br />
is a cost parameter. We consider two types <strong>of</strong> inequality constraints:<br />
• inequality constraints on the control f,<br />
• inequality constraints on the state u.<br />
In both cases, the first order system <strong>of</strong> necessary and sufficient optimality conditions <strong>of</strong> (1) is<br />
nonlinear. A semi-smooth Newton iteration is applied in order to linearize the system. In every<br />
Newton step a linear saddle point system has to be solved (after discretization). For these linear<br />
systems solvers are discussed. Numerical examples are given which illustrate the theoretical results.<br />
Lossy Compression <strong>of</strong> State Trajectories<br />
Sebastian Götschel, Martin Weiser (Zuse Institute Berlin) Schedule<br />
In large-scale, time-dependent optimal control problems, adjoint methods for gradient computations<br />
are <strong>of</strong>ten employed. As the state enters into the adjoint equation, the state trajectory has<br />
to be stored, which can result in high demand <strong>of</strong> storage capacity and bandwidth. In this talk<br />
we address lossy compression <strong>of</strong> state trajectories as a means to reduce these demands, without<br />
a significant loss <strong>of</strong> accuracy or increase <strong>of</strong> computational complexity. We present a-priori error<br />
estimates as well as heuristic schemes for adaptively selecting the quantization level. The different<br />
trade-<strong>of</strong>fs compared to checkpointing or model reduction are discussed. Quantitative aspects are<br />
illustrated on numerical examples.<br />
S19.2: Algorithmic Approaches II Tue, 16:00–18:00<br />
Chair: Anton Schiela S1|03–121<br />
(1)
332 Section 19: Optimization <strong>of</strong> differential equations<br />
Adaptive Multilevel SQP-Methods with Reduced Order Models for PDE-constrained<br />
Problems<br />
Jan Carsten Ziems, Stefan Ulbrich (TU <strong>Darmstadt</strong>) Schedule<br />
We present an adaptive multilevel generalized SQP-method for optimal control problems governed<br />
by nonlinear time-dependent PDEs with control constraints. For such problems, standard<br />
discretization techniques require in general many degrees <strong>of</strong> freedom for the optimization process<br />
and a good resolution <strong>of</strong> the optimal solution which is very time consuming. To overcome this<br />
difficulty the algorithm generates a hierarchy <strong>of</strong> adaptively refined discretizations. The discretized<br />
problems are then each approximated by an adaptively generated sequence <strong>of</strong> reduced order<br />
models. The adaptive refinement strategies are based on a posteriori error estimators for the<br />
original and the discretized PDE, the adjoint PDE and a criticality measure. In our numerical<br />
examples we construct the reduced order models by the proper orthogonal decomposition (POD)<br />
method from snapshots <strong>of</strong> the state and adjoint state. The effort for the nonlinearities <strong>of</strong> the<br />
resulting POD Galerkin discretization is additionally reduced by the discrete empirical interpolation<br />
method (DEIM) recently proposed by Chaturantabut and Sorensen. Numerical results for<br />
test problems and a 3D glass cooling application are presented.<br />
The Quadratic Penalty Method for solving Control-Constrained Optimal Control<br />
Problems<br />
Max Winkler (<strong>Universität</strong> der Bundeswehr München), Christian Grossmann (TU Dresden) Schedule<br />
We consider a method for solving elliptic optimal control problems with control constraints. The<br />
constraints are penalized by the quadratic penalty function. The resulting parameter-dependent<br />
unconstrained problems are investigated for existence and uniqueness <strong>of</strong> solutions, optimality<br />
conditions and convergence <strong>of</strong> its solutions.<br />
It can be proven [1] that the auxiliary solutions converge linearly towards the optimal control.<br />
The optimality condition <strong>of</strong> the auxiliary problems possess a resolution for the control depending<br />
only on the adjoint state. Thus, one can eliminate the control out <strong>of</strong> the optimality system. This<br />
leads to a nonlinear homotopy mapping whose roots characterize a central path towards the solution<br />
<strong>of</strong> the original optimal control problem. Since Fréchet differentiability is not given for this<br />
mapping we have to apply semi-smooth Newton methods for the solution <strong>of</strong> this operator equation.<br />
These methods converge Q-superlinearly and even Q-quadratically under some additional<br />
assumptions.<br />
[1] Ch. Grossmann, M. Winkler, Mesh-Independent Convergence <strong>of</strong> Penalty Methods Applied<br />
to Optimal Control with Partial Differential Equations, submitted (2011)<br />
Optimization <strong>of</strong> PDEs with state constraints via Infinite Penalization methods<br />
Richard C Barnard, Martin Frank, Michael Herty (RWTH Aachen) Schedule<br />
We consider optimization problems constrained by partial differential equations (PDEs) with additional<br />
constraints placed on the solution <strong>of</strong> the PDEs. We develop a general framework using<br />
infinite-valued penalization functions and Clarke subgradients and apply this to problems with<br />
box constraints as well as constraints arising in applications, such as constraints on the average<br />
value <strong>of</strong> the state in subdomains. We present numerical results <strong>of</strong> this algorithm for the elliptic<br />
case and compare with other state-constrained algorithms.<br />
Space Mapping Optimization and Model Hierarchies<br />
Rene Pinnau (TU Kaiserslautern) Schedule
Section 19: Optimization <strong>of</strong> differential equations 333<br />
Industrial optimization problems <strong>of</strong>ten require information on the adjoint variables for very complex<br />
model equations. Typically, there is a whole hierarchy <strong>of</strong> models available which allows to<br />
balance the computational costs and the exactness <strong>of</strong> the model. We use these hierarchies in combination<br />
with space mapping techniques to speed up the convergence <strong>of</strong> optimization algorithms.<br />
In this talk we present three applications where this approach proved to be very successful. We<br />
will cover questions from semiconductor design, the control <strong>of</strong> particles in fluids and shape optimization<br />
for filters.<br />
An Adaptive Semismooth Newton-CG Method for Constrained Parameter Identification<br />
in Seismic Tomography<br />
Christian Böhm, Michael Ulbrich (TU München) Schedule<br />
Earthquakes excite seismic waves that propagate through the Earth and can be recorded as seismograms<br />
at remote receiver locations. Seismic tomography means to infer the Earth’s material<br />
structure based on these observations. This can be stated as a PDE-constrained optimization<br />
problem that seeks to minimize the misfit between observed and synthetically generated seismograms.<br />
We present a semismooth Newton-CG method for full-waveform seismic inversion with boxconstraints<br />
on the material parameters. The implementation features the adjoint-based computation<br />
<strong>of</strong> the gradient and Hessian-vector products <strong>of</strong> the reduced problem, a Krylov subspace<br />
method to solve the Newton system in matrix-free fashion and globalization by a trust-region<br />
method.<br />
The governing equations are given by a coupled system <strong>of</strong> the acoustic and elastic wave<br />
equation for the numerical simulation in solid and fluid media. The wave equation is spatially<br />
discretized by high-order Lagrange polynomials and solved with an explicit time-stepping scheme.<br />
The parallel implementation utilizing MPI communication enables us to tackle large-scale seismic<br />
inverse problems.<br />
The ill-posedness <strong>of</strong> the problem is addressed by inverting sequentially for increasing frequencies.<br />
Thereby, the parameter grid is adaptively refined using goal-oriented a-posteriori error<br />
estimates. This enables us to choose the resolution <strong>of</strong> the reconstruction based on the information<br />
that is provided by the observed data.<br />
We show numerical results for the application <strong>of</strong> our method to a dataset <strong>of</strong> marine geophysical<br />
exploration in the North Sea.<br />
We gratefully acknowledge the support <strong>of</strong> this work by the Munich Centre <strong>of</strong> Advanced Computing<br />
and by the DFG.<br />
S19.3: Numerics and Error Estimation I Wed, 13:30–15:30<br />
Chair: Carsten Ziems S1|03–121<br />
Finite element error estimates for parabolic optimal control problems with semilinear<br />
state equation<br />
Ira Neitzel, Boris Vexler (TU München) Schedule<br />
In this talk, we present a priori error estimates for the space-time finite element discretization<br />
<strong>of</strong> control constrained optimal control problems governed by semilinear parabolic PDEs. We discuss<br />
a dG(0)cG(1) discretization <strong>of</strong> the state equation, i.e. we discretize it piecewise constant in<br />
time and cellwise (bi)linear in space. We extend error estimates shown by Meidner and Vexler<br />
for a linear-quadratic setting. Throughout, we focus on the specific difficulties introduced by the<br />
nonlinear state equation, such as associated boundedness resultson the semidiscrete and discrete<br />
level independent <strong>of</strong> the discretization parameters, as well as second-order sufficient optimality
334 Section 19: Optimization <strong>of</strong> differential equations<br />
conditions with quadratic growth conditions in L 2 -neighborhoods. We foucs in detail on piecewise<br />
constant control discretization and briefly discuss different types <strong>of</strong> control discretization and the<br />
extension to certain different problem classes such as problems with Lavrentiev-regularized state<br />
constraints, cf. the results by Hinze and Meyer for elliptic problems. We end the talk by showing<br />
some numerical experiments.<br />
Shape sensitivity analysis in the extended finite element method<br />
Franz-Joseph Barthold, Daniel Materna (TU Dortmund) Schedule<br />
The stiffness matrix K = ∂R/∂U , the pseudo load matrix P = ∂R/∂X and the sensitivity<br />
matrix S = −K −1 P can be derived from the residual vector R (weak form) by the analytical derivative<br />
(variation) with respect to the nodal displacements (displacement field) U and the nodal<br />
coordinates (geometry field) X, respectively. Thus, any design variation ∆X generates a variation<br />
<strong>of</strong> the displacement ∆U = S ∆X. These derivatives must be derived, implemented and computed<br />
in a consistent fashion to the underlying structural analysis. The term consistent linearisation is<br />
well-known in nonlinear continuum mechanics and nonlinear finite element methods and regularly<br />
applied to compute the consistent stiffness matrix K.<br />
This technique is applied to sensitivity analysis as well to derive the above mentioned pseudo<br />
load matrix P in a consistent way both with the physical (displacement field) as well as material<br />
(geometry field) model, see [?]. Nevertheless, it is practically important to set up a reliable<br />
technique to check all derived sensitivities in comparison with the numerical sensitivities.<br />
We outline our strategy to instantaneously check the analytical sensitivities with finite difference<br />
values for different classes <strong>of</strong> design variables. This is especially important for the extended<br />
finite element method (XFEM) and the above explained difficult situation <strong>of</strong> general shapes <strong>of</strong><br />
the background mesh and the great influence <strong>of</strong> the chosen integration scheme. We outline what<br />
kind <strong>of</strong> differences between both variants can be expected and tolerated.<br />
The combined shape optimisation <strong>of</strong> the overall domain as well as <strong>of</strong> the internal boundaries<br />
violates some <strong>of</strong> the assumptions <strong>of</strong> standard XFEM approaches. Thus, special attention has to<br />
be devoted to a consistent approach both in structural and sensitivity analysis. Here, the choice<br />
<strong>of</strong> Ansatz functions modelling the desired discontinuities along the interfaces in the element<br />
must be considered and revised. These modifications should be designed such that the described<br />
complexities are unlikely to occur in case <strong>of</strong> general design modifications. Furthermore, existing<br />
elements from sensitivity analysis <strong>of</strong> traditional finite elements should adequately be applied to<br />
XFEM. Thus, XFEM could be a model problem where the complexity <strong>of</strong> sensitivity analysis<br />
dominates the choice <strong>of</strong> the underlying structural analysis model.<br />
In this talk, we like to outline a modified XFEM formulation which is proved to generate<br />
correct sensitivity information for shape modifications <strong>of</strong> the background mesh as well as <strong>of</strong> the<br />
level set based boundaries <strong>of</strong> multi-material designs. Numerical examples illustrate the advocated<br />
theoretical concept.<br />
Time discretization with almost third order convergence for parabolic optimal control<br />
problems with control constraints<br />
Andreas Springer, Boris Vexler (TU München) Schedule<br />
We consider a linear quadratic parabolic optimal control problem with time-dependent control<br />
and box constraints on the control. For such problems it is straightforward to show that a timediscrete<br />
solution with second order convergence can be obtained either by the variational discretization<br />
approach or by a post-processing strategy. Here, by combining those two approaches we<br />
demonstrate that almost third order convergence with respect to the size <strong>of</strong> the time steps can<br />
be achieved.
Section 19: Optimization <strong>of</strong> differential equations 335<br />
To this end we discretize the state variable in time with the piecewise linear discontinuous Galerkin<br />
(dG(1)) method. The control is not discretized but instead computed from the semidiscrete<br />
adjoint state through the first order optimality condition. Exploiting superconvergence properties<br />
<strong>of</strong> the dG(1) method at the nodes <strong>of</strong> the Radau quadrature, we reconstruct an improved adjoint<br />
state from the optimal adjoint <strong>of</strong> the semidiscrete equation by piecewise quadratic interpolation.<br />
It is shown that this reconstructed adjoint converges with almost third order as the fineness <strong>of</strong><br />
the time discretization approaches zero. An improved control solution is obtained by point-wise<br />
projection <strong>of</strong> this reconstructed adjoint, again employing the first order optimality condition. This<br />
post-processed solution also converges with almost order three with respect to the size <strong>of</strong> the time<br />
step.<br />
A-posteriori verification <strong>of</strong> optimality conditions for control problems with finitedimensional<br />
control space<br />
Saheed Akindeinde, Daniel Wachsmuth (Johann Radon Institute for Computational and Applied<br />
Mathematics) Schedule<br />
In this paper we investigate non-convex optimal control problems. We are concerned with aposteriori<br />
verification <strong>of</strong> sufficient optimality conditions. If the proposed verification method confirms<br />
the fulfillment <strong>of</strong> the sufficient condition then a-posteriori error estimates can be computed.<br />
A special ingredient <strong>of</strong> our method is an error analysis for the Hessian <strong>of</strong> the underlying optimization<br />
problem. We derive conditions under which positive definiteness <strong>of</strong> the Hessian <strong>of</strong> the<br />
discrete problem implies positive definiteness <strong>of</strong> the Hessian <strong>of</strong> the continuous problem. The article<br />
is complemented with numerical experiments.<br />
Optimality conditions based on a numerical approximation<br />
Martin Naß, Arnd Rösch (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
We consider an abstract nonlinear optimization problem. We derive sufficient optimality conditions<br />
for a local solution ū based on a coercivity condition for a known numerical approximation<br />
ūh. Further we derive error estimates for ū in terms <strong>of</strong> the discretization parameter h, assumed<br />
the sufficient optimality conditions are fulfilled. The results are specified on an example <strong>of</strong> an<br />
optimal control problem with pointwise state constraints.<br />
S19.4: Numerics and Error Estimation II Wed, 16:00–18:00<br />
Chair: Ira Neitzel S1|03–121<br />
A Multiharmonic Finite Element Solver for Time-Periodic Parabolic Optimal Control<br />
Problems<br />
Ulrich Langer (<strong>Universität</strong> Linz) Schedule<br />
This paper presents the numerical analysis <strong>of</strong> distributed parabolic optimal control problems<br />
in a time-periodic setting. In particular, the desired state and the control are assumed to be<br />
time-periodic. After eliminating the control from the optimality system, we arrive at the reduced<br />
optimality system for the state and the co-state that is nothing but a coupled system <strong>of</strong> a<br />
forward and a backward parabolic partial differential equation (PDE). Due to the linearity, the<br />
state and the co-state are time-periodic as well. This coupled system <strong>of</strong> PDEs is discretized by<br />
the multiharmonic finite element method. Finally, we arrive at a large system <strong>of</strong> algebraic equations,<br />
which fortunately decouples into smaller systems each <strong>of</strong> them defining the cosine and sine<br />
Fourier coefficients for the state and co-state with respect to a single frequency. For these smaller<br />
systems, we construct preconditioners resulting in a fast converging minimal residual solver with<br />
a parameter-independent convergence rate. All these systems can be solved totally in parallel
336 Section 19: Optimization <strong>of</strong> differential equations<br />
with optimal or, at least, almost optimal complexity.<br />
This talk is based on a joint work with M. Kollmann, M. Kolmbauer, M. Wolfmayr and W.<br />
Zulehner. We gratefully acknowledge the financial support by the Austrian Science Fund (FWF)<br />
under the grants DK W1214 (projects DK4 and DK12) and P19255. We also thank the Austria<br />
Center <strong>of</strong> Competence in Mechatronics (ACCM), which is a part <strong>of</strong> the COMET K2 program <strong>of</strong> the<br />
Austrian Government, for supporting our work on optimization problems with PDE constraints<br />
in electromagnetics.<br />
Identification <strong>of</strong> an unknown parameter in the main part <strong>of</strong> an elliptic PDE<br />
Ute Aßmann, Arnd Rösch (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
We are interested in identifying an unknown material parameter a(x) in the main part <strong>of</strong> an<br />
elliptic partial differential equation<br />
−div (a(x) grad y(x)) = g(x) in Ω<br />
with corresponding boundary conditions. We discuss a Tichonov regularization<br />
min<br />
a J(y, a) = �y − yd� 2<br />
L 2 (Ω) + α�a�2 H s (Ω)<br />
with s > 0. Moreover, we require the following constraints for the unknown parameter<br />
0 < amin ≤ a(x) ≤ amax.<br />
The talk starts with results on existence <strong>of</strong> solutions and necessary and sufficient optimality conditions.<br />
The second part <strong>of</strong> the talk will be devoted to numerical aspects and recent results <strong>of</strong> the<br />
problem.<br />
Transient simultaneous multi-layered shape and material optimization for elastic vocal<br />
fold models<br />
Bastian Schmidt, Michael Stingl (<strong>Universität</strong> Erlangen-Nürnberg) Schedule<br />
Multi-layered bodies, characterized by at least two inner parts with different materials, are frequently<br />
used in various industrial or medical applications. The numerical optimization <strong>of</strong> the outer<br />
shape <strong>of</strong> these bodies as well as the material properties within the layers with respect to a given<br />
cost criterion are standard questions addressed in shape and material optimization, respectively.<br />
We consider a combination <strong>of</strong> both these techniques, however, we are interested in optimizing<br />
the inner partition <strong>of</strong> the body into its layers and material parameters in each <strong>of</strong> the layers<br />
while keeping the outer shape fixed. This is done by allowing shape parameters to modify a given<br />
reference configuration. Moreover, we use a tracking type objective functional in order to minimize<br />
the distance between a given reference displacement field and the response <strong>of</strong> the elastic body<br />
with respect to one or several dynamic loading scenarios.<br />
We present a rigorous mathematical formulation <strong>of</strong> the optimization problem and state equation<br />
together with results for existence <strong>of</strong> solutions and analysis <strong>of</strong> convergence <strong>of</strong> suitable discretizations<br />
involving a transient finite-element approach with either isotropic or transversal-isotropic<br />
material. Furthermore we apply the adjoint method in order to derive an adjoint problem allowing<br />
the efficient calculation <strong>of</strong> shape and material gradients and thus the use <strong>of</strong> gradient based<br />
optimization algorithms.<br />
We demonstrate the feasibility <strong>of</strong> the approach by a numerical study in the framework <strong>of</strong><br />
which the behavior <strong>of</strong> a numerical model <strong>of</strong> the human vocal folds is optimally adapted to a set<br />
<strong>of</strong> measured displacement fields obtained from physical experiments.
Section 19: Optimization <strong>of</strong> differential equations 337<br />
Adjoint Based Optimal Control <strong>of</strong> Multiphase Multicomponent Flow in Porous Media<br />
with Applications to CO2 Sequestration in Underground Reservoirs<br />
Moritz Simon, Michael Ulbrich (TU München) Schedule<br />
With the target <strong>of</strong> optimizing CO2 sequestration in underground reservoirs, we investigate constrained<br />
optimal control problems with multiphase multicomponent flow in porous media. Currently,<br />
we consider a two-phase (wetting and non-wetting), two-component (saline water and CO2)<br />
model, and the objective is to maximize the amount <strong>of</strong> trapped CO2 in an underground reservoir<br />
after a fixed period <strong>of</strong> CO2 injection. The time-dependent injection rates in multiple wells are<br />
used as control parameters. Extensions to more general models and to other optimization variables<br />
or objectives are readily possible. We describe the governing multiphase multicomponent Darcy<br />
flow PDE system, formulate the optimal control problem and derive the corresponding adjoint<br />
equations.<br />
For the discretization we use a variant <strong>of</strong> the BOX method, a control volume FE method with<br />
linear Lagrange elements on the primal mesh and piecewise constant test functions on the dual<br />
mesh. The timestep-wise Lagrange function <strong>of</strong> the control problem is implemented as a variational<br />
form in Sundance, a toolbox for rapid development <strong>of</strong> parallel finite element simulations, which<br />
is part <strong>of</strong> the HPC s<strong>of</strong>tware Trilinos. The symbolic capabilities <strong>of</strong> Sundance allow to derive the<br />
discrete state equation, adjoint equation and reduced gradient automatically from this variational<br />
form. In order to prepare Sundance for the BOX method, several new concepts, like control volume<br />
boundary integrals and upwinding, were added to its core structure.<br />
Via a C++ interface, the Sundance state and adjoint solvers are linked to the interior point<br />
optimization code IPOPT. Since we currently do not provide second derivative information, the<br />
interface is configured to use limited memory BFGS updates for approximating the Hessian matrix<br />
<strong>of</strong> the Lagrange function. The (non-)linear systems in the forward and adjoint simulations are<br />
solved in parallel, using interfaces to packages such as NOX, Amesos and AztecOO within Trilinos.<br />
In this talk we present several optimization results for partially miscible two-phase flow in both<br />
homogeneous and inhomogeneous reservoirs.<br />
The presented work is conducted in project K1 <strong>of</strong> the Munich Centre <strong>of</strong> Advanced Computing<br />
(MAC) within the KAUST–TUM Special Partnership. The funding by the King Abdullah<br />
University <strong>of</strong> Science and Technology (KAUST, Saudi Arabia) is gratefully acknowledged.<br />
Implementation and validation <strong>of</strong> an adjoint high-Reynolds number model for thermally<br />
driven flows<br />
Anne Lincke, Arthur Stück, Thomas Rung (TU Hamburg) Schedule<br />
This paper presents a high-Reynolds number (high-Re) approach to the adjoint Navier-Stokes-<br />
Fourier equations based upon a modified high-Re sensitivity equation for buoyancy-driven flows.<br />
For reasons <strong>of</strong> efficiency, the computational framework adheres to the continuous adjoint method<br />
using a frozen-turbulence assumption. In former approaches the primal equations were either solved<br />
with a wall function or a low-Re approach at the boundary, whereas the adjoint equations<br />
were usually solved without any wall function features. The consequence is an inconsistent treatment<br />
<strong>of</strong> the primal and adjoint equations which leads to sensitivity-errors. Opposed to the state<br />
<strong>of</strong> the art, the present model uses a high-Re model for the primal equations and a high-Re model<br />
for the adjoint equations. The adjoint high-Re model can easily be implemented and be used<br />
for flow problems where wall functions are needed. The impact <strong>of</strong> this approach is an improved<br />
consistency <strong>of</strong> primal and adjoint equations which leads to stable and realistic shape optimization<br />
results for industrial flows.<br />
In the first part <strong>of</strong> the paper a high-Re model for solving the adjoint Navier-Stokes-Fourier
338 Section 19: Optimization <strong>of</strong> differential equations<br />
equations is introduced. The idea is to transfer the information <strong>of</strong> the law <strong>of</strong> the wall directly into<br />
the adjoint system. This also leads to a modified sensitivity equation which adheres to the wall<br />
function.<br />
In the second part <strong>of</strong> the paper the model is validated by incompressible, steady-state test<br />
cases. Examples included are restricted to ducted flows. Results are compared to simulations<br />
where no wall functions are used for the primal and the dual solution. It can be seen that the<br />
sensitivities provided by the new application are smoother and therefore the design cycle becomes<br />
less sensitive to the step size.<br />
Keywords: adjoint Navier-Stokes-Fourier equations, buoyancy-driven flow, frozen-turbulence<br />
model, design optimization, shape sensitivities, wall functions.<br />
Optimal Control <strong>of</strong> the Wave Equation with Trigonometric Operators<br />
Stefan Reiterer (<strong>Universität</strong> Graz) Schedule<br />
In our work we consider minimization <strong>of</strong> a quadratic functional <strong>of</strong> the form<br />
subject to the wave equation<br />
1<br />
α<br />
�y − z�2 L2(0,T ;V ) +<br />
2 2 �u�2 L2(0,T ;H) ,<br />
∂2 y + Ay = βu,<br />
∂t2 y(0) = y0,<br />
yt(0) = y1,<br />
where V ⊂ H are Hilbert spaces, A : V → H is an linear elliptic operator, and the initial data<br />
y0 ∈ V , y1 ∈ H, as the constant α > 0, and the weight function β are given.<br />
To minimize the functional we use an inexact Conjugate Gradient Method on the operator<br />
S ∗ S+αI, where S : L2(0, T ; H) → H 1 (0, T ; V ) denotes the solution operator <strong>of</strong> the wave equation.<br />
The evaluation <strong>of</strong> the operators is realized with help <strong>of</strong> the Gautschi timestepping method proposed<br />
by Hochbbruck and Lubich in [1], where we evaluate the occurring trigonometric operators<br />
with help <strong>of</strong> rational Krylov methods proposed by Hochbbruck and Grimm in [2].<br />
We will prove convergence, and structural properties <strong>of</strong> the occurring optimization scheme in<br />
this abstract setting. Additionally we provide numerical results whith spectral element methods<br />
for space discretization. We will also outline benefits and drawbacks <strong>of</strong> this approach and discuss<br />
fast implementation and preconditioning <strong>of</strong> the algorithms.<br />
[1] M. Hochbruck, C. Lubich, A Gautschi-type method for oscillatory second-order differential<br />
equations Numerische Mathematik Vol. 83, Nr. 3 (1999) 403–426<br />
[2] V. Grimm and M. Hochbruck, Rational approximation to trigonometric operators, BIT Numerical<br />
Mathematics Vol. 48, Nr. 2 (2008), 215–229, Springer<br />
S19.5: Applications I Thu, 13:30–15:30<br />
Chair: Andreas Günther S1|03–121<br />
PDE-constrained optimization in electromagnetic problems<br />
Irwin Yousept (TU Berlin) Schedule
Section 19: Optimization <strong>of</strong> differential equations 339<br />
Electromagnetism plays an essential role in many modern advanced technologies and applications.<br />
Optimal control and parameter estimation <strong>of</strong> electromagnetic problems are delicate issues and<br />
call for a careful study. In this talk, we discuss application problems arising from electromagnetic<br />
induction heating, electrorheological (ER) fluids, and parameter estimation <strong>of</strong> electromagnetic<br />
materials. Recent theoretical and numerical results <strong>of</strong> these topics are presented.<br />
Multilevel Optimization for PDAE-Constrained Optimal Control Problems - Application<br />
to Radiative Heat Transfer in 3d<br />
Debora Clever (TU <strong>Darmstadt</strong>) Schedule<br />
During the last decade it has been becoming <strong>of</strong> growing interest to not only simulate the behavior<br />
<strong>of</strong> engineering, medical or financial applications but to also optimize their performance. Modeling<br />
the considered process by a system <strong>of</strong> space-time dependent partial differential algebraic equations<br />
(PDAEs), the task can be formulated as a PDAE-constrained optimal control problem, most likely<br />
with additional constraints on control and state. For real world applications, the bottleneck <strong>of</strong><br />
solving such problems is the high complexity <strong>of</strong> the involved PDAEs, which have to be solved<br />
several times within each optimization iteration. Therefore, an efficient optimization environment<br />
has to combine highly efficient optimization techniques with fully adaptive PDAE solvers <strong>of</strong> high<br />
order. To even gain more efficiency without loss <strong>of</strong> accuracy for the optimal control, multilevel<br />
techniques are an attractive means.<br />
We present an approach, where we reduce the considered problem to the control component<br />
and apply a generalized multilevel SQP-method [1,2]. Control constraints are handled by an appropriate<br />
projection. Reduced gradients and actings <strong>of</strong> the reduced Hessian are computed with<br />
the continuous adjoint approach. We follow Rothe’s method with adaptive Rosenbrock methods<br />
in time and adaptive multilevel finite elements in space. To be able to choose the discretization<br />
scheme in accordance to the structure <strong>of</strong> the considered PDAE, we explicitly allow for an independent<br />
discretization <strong>of</strong> state and adjoint systems. The resulting inexactness is controlled by<br />
refining grids adaptively in space and time as the optimization proceeds.<br />
We present numerical experiments for the cooling <strong>of</strong> hot glass down to room temperature,<br />
modeled by radiative heat transfer and semi-transparent boundary conditions. We consider the<br />
so called gray scale model, which is a space-time-dependent PDAE, including the highly nonlinear<br />
and nonlocal exchange <strong>of</strong> energy between glass temperature and mean radiative intensities<br />
[3]. Due to the high efficiency <strong>of</strong> the developed optimization environment it is possible to solve<br />
such complex space-time-dependent optimal control problems even on non-trivial computational<br />
domains in three spatial dimensions.<br />
[1] D. Clever, J. Lang, S. Ulbrich, and J. C. Ziems. Combination <strong>of</strong> an adaptive multilevel SQP<br />
method and a space-time adaptive PDAE solver for optimal control problems. Procedia<br />
Computer Science, 1:1429–1437, 2010.<br />
[2] D. Clever, J. Lang, S. Ulbrich, and J. C. Ziems. Generalized multilevel SQP-methods for<br />
PDAE-constrained optimization based on space-time adaptive PDAE solvers. In G. Leugering,<br />
et al., Constrained Optimization and Optimal Control for Partial Differential Equations,<br />
pages 37–60. International Series <strong>of</strong> Numerical Mathematics, Vol. 160, Basel, <strong>2012</strong>.<br />
[3] E. W. Larsen, G. Thömmes, A. Klar, M. Seaïd, and T. Götz. Simplified PN approximations to<br />
the equations <strong>of</strong> radiative heat transfer and applications. Journal <strong>of</strong> Computational Physics,<br />
183:652–675, 2002.
340 Section 19: Optimization <strong>of</strong> differential equations<br />
An optimization problem in the human knee<br />
Anton Schiela (TU Berlin), Oliver Sander (FU Berlin) Schedule<br />
Among the various difficulties in the modelling and simulation <strong>of</strong> the human knee the coupling<br />
between ligaments and bone poses particularly interesting problems. While bones can be modelled<br />
as elastic bodies, it is appropriate to model the ligaments as geometrically exact elastic<br />
rods, so called cosserat rods. The task is to derive coupling conditions that allow for a rigorous<br />
mathematical treatment and a well founded physical interpretation.<br />
Our approach is to consider the coupled problem as an energy minimization problem, in which<br />
the stored energy <strong>of</strong> both the rod and the elastic body is minimizer, subject to the equality constraints<br />
that both bodies coincide at the coupling interface. We show existence <strong>of</strong> energy minimizers<br />
for two variants <strong>of</strong> coupling conditions, and derive, under suitable assumptions, first order optimality<br />
conditions. These optimality conditions can be interpreted as force and momentum balances<br />
at the interface, and the involved Lagrangian multipliers are identified as constraint forces.<br />
Optimal Control <strong>of</strong> Transient Drift diffusion Models<br />
Pr<strong>of</strong>.Dr. Martin Burger, Marcisse Fouego (<strong>Universität</strong> Münster) Schedule<br />
In this paper We investigate the optimal control <strong>of</strong> transient drift-diffusion models for semiconductors.<br />
Our main focus is the control <strong>of</strong> the current by optimizing the applied voltage and/or<br />
the doping pr<strong>of</strong>ile, which are the natural control variables.<br />
The control problem is analyzed incluing existence, first-oder optimality and existence <strong>of</strong> adjoint<br />
variables.<br />
For the numerical simulation a simple but efficient Gummel iteration is derived . Furthermore we<br />
investigage the augmented Lagrangian method for the contraints on the control. Numerical resuls<br />
are presented for the n-p diode, in particular for the application <strong>of</strong> time-optimal switching<br />
Quantitative hybrid electrical impedance imaging<br />
Wolf Naetar (<strong>Universität</strong> Wien) Schedule<br />
In recent years, several new hybrid imaging methods which combine Electrical Impedance Tomography<br />
(which on its own is ill-posed) with other physical modalities have been proposed.<br />
We apply the Levenberg-Marquardt algorithm to a hybrid conductivity imaging problem originating<br />
from the coupling <strong>of</strong> Electrical Impedance Tomography with acoustic modalities. To be<br />
precise, we aim for estimating the spatially varying conductivity σ inside the object <strong>of</strong> interest Ω<br />
from measurements <strong>of</strong> the power density E(σ) = σ|∇u(σ)| 2 in Ω.<br />
Under the assumption <strong>of</strong> Lipschitz-stability <strong>of</strong> the linearized inverse problem, we are able to<br />
verify conditions for local convergence <strong>of</strong> the iteration method for Galerkin approximations <strong>of</strong> the<br />
problem. Moreover, we implemented the algorithm and two fast modifications, which we tested<br />
on simulated data.<br />
S19.6: Applications II Thu, 16:00–18:00<br />
Chair: Barbara Kaltenbacher S1|03–121<br />
Optimal control <strong>of</strong> multiphase induction hardening<br />
Dietmar Hömberg, Thomas Petzold (WIAS Berlin), Elisabetta Rocca (Universita’ degli studi di<br />
Milano) Schedule<br />
In my talk I investigate a new hardening process called multi-frequency induction hardening. In<br />
contrast to standard induction heating approaches it allows for a true contour hardened pattern<br />
<strong>of</strong> gears. The mathematical model consists <strong>of</strong> a vector potential equation <strong>of</strong> Maxwells equations<br />
coupled with an energy balance and rate law to describe the growth <strong>of</strong> the high temperature
Section 19: Optimization <strong>of</strong> differential equations 341<br />
phase in steel.<br />
The equations are coupled via phase dependent material parameters. In the talk I will briefly<br />
explain the model, comment on existence and uniqueness results, derive optimality conditions<br />
and conclude with some numerical simulations.<br />
Specific challenge for the numerical treatment is the resolution <strong>of</strong> the different spatial and<br />
temporal scales. To this end we employ an hp-adaptive edge element discretization <strong>of</strong> Maxwells<br />
equations and use different time scales to resolve magnetic and temperature effects, respectively.<br />
Parameter identification in the crystallization <strong>of</strong> polymers<br />
Shuai Lu (Fudan University), Yikan Liu (University <strong>of</strong> Tokyo), Xiang Xu (Michigan State University),<br />
Masahiro Yamamoto (University <strong>of</strong> Tokyo) Schedule<br />
Nucleation and growth mechanisms are the most important kinetics <strong>of</strong> the phase transformation<br />
model which arises in the crystallization <strong>of</strong> the polymer materials. In each stage, the nucleation<br />
rate and the growth rate have been the crucial coefficients describing the kinetics <strong>of</strong> the process as<br />
well as the properties <strong>of</strong> the specimens. In this talk, we will firstly revisit the time cone approach<br />
by Cahn where a hyperbolic governing equation is derived for the heterogenous nucleation rate<br />
and spatially homogeneous growth rate. As for the inverse problem, by utilizing the eigenfunction<br />
expansion method, we investigate the identification <strong>of</strong> the growth rate for an isothermal one<br />
dimension specimen. Such a problem can be seem as an inverse coefficient problem for a hyperbolic<br />
equation which is highly nonlinear with respect to the observation data. A two-step Tikhonov<br />
type regularization method is proposed to reconstruct the growth rate provided with the final<br />
noisy observation data. Numerical prototype examples are presented to illustrate the validity and<br />
effectiveness <strong>of</strong> the proposed scheme.<br />
An optimal control problem in polyconvex elasticity<br />
Lars Lubkoll, Anton Schiela, Martin Weiser, Stefan Zachow (Zuse Institut Berlin) Schedule<br />
Congenital malformations or trauma-related defects <strong>of</strong> facial bones are <strong>of</strong>ten corrected by patientspecific<br />
implants to substitute or complement bone structures. As the implant’s shape and position<br />
affect the s<strong>of</strong>t tissue and hence the visual appearance <strong>of</strong> the patient, the prediction <strong>of</strong> implant<br />
formation and placement are <strong>of</strong> utmost importance for the final outcome <strong>of</strong> rehabilitative facial<br />
surgery. Currently the shape <strong>of</strong> an implant is customized individually during the operation, which<br />
is a tedious and time consuming process. A preoperative design <strong>of</strong> implants using CAD methods<br />
has the potential to shorten operation time and to open new perspectives regarding education <strong>of</strong><br />
surgeons, surgical planning and the verification procedure.<br />
From a mathematical point <strong>of</strong> view the task <strong>of</strong> finding an optimal implant shape, such that a<br />
desired result is achieved, can be formulated as an optimal control problem <strong>of</strong> the form<br />
min J(u, g) s.t. u ∈ Ig(v)<br />
v∈Uad<br />
where u is the resulting displacement <strong>of</strong> the material and the sequentially weakly lower semicontinuous<br />
cost functional J measures the deviation from the desired result. Ig is an elastic<br />
energy functional associated with the boundary force g and a compressible, polyconvex stored<br />
energy function in the sense <strong>of</strong> [1]. For this inverse problem, we give an existence result using the<br />
direct method <strong>of</strong> the calculus <strong>of</strong> variations, discuss the occuring lack <strong>of</strong> regularity and difficulties<br />
in the derivation <strong>of</strong> necessary optimality conditions as well as implications on the numerical<br />
solution process. Finally we give some numerical examples for the case that Ig is associated with<br />
a compressible Mooney-Rivlin material.
342 Section 19: Optimization <strong>of</strong> differential equations<br />
[1] J.M. Ball, Convexity Conditions and Existence Theorems in Nonlinear Elasticity, Arch. Rat.<br />
Mesh. Anal. 63 (1977), 337–403<br />
Shape Optimization for an Interface Problem in (linear) Elasticity for distortion<br />
compensation<br />
Kevin Sturm, Dietmar Hömberg (WIAS Berlin), Michael Hintermüller (Humboldt <strong>Universität</strong>)<br />
Schedule<br />
In this talk I will introduce a sharp interface model describing a workpiece made <strong>of</strong> steel. In<br />
the heat treatment <strong>of</strong> steel different phases e.g. martensite and pearlite can be produced in the<br />
workpiece. The goal <strong>of</strong> my work is to obtain a desired workpiece shape by controlling the final<br />
phase distribution. Therefore our control variables are sets and thus we have to consider a shape<br />
optimization problem. I will show how one can derive the shape derivative for this problem,<br />
which then can be used to solve the shape optimization problem. Moreover, numerical results for<br />
different workpiece shapes in two dimensions will be presented.<br />
Dynamic PET Reconstruction based on aReaction-Diffusion Model<br />
Louise Reips, Ralf Engbers, Martin Burger (<strong>Universität</strong> Münster) Schedule<br />
PET is an imaging technique applied in nuclear medicine able to produce images <strong>of</strong> physiological<br />
processes in 2D or 3D. The use <strong>of</strong> 18F-FDG PET is now a widely established method to quantify<br />
tumour metabolism, but other investigations based on different tracers are still far from clinical<br />
use, although they <strong>of</strong>fer great opportunities such as radioactive water as a marker <strong>of</strong> cardiac<br />
perfusion. A major obstacle is the need for dynamic image reconstruction from low quality data,<br />
which applies in particular for tracers with fast decay like H 15<br />
2 O.<br />
Here we present a model-based approach to overcome those difficulties. We derive a set <strong>of</strong><br />
differential equations able to represent the kinetic behavior <strong>of</strong> H 15<br />
2 O PET tracers during cardiac<br />
perfusion. In this model one takes into account the exchange <strong>of</strong> materials between artery, tissue<br />
and vein which predicts the tracer activity if the reaction rates, velocities, and diffusion coefficients<br />
are known. One then interpretes, the computation <strong>of</strong> these distributed parameters as a nonlinear<br />
inverse problem, which we solve using variational regularization approaches. For the minimization<br />
we use the gradient-based methods and Forward-Backward Splitting.<br />
The main advantage is the reduction <strong>of</strong> the degrees <strong>of</strong> freedom, which makes the problem<br />
overdetermined and thus allows to proceed to low quality data. Instead <strong>of</strong> reconstructing the<br />
4D tracer activity distribution (in space and time) we identify a set <strong>of</strong> 3D parameters (spatially<br />
dependent only).<br />
[1] M. Benning, T. Kösters, F. Wübbeling, K. P. Schäfers, and M. Burger. A nonlinear variational<br />
method for improved quantification <strong>of</strong> myocardial blood flow using dynamic H15 2 O PET,<br />
IEEE Nuclear Science Symposium Conference Record, (2008), 4472–4477.<br />
[2] M. E. Kamasak, C. A. Bouman, E. D. Morris, and K. Sauer, Direct Reconstruction <strong>of</strong> Kinetic<br />
Parameter Images from Dynamic PET Data, IEEE Transactions on Medical Imaging,<br />
24(2005), 636-650.<br />
[3] M. N. Wernick and J. N. Aarsvold. Emission Tomography: The Fundamentals <strong>of</strong> PET and<br />
SPECT. Elsevier Academic Press, 2004.
Section 20: Dynamics and control 343<br />
Section 20: Dynamics and control<br />
Organizers: Knut Graichen (<strong>Universität</strong> Ulm), Stephan Trenn (<strong>Universität</strong> Kaiserslautern)<br />
S20.1: Differential algebraic equations and applications Tue, 13:30–15:30<br />
Chair: Stephan Trenn, Knut Graichen S1|01–A4<br />
Positivity preserving simulation <strong>of</strong> Differential-Algebraic Equations<br />
Ann-Kristin Baum (TU Berlin) Schedule<br />
Positive dynamical systems arise in every application in which the considered variables represent<br />
a material quantity that does not take negative values, like e.g. the concentration <strong>of</strong> chemical and<br />
biological species or the amount <strong>of</strong> goods and individuals in economic and social sciences. Beside<br />
positivity, the dynamics are <strong>of</strong>ten subject to constraints resulting from limitation <strong>of</strong> resources,<br />
conservation or balance laws, which extend the differential system by additional algebraic equations.<br />
In order to obtain a physically meaningful simulation <strong>of</strong> such processes, both properties, the<br />
positivity and the constraints, should be reflected in the numerical solution. In this talk, we discuss<br />
these issues for linear time-varying systems, as they arise for example in the linearization <strong>of</strong><br />
non-linear systems in chemical reaction kinetics or process engineering. We first consider index-1<br />
problems, in which the differential and algebraic equations are explicitly given and explain under<br />
which conditions we can expect a positive numerical approximation that meets the algebraic<br />
constraints. We extend these results to higher index problems, i.e., problems in which some <strong>of</strong> the<br />
algebraic equations are hidden in the system, by a positivity preserving index reduction. This is a<br />
remodeling procedure which filters out these hidden constraints without destroying the positivity<br />
property and thus admits to trace back these systems to the index-1 case.<br />
Normal forms for DAEs and tracking control<br />
Achim Ilchmann, Thomas Berger (TU Ilmenau), Timo Reis (<strong>Universität</strong> Hamburg) Schedule<br />
As a counterpart to the Byrnes-Isidori form for linear time-invariant ODEs, we derive a normal<br />
form (“almost a canonical form”) for linear time-invariant DAEs whose transfer function<br />
C(sE − A) −1 B has either positive strict relative degree or has proper inverse. These forms are<br />
exploited to investigate the zero dynamics <strong>of</strong> the system and to show that funnel control <strong>of</strong> a<br />
rather large class <strong>of</strong> tracking signals is feasible.<br />
Regularization <strong>of</strong> descriptor systems in behaviour form<br />
S. L. Campbell (North Carolina State University), P. Kunkel (<strong>Universität</strong> Leipzig), V. Mehrmann<br />
(TU Berlin) Schedule<br />
Differential-algebraic equations (DAEs) present today the state-<strong>of</strong>-the-art in dynamical systems<br />
arising from automated modularized modeling in almost all areas <strong>of</strong> science and engineering.<br />
While the modeling becomes more and more convenient, the resulting models are typically not<br />
easy to treat with current numerical simulation, control and optimization methods. In many cases<br />
a reformulation <strong>of</strong> the models or even a regularization is necessary to avoid failure <strong>of</strong> the<br />
computational methods. We will discuss general DAE control problems and how they can be<br />
systematically reformulated and regularized so that the resulting system can be used in control<br />
and optimization procedures without much further difficulties.<br />
Self-Adjoint Differential-Algebraic Equations arising in Linear-Quadratic Optimal<br />
Control Problems<br />
Lena Scholz (TU Berlin) Schedule
344 Section 20: Dynamics and control<br />
Motivated from the linear-quadratic optimal control problem for differential-algebraic equations<br />
(DAEs) given in the form<br />
minimize<br />
1<br />
2 x(t)T Mex(t) + 1<br />
2<br />
� t<br />
subject to E ˙x = Ax + Bu + f, x(t) = x ∈ R n ,<br />
t<br />
� x T W x + x T Su + u T S T x + u T Ru � dt<br />
we study the functional analytic properties <strong>of</strong> the operator associated with the necessary optimality<br />
boundary value problem and show that it is associated with a self-conjugate operator and<br />
a self-adjoint pair <strong>of</strong> matrix functions. If we denote the differential-algebraic equation associated<br />
with the necessary optimality boundary value problem by<br />
E ˙z = Az + ˜ f,<br />
then the pair (E, A) has the property that E T = −E and A T = A + ˙<br />
E.<br />
We analyze the structure <strong>of</strong> the resulting self-adjoint pair <strong>of</strong> matrix functions and <strong>of</strong> the associated<br />
boundary value problem via condensed forms under orthogonal congruence transformations<br />
that preserve the self-adjoint structure. Based on these condensed forms we can characterize the<br />
consistency <strong>of</strong> boundary values, as well as the consistency and smoothness requirements for the<br />
inhomogeneities, and thus derive altogether the conditions for unique solvability <strong>of</strong> the system.<br />
Further, we show that the underlying ordinary differential equation <strong>of</strong> a differential-algebraic system<br />
associated with a self-adjoint pair <strong>of</strong> matrix functions is a Hamiltonian system and generates<br />
a symplectic flow. For self-adjoint DAEs with symplectic flow a global condensed form is derived<br />
and, furthermore, we discuss the structure preserving construction <strong>of</strong> the symplectic flow from<br />
derivative arrays.<br />
This is a joint work with Volker Mehrmann (TU Berlin) and Peter Kunkel (<strong>Universität</strong> Leipzig).<br />
A projection method for the solution <strong>of</strong> large-scale Lur’e equations<br />
Federico Poloni (TU Berlin), Timo Reis (<strong>Universität</strong> Hamburg) Schedule<br />
The Lur’e equations<br />
A ∗ X + XA + Q =K ∗ K,<br />
XB + C =K ∗ L,<br />
R =L ∗ L,<br />
to be solved for a Hermitian n × n X, and K, L with as few columns as possible, arise in optimal<br />
control and in model reduction. Typically, the system is reduced to an algebraic Riccati equation<br />
by inverting R, but this is not a viable approach when R is singular, which is <strong>of</strong>ten a structural<br />
property.<br />
In this work, we present a numerical method for their solution which works when R is singular<br />
and is suitable to provide approximate low-rank factored solution in the large and sparse case.<br />
We compute the even invariant subspace <strong>of</strong> the associate even matrix pencil (as per the theory<br />
<strong>of</strong> [Reis, Lur’e equations and even matrix pencils, LAA 2011]) relative to the singular and infinite<br />
Kronecker blocks, and use it to deflate the Lur’e equations to a smaller version with nonsingular<br />
R. The whole procedure has to be carried out implicitly in order to be able to exploit the sparsity<br />
properties <strong>of</strong> A, and thus we have to deal with implicit representations <strong>of</strong> these coefficients in<br />
terms <strong>of</strong> invariant subspace projectors. We show that the Newton-ADI method [Benner, Li, Penzl,
Section 20: Dynamics and control 345<br />
Numerical solution <strong>of</strong> large-scale Lyapunov equations, Riccati equations, and linear-quadratic optimal<br />
control problems, NLAA 2008] [LYAPACK library, http://bit.ly/vnHgUh] can be applied<br />
to this projected Riccati equation in implicit form, and that an extended matrix approach can be<br />
used to provide an efficient solver for the linear systems that appear in the ADI iteration.<br />
Reduced Order State Space Modeling <strong>of</strong> Piezo-Mechanical Systems<br />
Jens Saak, Peter Benner , Mohammed Monir Uddin (MPI Magdeburg), Burkhard Kranz (Fraunh<strong>of</strong>er<br />
IWU Dresden) Schedule<br />
We are investigating the fine positioning <strong>of</strong> a spindle head structure in machine tool control [1].<br />
The tool center point (tcp) is steered by a redundant axis model allowing to distribute large scale<br />
head movements to the structure mounting and small scale positioning <strong>of</strong> the tcp to a set <strong>of</strong> piezo<br />
actuators. The special focus in this contribution lies on the structural model <strong>of</strong> the spindle head<br />
with the piezo actuators included. The large scale movements are realized by mounting the device<br />
to the surrounding machine tool. They are thus not contained in our model. The finite element<br />
(FEM) discretization <strong>of</strong> the structural CAD model leads to a very large second order model <strong>of</strong><br />
the form<br />
M ¨x(t) + E ˙x(t) + Kx(t) = Bu(t), y(t) = Cx(t) + Du(t). (1)<br />
Due to the modeling <strong>of</strong> the piezo actuation the M and E matrices are singular, but the part in K<br />
corresponding to the joint null-space <strong>of</strong> M and E is invertible and thus the differential algebraic<br />
equation is <strong>of</strong> index 1.<br />
The FEM model is much to large to be feasible for fast simulation and controller design. We<br />
seek to replace it by a reduced order surrogate model. We concentrate on the derivation <strong>of</strong> the<br />
first order standard state space model required in the following steps <strong>of</strong> the controller design.<br />
We tackle this equation by an S-LRCF-ADI [2] based balanced truncation approach. To this<br />
end we reformulate (1) in first order form, exploiting that in our case we additionally have that<br />
C = B T and M, E and K are symmetric. This allows us to reduce the amount <strong>of</strong> necessary<br />
computations in the balancing even further, since the two system Gramians coincide.<br />
[1] Neugebauer, R., Drossel, W.G., Bucht, A., Kranz, B., Pagel, K.: Control design and experimental<br />
validation <strong>of</strong> an adaptive spindle support for enhanced cutting processes. CIRP<br />
Annals - Manufacturing Technology 59(1), 373–376 (2010). http://www.sciencedirect.<br />
com/science/article/pii/S0007850610000302<br />
[2] Freitas, F., Rommes, J., Martins, N.: Gramian-based reduction method applied to large sparse<br />
power system descriptor models. IEEE Transactions on Power Systems 23(3), 1258–1270<br />
(2008)<br />
S20.2: Mechatronics Tue, 16:00–18:00<br />
Chair: Knut Graichen, Stephan Trenn S1|01–A4<br />
On Measuring Vibration <strong>of</strong> Cutting-Off Machines with Endless Bandsaw Based on<br />
Zigbee Technique<br />
Józef Wojnarowski, Wladysław Kaliński (Silesian University <strong>of</strong> Technology Gliwice), Bohdan Borowik<br />
(University <strong>of</strong> Bielsko-Biala) Schedule<br />
As has been found, the dominants in the spectra <strong>of</strong> the acceleration <strong>of</strong> vibrations are most affected<br />
by the tooth pitch <strong>of</strong> the saw, its rate <strong>of</strong> travel and the value <strong>of</strong> the force <strong>of</strong> pressure exerted on<br />
the cut object, which value is adjusted by hand (1). If the feed is to large, the frequencies <strong>of</strong> the
346 Section 20: Dynamics and control<br />
dominants decrease due to the reaction <strong>of</strong> the asynchronous motor: in many cases there occur<br />
vibrations characterized by beats. While analyzing the presented spectra it has been found that<br />
they include components with a characteristic frequency for the determined scale on teeth and<br />
the speed <strong>of</strong> their shift along the object or pack <strong>of</strong> objects which is be cut. These values depend<br />
on the pressure <strong>of</strong> the saw on the object, i.e. on the feed. Knowing the admissible feed <strong>of</strong> the saw<br />
in relation to one tooth, this fact may be utilized in the development <strong>of</strong> the system <strong>of</strong> automatic<br />
control <strong>of</strong> the feed <strong>of</strong> saws operating under differing conditions. For measuring and monitoring<br />
vibration we proposed wireless network based on ZigBee technique such, that sensor with end<br />
device node is attached to moving element <strong>of</strong> the machine and sensor reading are sent over the air<br />
to remote coordinator node. ZigBee module with inherent firmware provides a wireless personal<br />
area networking PAN <strong>of</strong> data from the sensor to microcontroller dsPIC33FJ256. The base <strong>of</strong><br />
Zigbee hybrid module is IC ZDMAI128-B0. It provides point-to-point communication. As our<br />
investigation show, PIC24 microcontroller appears suitable in monitoring vibration <strong>of</strong> dynamic<br />
mechanical object.<br />
[1] Wojnarowski J. et al., The restriction <strong>of</strong> vibrations <strong>of</strong> cutting-<strong>of</strong>f machines with endless<br />
bandsaws. Monograph. SP Department <strong>of</strong> Applied Mechanics, Silesian Technical University,<br />
Gliwice 2007, pp. 392. (In Polish).<br />
jozef.wojnarowski@polsl.pl<br />
LQR Control for Vibration Suppression <strong>of</strong> Piezoelectric Integrated Smart Structures<br />
Shun-Qi Zhang, Rüdiger Schmidt (RWTH Aachen) Schedule<br />
In the present paper, a motion equation <strong>of</strong> piezoelectric integrated beams has been derived by<br />
using Hamiltons principle and the finite element method based on the First-Order Shear Deformation<br />
(FOSD) theory. Then, for control design a state space model is constructed from the motion<br />
equation. Linear Quadratic Regulator (LQR) control has been implemented on the mathematical<br />
model <strong>of</strong> a piezoelectric bonded beam for vibration suppression. Finally, a numerical application<br />
has been performed to testify the applicability and effectiveness <strong>of</strong> present method.<br />
Force Control <strong>of</strong> a 6DoF parallel Platform driven by Fluidic Muscles<br />
C.Michael, A. Kecskemethy (<strong>Universität</strong> Duisburg-Essen) Schedule<br />
Described in this paper is a force control scheme for a six-legged parallel platform driven by hybrid<br />
actuators. Each leg <strong>of</strong> type RRPS is equipped with a fluidic muscle and a coaxial linear spring<br />
providing push and pull forces. Fluidic muscles require that the gas model as well as the nonlinear<br />
pressure stroke force relation is included in the control scheme. In addition, the dynamics <strong>of</strong> the<br />
proportional control valve needs to be taken into account.<br />
The presented model based force control scheme computes the target pressure for the desired<br />
force by evaluating a polynomial in the actual position and pressure. Computation <strong>of</strong> the control<br />
input u requires the generation <strong>of</strong> set-points for the pressure change ˙p. Two different approaches<br />
are presented. First a backward difference method with prescribed time to target pressure is illustrated.<br />
The second approach evaluates the compliance <strong>of</strong> the close loop <strong>of</strong> the actuator with<br />
the environment.<br />
End-Effector Trajectory Tracking <strong>of</strong> Serial Flexible Manipulators<br />
Robert Seifried, Mark Wörner, Thomas Gorius (<strong>Universität</strong> Stuttgart) Schedule<br />
Modern light weight manipulator designs result in low energy consumption and allow <strong>of</strong>ten high<br />
working speeds. However, due to the light weight design the bodies have a significant flexibility<br />
which yields undesired vibrations. In the control design these flexibilities must be taken into
Section 20: Dynamics and control 347<br />
account, yielding a flexible multibody system. In order to obtain a good performance in endeffector<br />
trajectory tracking <strong>of</strong> flexible manipulators an accurate and efficient feedforward control<br />
is very helpful. This is then supplemented by additional feedback control to account for small<br />
disturbances and uncertainties.<br />
In this contribution feedforward control design based on model inversion is presented and<br />
applied to a serial manipulator with two flexible arms. Thereby, for a given system output the<br />
inverse model provides the control input for exact output reproduction. In addition the inverse<br />
model provides the trajectories for all generalized coordinates, which can be used in additional<br />
feedback control. The derived inverse model consists <strong>of</strong> a chain <strong>of</strong> differentiators, driven internal<br />
dynamics and an algebraic part. For flexible manipulators in end-effector trajectory tracking<br />
the internal dynamics is in most cases unbounded. This requires stable inversion by solution <strong>of</strong><br />
a boundary value problem. The accuracy <strong>of</strong> the feedforward control depends on the number <strong>of</strong><br />
modes used in flexible multibody system model, and is investigated in detail by simulation. As<br />
feedback strategy a combination <strong>of</strong> PID control for the joint coordinates and curvature feedback<br />
is used as first approach. Further, the obtained results from the model inversion can be used in a<br />
passivity based robust control schema.<br />
Fault detection, diagnosis, and reconfiguration <strong>of</strong> planetary rovers<br />
Alexandre Carvalho Leite, Bernd Schäfer (DLR), Marcelo Lopes de Oliveira e Souza (National<br />
Institute for Space Research - Brazil) Schedule<br />
This work describes the theoretic development <strong>of</strong> new FDDR (Fault Detection, Diagnosis, and<br />
Reconfiguration) methods and a path following control simulation which illustrates the application<br />
<strong>of</strong> these methods in an ExoMars-type rover. Planetary exploration rovers are wheeled vehicles<br />
devoted to provide mobility in hostile extraterrestrial environment. An imperative characteristic<br />
<strong>of</strong> such vehicles is fault tolerance, because maintenance in case <strong>of</strong> severe failures is not yet a practicable<br />
option. To employ fault tolerance we propose new FDDR methods coping with robustness in<br />
fault detection and safe decision to reconfigure the control system based on inconclusive diagnosis<br />
statements. The new methods are tw<strong>of</strong>old: 1) a variable threshold based on adaptive filtering is<br />
applied; 2) a multi-objective decision maker is used acting between multiple diagnosis statement<br />
and reconfiguration switching, called Dilemma Diagnoser. A fault tolerant control system has been<br />
designed and applied to the European Space Agencys ExoMars rover B2X2 simulation model: it<br />
is motorized by six independently steerable wheels mounted on a passive suspension for all-terrain<br />
locomotion. A multi-body simulation model describes the rigid mechanical structure and interacts<br />
with the environment (stones, bedrocks, and sandy terrain) through a detailed contact model.<br />
Realistic and important terrain features like multi-pass effects in deformable terrain and multiple<br />
contacts with complexly shaped stones are taken into account for modeling and simulation <strong>of</strong><br />
the overall dynamics behaviour. The simulation cases are to be tested in our planetary testbed<br />
with the breadboard model <strong>of</strong> the B2X2 ExoMars rover. Some experiments were carried out to<br />
correlate our contact model against experimental data; additional tests are planned to further<br />
model tuning and experimentation <strong>of</strong> the simulated FDDR scheme.<br />
S20.3: Controller design and MPC Wed, 13:30–15:30<br />
Chair: Knut Graichen, Stephan Trenn S1|01–A4<br />
Model predictive control for optimal invariance problems<br />
Lars Grüne (<strong>Universität</strong> Bayreuth) Schedule<br />
We consider the problem <strong>of</strong> keeping the state <strong>of</strong> a nonlinear discrete time control system within<br />
a prespecified admissible set with minimal control effort. We use a model predictive control ap-
348 Section 20: Dynamics and control<br />
proach without terminal constraints in order to obtain a feedback law for this task. We prove<br />
that under appropriate controllability conditions this approach yields near optimal performance<br />
with the gap to optimality tending to zero for increasing prediction horizon. Several numerical<br />
simulations illustrate our theoretical result.<br />
Computationally efficient receding horizon tracking control applied to a tubular reactor<br />
example<br />
Tilman Utz, Knut Graichen (<strong>Universität</strong> Ulm) Schedule<br />
Receding horizon control (or model predictive control) relies on the repeated solution <strong>of</strong> an optimal<br />
control problem over a prediction horizon and is widely considered as a powerful design<br />
method for feedback control, in particular if constrained nonlinear dynamical systems are concerned.<br />
Besides the classical stabilization task, the control <strong>of</strong> transient processes such as setpoint<br />
transitions, is <strong>of</strong>ten carried out using a suitable (model-based) feedforward controller. If the system<br />
under consideration is unstable or in order to account for model uncertainties and disturbances,<br />
the feedforward control has to be amended by a trajectory tracking controller that stabilizes the<br />
tracking error.<br />
This contribution focuses on the combination <strong>of</strong> feedforward control with a receding horizon<br />
tracking controller in the context <strong>of</strong> the well-known two-degrees-<strong>of</strong>-freedom control scheme. The<br />
receding horizon controller is based on the tracking error dynamics in order to stabilize the system<br />
along the nominal trajectory <strong>of</strong> the feedforward part. However, the error dynamics are in general<br />
nonlinear and time-varying. A linear (but still time-varying) error dynamics can be obtained by<br />
linearizing the system along the nominal trajectories, which leads to a linear-quadratic optimal<br />
control problem for the receding horizon controller.<br />
The two tracking control schemes based on the nonlinear and linearized time-varying error<br />
dynamics are evaluated for transitions between unstable setpoints <strong>of</strong> a tubular reactor example.<br />
An early lumping approach is used to reduce the parabolic partial differential equation to a<br />
nonlinear finite-dimensional system. This system constitutes a suitable test case, since on the one<br />
hand high-dimensional discretizations have to be chosen in order to capture the relevant dynamics<br />
<strong>of</strong> the system, whereas on the other hand the optimization has to be completed in a short period<br />
<strong>of</strong> time in order to stabilize the system.<br />
Multi-Agent Motion Control <strong>of</strong> Autonomous Vehicles in Three-Dimensional Fluid<br />
Flow Fields<br />
Axel Hackbarth, Edwin Kreuzer (TU Hamburg) Schedule<br />
Motion control <strong>of</strong> multiple autonomous vehicles is necessary to assure safe interaction <strong>of</strong> agents<br />
operating in the same environment. Under the influence <strong>of</strong> fluid flow the control strategy for the<br />
agents has to adapt to the forces acting upon the vehicles.<br />
A potential-field based algorithm for multi-agent control has been extended to account for<br />
correct guidance under the influence <strong>of</strong> flow. Path following and collision avoidance are the main<br />
objectives for the control algorithm which is developed for an underwater sensor network. An<br />
approximation <strong>of</strong> the flow is used for the path planning with model predictive control, whereas<br />
path following is assured through sliding mode control.<br />
The controller has yet been tested in simulations only, but experiments are planned with a<br />
swarm <strong>of</strong> five to ten micro submarines in a water tank with natural and forced convection. The<br />
fluid field in the simulation originates from a CFD analysis <strong>of</strong> the water tank under steady flow<br />
conditions where the impact <strong>of</strong> the vehicles has been neglected.
Section 20: Dynamics and control 349<br />
Optimal Control on Stable Manifolds for a Double Pendulum<br />
Kathrin Flaßkamp, Julia Timmermann (<strong>Universität</strong> Paderborn), Sina Ober-Blöbaum (TU München/<strong>Universität</strong><br />
Paderborn), Michael Dellnitz and Ansgar Trächtler (<strong>Universität</strong> Paderborn)<br />
Schedule<br />
Optimal control problems for mechanical systems <strong>of</strong>ten arise in technical applications, e.g. in the<br />
computation <strong>of</strong> energy efficient or time optimal steering maneuvers between operation points. To<br />
find solutions with minimal control effort, the system’s natural, i.e. uncontrolled dynamics should<br />
be used whenever appropriate. Promising candidates to consider for energy efficient trajectories<br />
are the highly dynamic, but uncontrolled motions on (un)stable manifolds <strong>of</strong> equilibria.<br />
In this contribution, we propose a control strategy for mechanical systems that includes uncontrolled<br />
trajectories on (un)stable manifolds in a sequence together with short control maneuvers<br />
to design a feedforward control. In particular, we present optimal swing-up solutions for a double<br />
pendulum that are based on trajectories on the stable manifold <strong>of</strong> the pendulum’s upper<br />
equilibrium. Approximations <strong>of</strong> the manifolds are computed by the s<strong>of</strong>tware tool GAIO (Global<br />
Analysis <strong>of</strong> Invariant Objects). For the numerical solution <strong>of</strong> the optimal control problems we use<br />
the method DMOC (Discrete Mechanics and Optimal Control). To demonstrate the advantages<br />
<strong>of</strong> our approach compared to a black box optimization, we perform a post optimization with the<br />
optimal control sequence as an initial guess. The numerical results are evaluated in a simulation<br />
environment for the double pendulum.<br />
The Bang-Bang Funnel Controller: An experimental verification<br />
Christoph Hackl (TU München), Stephan Trenn (TU Kaiserslautern) Schedule<br />
We adjust the newly developed bang-bang funnel controller [1] such that it is more applicable<br />
for real world scenarios. The main idea is to introduce a third “neutral” input value to account<br />
for the situation when the error is already small enough and no control action is necessary. We<br />
present simulation and experimental results which show the advantage to the bang-bang funnel<br />
controller with only two input values. Finally, we compare the experimental results with the one<br />
obtained by the application <strong>of</strong> the continuous funnel controller as reported in [2].<br />
[1] Daniel Liberzon and Stephan Trenn. The bang-bang funnel controller. In Proc. 49th IEEE<br />
Conf. Decis. Control, Atlanta, USA, pages 690695, 2010.<br />
[2] Christoph M. Hackl, Norman Hopfe, Achim Ilchmann, Markus Mueller, and Stephan Trenn.<br />
Funnel control for systems with relative degree two. Submitted for publication, preprint<br />
available from the websites <strong>of</strong> the authors, 2010.<br />
Approximately linear tracking control <strong>of</strong> nonlinear systems<br />
Klaus Röbenack, Fabian Paschke (TU Dresden) Schedule<br />
An elegant approach to control nonlinear state-space systems is the exact input-to-state linearization,<br />
where a nonlinear change <strong>of</strong> coordinates combined with a nonlinear feedback law yields<br />
a linear controllable system [1]. In this contribution, we treat the single-input case, where inputto-state<br />
linearizability is equivalent to flatness. Sufficient and necessary existence conditions are<br />
well-known, but quite restrictive.<br />
Although the flat output can be guessed in many practical applications, the formal computation<br />
is complicated due to the required symbolic solution <strong>of</strong> a system <strong>of</strong> partial differential<br />
equations resulting from Frobenius’ theorem. We propose the design <strong>of</strong> a tracking controller for<br />
flat single-input systems, where the explicit knowledge <strong>of</strong> the flat output is not required. Our
350 Section 20: Dynamics and control<br />
approach is based on a series expansion <strong>of</strong> the tracking error along a given reference trajectory.<br />
For point-to-point control, the desired reference trajectory can be obtained numerically solving<br />
a boundary value problem [2]. For a first order approximation, our method coincides with the<br />
linear time-varying controller suggested by Föllinger [3], where the linearization <strong>of</strong> the nonlinear<br />
system is carried out along the reference trajectory. In this case, the controller is in some sense<br />
dual to the extended Luenberger observer developed by Zeitz [4]. Nevertheless, our approach can<br />
also be modified for zeroth as well as high order approximations.<br />
[1] A. Isidori. Nonlinear Control Systems: An Introduction. Springer-Verlag, London, 3rd edition,<br />
1995.<br />
[2] K. Graichen, V. Hagenmeyer, and M. Zeitz. A new approach to inversion-based feedforward<br />
control design for nonlinear systems. Automatica, 41(12):2033–2041, 2005.<br />
[3] O. Föllinger. Entwurf zeitvarianter Systeme durch Polvorgabe. Regelungstechnik, 26(6):189–<br />
196, 1978.<br />
[4] M. Zeitz. The extended Luenberger observer for nonlinear systems. Systems & Control<br />
Letters, 9:149–156, 1987.<br />
S20.4: Control theory Wed, 16:00–18:00<br />
Chair: Stephan Trenn, Knut Graichen S1|01–A4<br />
Some remarks concerning differential flatness and tangent systems.<br />
Matthias Franke (Fraunh<strong>of</strong>er IIS, Design Automation Division), Klaus Röbenack (TU Dresden)<br />
Schedule<br />
We consider control systems governed by ˙x = f(x) + �m i=1 gi(x)ui . A possible way <strong>of</strong> calculating<br />
a flat output yi , i = 1, .., m <strong>of</strong> such a system is as follows, see [1]. Assuming the tangent system<br />
�<br />
∂f<br />
d ˙x =<br />
∂x +<br />
m� ∂gi<br />
∂x ui<br />
�<br />
m�<br />
dx + gidu i .<br />
i=1<br />
is controllable, we can directly determine a flat output ω = (ωi )i=1,..,m <strong>of</strong> this linear time-varying<br />
system. If ω satisfies an integrability condition, the flat output y <strong>of</strong> the nonlinear system can be<br />
calculated by integration <strong>of</strong> dyi = �m j=1 µijω j (possibly with an integrating factor µ i j). In contrast<br />
to [1], where a generalized version <strong>of</strong> the moving frame structure equations is used for checking<br />
integrability, an adapted version <strong>of</strong> the Frobenius theorem is employed here. We investigate two<br />
special cases.<br />
For systems with one input, the integrability condition reads as dω1 ∧ ω1 = 0, where ω1 can<br />
be taken as the last row <strong>of</strong> the inverse <strong>of</strong> the local controllability matrix. This condition is a dual<br />
version <strong>of</strong> the well known involutivity condition (see for example [3]). For systems with m + 1<br />
states and m inputs, there are ω depending on the state x only, i.e.<br />
ω i =<br />
m+1 �<br />
j=1<br />
ω i j(x)dx j ,<br />
provided that the tangent linear system is controllable. In this case, the integrability conditions<br />
dω i ∧ ω 1 ∧ · · · ∧ ω m = 0, i = 1, . . . , m are always fulfilled. This result can be found (derived<br />
differently) in [3], cf. also [4].<br />
i=1
Section 20: Dynamics and control 351<br />
[1] J. Lévine, Analysis and Control <strong>of</strong> Nonlinear Systems: A Flatness-based Approach (Springer,<br />
Berlin, 2009).<br />
[2] P. Martin, A geometric sufficient condition for flatness <strong>of</strong> systems with m inputs and m + 1<br />
states, Proc. 32nd CDC (1993), 3431 – 3436.<br />
[3] R. Su, On the linear equivalents <strong>of</strong> nonlinear systems, Systems & Control Letters 2 (1982),<br />
48–52.<br />
[4] K. Schlacher and M. Schöberl, Construction <strong>of</strong> flat outputs by reduction and elimination,<br />
Proc. 7th NOLCOS (2007).<br />
Orbital stabilization <strong>of</strong> a class <strong>of</strong> underactuated mechanical systems<br />
Carsten Knoll, Klaus Röbenack (TU Dresden) Schedule<br />
Typically, the aim <strong>of</strong> a controller applied to a mechanical system with an unstable equilibrium<br />
is to alter the system dynamics such that the equilibrium becomes stable. Another possibility,<br />
however, would be to design the controller such that the closed loop system has a stable limit<br />
cycle with the considered equilibrium as center. Even if the controller is designed to stabilize the<br />
equilibrium, limit cycles may occur in mechanical control systems due to discontinuous effects<br />
such as backlash or dry friction. Explicitly imposing a stable limit cycle by a suited controller,<br />
in contrast, would at least allow to influence directly properties such as frequency and amplitude<br />
<strong>of</strong> the resulting oscillation. Moreover, other applications <strong>of</strong> orbital stabilization are possible, e.g.<br />
in the field <strong>of</strong> parameter identification and adaptive controllers where conditions for persistent<br />
excitation have to be fulfilled.<br />
In this contribution we consider underactuated mechanical systems whose linearization about<br />
the equilibrium is stabilizable and has at least a controllable subspace <strong>of</strong> dimension two. We design<br />
the feedback in two steps: A linear feedback ensures that the linearization <strong>of</strong> the resulting<br />
system has exactly one pair <strong>of</strong> eigenvalues on the imaginary axis, while the rest is located in the<br />
left half-plane. Then, an additional nonlinear feedback basing on a suited bilinear form renders<br />
one closed orbit asymptotically stable. As an illustrative example we consider the well known ball<br />
and beam benchmark system.<br />
Passivity based stabilization <strong>of</strong> mechanical systems with dissipation in unactuated<br />
degrees <strong>of</strong> freedom<br />
Paul Kotyczka, Sergio Delgado L. (TU München) Schedule<br />
Passivity based techniques allow a systematic nonlinear controller design using physically inspired<br />
energetic arguments. The method Interconnection and Damping Assignment Passivity Based Control<br />
(IDA-PBC) is one approach to solve the stabilization problem for underactuated mechanical<br />
systems [1]. IDA-PBC aims at finding a state feedback control law such that the closed loop dynamics<br />
is represented as a Port-Hamiltonian (PH) system with the desired properties positive definiteness<br />
<strong>of</strong> the virtual energy function (around an equilibrium (q ∗ , 0)) and a positive semi-definite<br />
damping structure such that the closed loop energy is non-increasing along the system trajectories.<br />
PH systems generalize the Hamiltonian formulation <strong>of</strong> dynamical systems, known from mechanics.<br />
In its common version for (underactuated) mechanical systems IDA-PBC requires the closed loop<br />
system to have simple mechanical structure, i. e. the closed loop energy to be a sum <strong>of</strong> potential<br />
plus kinetic energy. It is known that the presence <strong>of</strong> physical damping in unactuated degrees<br />
<strong>of</strong> freedom can impede the closed loop energy and the dissipation matrix to be positive (semi-)<br />
definite at the same time [2].
352 Section 20: Dynamics and control<br />
The present contribution proposes a possibility to overcome this dissipation obstacle in the<br />
application <strong>of</strong> IDA-PBC by adding a cross term between coordinates and momenta to the closed<br />
loop energy. A solution is derived for the 2 DOF Acrobot system with physical damping. Stability<br />
<strong>of</strong> the equilibrium with a well-defined estimate <strong>of</strong> the domain <strong>of</strong> attraction can be proven<br />
analytically by the closed loop energy as a Lyapunov function. Even though (locally) predefined<br />
closed loop dynamics is realized by Local Linear Dynamics Assignment [3] the reasonable<br />
parametrization <strong>of</strong> the remaining design quantities is an open issue.<br />
[1] R. Ortega, M. W. Spong, F. Gómez-Estern, G. Blankenstein, Stabilization <strong>of</strong> a Class <strong>of</strong><br />
Underactuated Mechanical Systems Via Interconnection and Damping Assignment, IEEE<br />
TAC 47 (2002), 1218 – 1233.<br />
[2] F. Gómez-Estern, A. J. van der Schaft, Physical Damping in IDA-PBC Controlled Underactuated<br />
Mechanical Systems, EJC 10 (2004), 451 – 468.<br />
[3] P. Kotyczka, Local Linear Dynamics Assignment in IDA-PBC for Underactuated Mechanical<br />
Systems, In: Proc. 50th CDC/ECC, Orlando (2011).<br />
On the number <strong>of</strong> zero crossings in the step response <strong>of</strong> linear time-delay systems<br />
Luc N. Muhirwa, Tobias Damm (<strong>Universität</strong> Bayreuth) Schedule<br />
The similarities between the linear time-delay systems and the standard linear time-invariant<br />
systems are widely studied and discussed in the literature. In this paper we are going to study<br />
the effects <strong>of</strong> the zeros <strong>of</strong> the transfer function <strong>of</strong> the time-delay system on the the step response,<br />
this can be regarded as a genaralization <strong>of</strong> the familiar results on linear time-invariant system.<br />
It will be demonstrated that the phenomena like zerocrossings, undershoot and overshoot in the<br />
step response <strong>of</strong> a time-delay system -which present difficulities in control design- appear as a<br />
result <strong>of</strong> the existence <strong>of</strong> non-minimum phase zeros.<br />
Convergent systems and Incremental Stability<br />
Björn S. Rüffer (<strong>Universität</strong> Paderborn), Nathan van de Wouw (Eindhoven University <strong>of</strong> Technology),<br />
Markus Mueller (University <strong>of</strong> Exeter) Schedule<br />
We consider two similar stability notions that are <strong>of</strong> interest in output-regulation, synchronization,<br />
as well as observer design (see [2] for an overview).<br />
One is the long established notion <strong>of</strong> convergent systems, which is mainly known from the<br />
Russian literature: A system<br />
˙x = f(t, x) (1)<br />
is (globally) uniformly convergent [2] if<br />
1. all solutions x(t, t 0 , x 0 ) exist for all t ≥ t 0 for all initial conditions (t 0 , x 0 ) ∈ R × R n ;<br />
2. there exists a unique solution x(t) in R n defined and bounded for all t ∈ R;<br />
3. the solution x(t) is (globally) uniformly asymptotically stable, i.e., there exists a function<br />
β ∈ KL such that for all (t 0 , x 0 ) ∈ R × R n and t ≥ t 0 ,<br />
�x(t, t 0 , x 0 ) − x(t)� ≤ β � �x 0 − x(t 0 )�, t − t 0� .
Section 20: Dynamics and control 353<br />
The other one is the younger notion <strong>of</strong> incremental stability: System (1) is (globally) incrementally<br />
asymptotically stable [1] if there exists a function β ∈ KL such that for any ξ1, ξ2 ∈ R n and t ≥ t 0 ,<br />
�x(t, t 0 , ξ1) − x(t, t 0 , ξ2)� ≤ β(�ξ1 − ξ2�, t − t 0 ) .<br />
Both notions require that any two solutions <strong>of</strong> a system converge to each other. Yet these<br />
stability concepts are different, in the sense that none implies the other, as we will show using<br />
several examples.<br />
Next, we will illustrate under what additional assumptions one property indeed implies the<br />
other. To that end we characterize both properties in terms <strong>of</strong> Lyapunov functions. We will find<br />
that incremental stability implies uniform convergence if the vector field f(t, x) satisfies a specific<br />
bound or if there exists a compact invariant set for system (1). Uniform convergence implies<br />
incremental stability if the Lyapunov function for convergence satisfies a growth condition. And<br />
lastly, the properties are equivalent when the dynamics <strong>of</strong> system (1) is constrained to a compact<br />
set.<br />
[1] David Angeli, A Lyapunov approach to the incremental stability properties, IEEE Trans.<br />
Autom. Control 47 (2002), no. 3, 410–421.<br />
[2] Alexey Pavlov, Nathan van de Wouw, and Henk Nijmeijer, Uniform output regulation <strong>of</strong><br />
nonlinear systems. A convergent dynamics approach, Birkhäuser, Boston, 2006.<br />
Optimal value functions for weakly coupled systems: a posteriori estimates<br />
Péter Koltai, Oliver Junge (TU München) Schedule<br />
We consider weakly coupled LQ optimal control problems and derive estimates on the sensitivity<br />
<strong>of</strong> the optimal value function in dependence <strong>of</strong> the coupling strength. Our main result is that if<br />
a weak coupling suffices to destabilize the closed loop system with the optimal feedback <strong>of</strong> the<br />
uncoupled system (i.e. when additional efforts has to be made in order to stabilize the coupled<br />
system), then the value function might change drastically with the coupling. As a consequence,<br />
it is not reasonable to expect that a weakly coupled system possesses a ”weakly coupled” optimal<br />
value function. This lack <strong>of</strong> regularity suggests that the approximation <strong>of</strong> the optimal value function<br />
in high dimensions is even for weakly coupled systems a rather difficult task.<br />
S20.5: Partial differential equations Thu, 13:30–15:30<br />
Chair: Stephan Trenn, Knut Graichen S1|01–A4<br />
An approach for parameter identification in distributed parameter systems<br />
T. Knüppel, F. Woittennek (TU Dresden) Schedule<br />
Recently, an approach for the parameter identification in linear finite-dimensional systems introduced<br />
in [1] has been generalized to linear distributed parameter systems [3]. The approach is<br />
based on algebraic computations over certain convolution rings <strong>of</strong> generalized functions. The fact<br />
that only boundary measurements are necessary makes the approach very attractive for applications.<br />
The present contribution is concerned with a modified approach to the same problem. As<br />
before only boundary measurements are necessary. The starting point is a linear boundary value<br />
problem involving partial differential equations <strong>of</strong> hyperbolic or parabolic type. It is assumed that<br />
the equations depend linearly on several initially unknown parameters.<br />
As in the flatness based approach to the control <strong>of</strong> infinite dimensional systems the first<br />
step is the reformulation <strong>of</strong> the boundary value problem under consideration as a system <strong>of</strong>
354 Section 20: Dynamics and control<br />
convolution equations for the boundary trajectories [2]. These equations which constitute the basis<br />
for the parameter identification may involve derivatives <strong>of</strong> the boundary trajectories. Therefore,<br />
the identification is preceded by a regularization procedure. Then the parameters are computed<br />
by minimizing appropriate error functionals.<br />
The approach is demonstrated with the help <strong>of</strong> simple examples comprising the heat equation<br />
and the wave equation.<br />
[1] M. Fliess and H. Sira-Ramírez, An algebraic framework for linear identification, ESAIM:<br />
COCV (Control, Optimisation and Calculus <strong>of</strong> Variations) 9, 151–168 (2003).<br />
[2] H. Mounier, J. Rudolph, and F. Woittennek, Boundary value problems and convolutional systems<br />
over rings <strong>of</strong> ultradistributions, in: Lecture Notes In Control and Information Sciences<br />
Vol. 407 (Springer-Verlag, 2010).<br />
[3] J. Rudolph and F. Woittennek, An algebraic approach to parameter identification in linear<br />
infinite dimensional systems, in: Proc. 16th Mediterranean Conference on Control and<br />
Automation, (2008), pp. 332–337.<br />
Algebraic parameter identification for a heavy rope with internal damping<br />
Nicole Gehring (<strong>Universität</strong> des Saarlandes), Torsten Knüppel (TU Dresden), Joachim Rudolph<br />
(<strong>Universität</strong> des Saarlandes), Frank Woittennek (TU Dresden) Schedule<br />
Extending work <strong>of</strong> M. Fliess and H. Sira-Ramírez [1], two <strong>of</strong> the authors proposed an algebraic<br />
approach to the parameter identification for systems described by linear partial differential equations<br />
with constant coefficients [2,3]. The approach uses operational calculus to generate equations<br />
that involve only convolution products <strong>of</strong> known (boundary) measurements and the system parameters.<br />
Here, by considering a heavy rope model the approach is extended to a partial differential<br />
equation with spatially dependent coefficients. As in the case <strong>of</strong> constant coefficients, the time<br />
derivatives are replaced by the operator s and the system variables and their derivatives are<br />
represented by Mikusiński operators and operational functions. As well known, the resulting<br />
ordinary differential equation is a Bessel equation. Hence, the solution <strong>of</strong> the boundary value<br />
problem can be expressed as a linear combination <strong>of</strong> Bessel functions <strong>of</strong> the first and second kind.<br />
Note that these Bessel functions satisfy a known differential relation with respect to s. Assuming<br />
homogeneous initial conditions this knowledge can be exploited to eliminate the Bessel functions.<br />
The resulting equation involves convolution products <strong>of</strong> the system variables and is polynomial<br />
with respect to the system parameters. Based on these equations the parameters can be calculated<br />
either by solving nonlinear equations or by considering them as mutually independent and using<br />
overparameterization.<br />
The rope is modeled with an internal damping and a horizontally moving suspension point.<br />
A mass may be attached to the free end. It will be shown that the knowledge <strong>of</strong> the trajectories<br />
<strong>of</strong> the boundary values at the suspension is sufficient to identify all physical parameters <strong>of</strong> the<br />
rope. Simulation results are given to illustrate the approach.<br />
[1] M. Fliess, H. Sira-Ramírez, An algebraic framework for linear identification, ESAIM: COCV<br />
9 (2003), 151–168.<br />
[2] J. Rudolph, F. Woittennek, Ein algebraischer Zugang zur Parameteridentifikation in linearen<br />
unendlichendimensionalen Systemen, at – Automatisierungstechnik 55 (2007), 457–467.
Section 20: Dynamics and control 355<br />
[3] J. Rudolph, F. Woittennek, Identification de paramètres d’un modèle d’échangeurs de chaleur,<br />
in: Actes Conf. Int. Francophone d’Automatique, Nancy (France), 2–4 juin 2010.<br />
Identification <strong>of</strong> transmission line parameters using algebraic methods<br />
Nicole Gehring, Joachim Rudolph (<strong>Universität</strong> des Saarlandes), Christian Stauch (ZeMA gGmbH,<br />
Saarbrücken) Schedule<br />
An algebraic approach to parameter identification for transmission lines is proposed. The class <strong>of</strong><br />
systems under consideration can be modelled by means <strong>of</strong> a pair <strong>of</strong> coupled first order linear partial<br />
differential equations in one spatial dimension. That includes examples from different technical<br />
domains such as the telegrapher’s equations or models for fluid transmission lines. Under the<br />
assumption <strong>of</strong> homogeneous initial conditions, replacing the system variables for effort and flow<br />
by operational functions ê and ˆ f leads to<br />
d<br />
dz ê(s, z) + ˆ Γ(s) ˆ Z(s) ˆ f(s, z) = 0 (1a)<br />
d<br />
� �<br />
ˆZ(s) f(s, ˆ z) +<br />
dz<br />
ˆ Γ(s)ê(s, z) = 0, (1b)<br />
where z denotes the spatial variable and ˆ Γ(s) and ˆ Z(s) are the propagation operator and the<br />
impedance operator. The use <strong>of</strong> operational calculus has been shown to be suitable for parameter<br />
identification in systems <strong>of</strong> both finite and infinite dimension (see e.g., [1,2]). The main idea <strong>of</strong><br />
this approach is to generate a set <strong>of</strong> equations involving only measured signals and parameters,<br />
in such a way that it can be easily interpreted in the time domain. To this end, operators are<br />
eliminated using the differential equations they satisfy. Finally, time domain equations are used<br />
for pointwise calculation <strong>of</strong> the unknown parameters.<br />
The proposed identification method is illustrated considering a fluid transmission line model<br />
with laminar flow and frequency dependent viscous friction [3]. Using simulation data, the<br />
kinematic viscosity and the bulk modulus <strong>of</strong> the fluid are identified.<br />
[1] M. Fliess, H. Sira-Ramírez: An algebraic framework for linear identification, ESAIM: COCV,<br />
9, 151–168 (2003).<br />
[2] J. Rudolph, F. Woittennek: Ein algebraischer Zugang zur Parameteridentifikation in linearen<br />
unendlichdimensionalen Systemen, at – Automatisierungstechnik, 55, 457–467 (2007).<br />
[3] A.F. D’Souza, R. Oldenburger: Dynamic response <strong>of</strong> fluid lines, Journal <strong>of</strong> basic engineering,<br />
86, 589–598 (1964).<br />
POD and CVT Galerkin reduced-order modeling <strong>of</strong> the flow around a cylinder<br />
Sebastian Ullmann, Jens Lang (TU <strong>Darmstadt</strong>) Schedule<br />
In this talk the application <strong>of</strong> Galerkin reduced-order models to the laminar incompressible vortexshedding<br />
flow around a circular cylinder is presented. The methods rely on approximate bases <strong>of</strong><br />
the solution space computed from a set <strong>of</strong> velocity snapshots {�un} N n=1. While the proper orthogonal<br />
decomposition (POD) delivers basis functions {�ϕr} R r=1 that minimize the kinetic energy <strong>of</strong> the<br />
projection error,<br />
min<br />
{�ϕr}<br />
N� � R� �<br />
�<br />
�<br />
��un − (�ϕr, �un)�ϕr � 2<br />
,<br />
n=1<br />
r=1
356 Section 20: Dynamics and control<br />
the centroidal Voronoi tessellation (CVT) delivers basis functions that are themselves approximations<br />
<strong>of</strong> snapshots. This is achieved by arranging the snapshots in clusters {Vr} R r=1 and using<br />
the cluster centroids as basis functions, which leads to the minimization problem<br />
min min<br />
{�ϕr} {Vr}<br />
R� � � �<br />
� �<br />
��un − �ϕr � 2<br />
.<br />
r=1 �un∈Vr<br />
The errors in the reduced velocities are dependent on the number <strong>of</strong> modes and the accuracy <strong>of</strong><br />
the underlying finite element simulation. An appropriate choice <strong>of</strong> the outflow boundary condition<br />
eliminates the need for pressure modeling or calibration. Still, to obtain drag and lift forces, a<br />
reduced-order pressure model can be solved, additionally. A comparison <strong>of</strong> the CVT and POD<br />
methods with respect to their efficiency and accuracy will be presented.<br />
Flatness-based Feedforward Control Design <strong>of</strong> a System <strong>of</strong> Parabolic PDEs Basedon<br />
Finite Difference Semi-Discretization<br />
Tilman Utz (<strong>Universität</strong> Ulm), Andreas Kugi (TU Wien) Schedule<br />
Tubular catalytic fixed-bed reactors constitute a form <strong>of</strong> chemical reactors which can be found in a<br />
wide range <strong>of</strong> applications from automotive catalytic converters to large polymerization reactors.<br />
An important control objective for chemical reactors is the realization <strong>of</strong> setpoint transitions for<br />
example for ignition or extinction as well as for grade transitions. A main difficulty thereby can<br />
be identified by the usually very significant nonlinearities caused by the chemical reaction.<br />
In order to mathematically model fixed-bed reactors, in particular to sufficiently describe<br />
the chemical reaction, it is necessary to consider the distribution <strong>of</strong> the temperature and <strong>of</strong><br />
the reacting species concentration over the length <strong>of</strong> the reactor. Taking into account nonlinear<br />
reaction expressions, for example in terms <strong>of</strong> the Arrhenius equation, this leads to a system <strong>of</strong><br />
semilinear parabolic partial differential equations in a one-dimensional spatial domain. Control<br />
thereby usually is applied via one <strong>of</strong> the boundaries, namely the inlet <strong>of</strong> the reactor, e. g., [1].<br />
For the feedforward control design, an approach is applied, which is based on the semidiscretization<br />
<strong>of</strong> the governing partial differential equations and <strong>of</strong> the boundary conditions using<br />
finite differences with respect to the spatial coordinate. It is shown that the temperature and<br />
the concentration at the reactor outlet represent a so-called flat output <strong>of</strong> the semi-discretized<br />
system. This allows for the parametrization <strong>of</strong> the states and the boundary inputs <strong>of</strong> the semidiscretized<br />
system in terms <strong>of</strong> the flat output and its time derivatives and therefore constitutes a<br />
systematic approach to the design <strong>of</strong> feedforward control for the considered transition problems<br />
[2]. Furthermore, it is shown that with the use <strong>of</strong> non-equidistant grids for the semi-discretization<br />
it is possible to partly resolve the antagonistic demands to carry out the parametrization on a<br />
very fine grid in order to properly reflect the nonlinearities and to use a coarse grid in view <strong>of</strong> the<br />
computational efficiency.<br />
[1] van Doesburg, H.; de Jong, W. A.: Chem. Eng. Sci. 31 (1976), 45–51.<br />
[2] Utz, T.; Meurer, T.; Kugi, A.: Int. J. Control., 83 (2010), 1093–1106.<br />
Modelling and control <strong>of</strong> a smart beam<br />
Nader Ghareeb, Rüdiger Schmidt (RWTH Aachen) Schedule<br />
In modern engineering, weight optimization has always the highest priority during the design <strong>of</strong><br />
structures. It has the advantage <strong>of</strong> minimizing the amount <strong>of</strong> raw material used and this will
Section 20: Dynamics and control 357<br />
reduce the manufacturing and operational costs. On the other hand, it results in lower stiffness<br />
and thus more sensitivity to vibrations.<br />
In this work, a simple and active controller is presented. It is used to attentuate the vibrations<br />
<strong>of</strong> a smart beam. A modified FE-Model <strong>of</strong> that beam is used and the adequate damping coefficients<br />
are calculated and added to it. After that, a super element is created and then represented in the<br />
form <strong>of</strong> state-space equations prior to the design <strong>of</strong> the controller.<br />
Finally, the model is excited by its natural frequency and it is left to vibrate freely. Through<br />
the design <strong>of</strong> a suitable controller, these vibrations are minimized, and results are shown.<br />
S20.6: Model reduction and simulation Thu, 16:00–18:00<br />
Chair: Knut Graichen, Stephan Trenn S1|01–A4<br />
Model reduction for optimal control problems in field-flow fractionation<br />
Carina Willbold, Tatjana Stykel (<strong>Universität</strong> Augsburg) Schedule<br />
We discuss the application <strong>of</strong> model order reduction to optimal control problems governed by<br />
coupled systems <strong>of</strong> the Stokes-Brinkmann and advection diffusion equations. Such problems arise<br />
in field-flow fractionation processes for the efficient and fast separation <strong>of</strong> particles <strong>of</strong> different<br />
size in micr<strong>of</strong>luidic flows. Our approach is based on a combination <strong>of</strong> balanced truncation and<br />
tangential interpolation for model reduction <strong>of</strong> the semidiscretized optimality system. Numerical<br />
results demonstrate the properties <strong>of</strong> this approach.<br />
Balanced Truncation <strong>of</strong> positive linear systems<br />
Christian Grußler (TU Kaiserslautern), Pr<strong>of</strong>. Tobias Damm (<strong>Universität</strong> Bayreuth) Schedule<br />
We consider methods <strong>of</strong> model order reduction for positive linear time-invariant systems<br />
preserving the positivity. This issue has been addressed earlier e.g. in [1] − [3]. The methods<br />
presented there, however, <strong>of</strong>ten do not give a good approximation in the H ∞ -norm and neglect<br />
the advantage <strong>of</strong> a projection approach such as standard balanced truncation.<br />
In our talk we first show that standard balanced truncation to first order always leads to<br />
a positive system, which outperforms earlier methods in many examples, especially in case <strong>of</strong><br />
SISO systems. This idea is then extended to obtain higher order positive approximations. To<br />
this end we derive a symmetry property <strong>of</strong> the balanced realization <strong>of</strong> any linear SISO system.<br />
Again we provide numerical examples to illustrate the properties <strong>of</strong> this approach.<br />
[1] T. Reis and E. Virnik, Positivity preserving balanced truncation for descriptor systems, SIAM<br />
J. Control Optim., vol. 48, no.4, pp. 2600 - 2619, 2009<br />
[2] J. Feng, J. Lam, Z. Shu and Q. Wand, Internal positivity preserved model reduction, Int. J.<br />
Control, vol. 83, no. 3, pp. 575 - 584, 2010<br />
[3] P. Li, J. Lam and Z. Wang, Positivity-preserving H∞ model reduction for positive systems,<br />
Automatica, vol. 47, pp. 1504 - 1511, 2011<br />
Model order reduction methods and their possible application in compliant mechanisms<br />
Malte Rösner, Rolf Lammering (<strong>Universität</strong> der Bundeswehr Hamburg) Schedule<br />
A new approach to develop a feed unit <strong>of</strong> small machine tools for small workpieces is based<br />
on the application <strong>of</strong> compliant mechanisms. Currently, non-intuitive design and optimization
358 Section 20: Dynamics and control<br />
techniques are in progress as well as controlling, measuring and calibration strategies. To describe<br />
the mechanical behavior <strong>of</strong> a feed unit in an accurate way, very large and sparse finite element<br />
models arise. This leads to numerical simulations which require an unacceptable amount <strong>of</strong> time<br />
and memory space and motivates the introduction and application <strong>of</strong> model order reduction<br />
(MOR) techniques.<br />
Model order reduction appears to be beneficial for the synthesis and simulation <strong>of</strong> compliant<br />
mechanisms due to computational costs. It is an established method in many technical fields for<br />
the approximation <strong>of</strong> large-scale linear time-invariant and nonlinear dynamical systems described<br />
by differential equations. Based on system theory, underlying representations <strong>of</strong> the dynamical<br />
system are introduced from which the general reduced order model is derived by projection.<br />
During the last years, numerous new procedures were published and investigated appropriate to<br />
simulation, optimization and control. Methods based on condensation [1], Krylov subspacess [2],<br />
singular value decomposition [3] and proper orthogonal decomposition [4] are reviewed and their<br />
advantages and disadvantages are outlined. The convenience <strong>of</strong> applying model order reduction<br />
in compliant mechanisms is quoted.<br />
[1] Gasch, R. and Knothe, K.: Strukturdynamik, Bd. 2, Springer, New York, NY, USA, 1989.<br />
[2] Eid, R.: Time Domain Model Reduction by Moment Matching, Ph.D. thesis, TU München,<br />
2009.<br />
[3] A. Antoulas. Approximation <strong>of</strong> large-scale dynamical systems. Society for Industrial Mathematics,<br />
2005.<br />
[4] Liang, Y.; Lee, H.; Lim, S.; Lin, W.; Lee, K. Wu, C. Proper orthogonal decomposition and its<br />
applications - Part I: Theory. Journal <strong>of</strong> Sound and Vibration, Elsevier, 2002, 252, 527-544<br />
.<br />
Simulating steady flows with Gappy POD<br />
Alexander Vendl (TU Braunschweig) Schedule<br />
We will use a reduced order method called Gappy POD to simulate steady aerodynamic flows for<br />
varying angles <strong>of</strong> attack. Gappy POD is - as the name suggests - based on Proper Orthogonal<br />
Decomposition (POD). Given a set <strong>of</strong> snapshots, which are solutions characteristic <strong>of</strong> the dynamics,<br />
POD stores these snapshots in a matrix and computes a Singular Value Decomposition <strong>of</strong><br />
it. This yields an optimal basis to represent the flow solutions.<br />
The basic idea <strong>of</strong> Gappy POD is to find coefficients for the POD basis vectors such that the<br />
thus given POD representation best fits some given data. This is achieved by a least-squares linear<br />
regression approach.<br />
In our work we try to match the boundary conditions <strong>of</strong> the farfield, which are strongly<br />
dependent on the varying parameter, that is, the angle <strong>of</strong> attack. Since the boundary conditions<br />
are known a priori, it is in fact justified to speak <strong>of</strong> simulating the solution.<br />
The simulation model <strong>of</strong> a laboratory truck crane<br />
Dawid Cekus, Pawel Warys (Częstochowa University <strong>of</strong> Technology) Schedule<br />
The exhaustive construction <strong>of</strong> prototypes <strong>of</strong> all classes <strong>of</strong> cranes or other labour-machines <strong>of</strong><br />
interest to experimental research is economically and practically infeasible. Therefore, simulation<br />
modelling is very useful and has fundamental influence on the design <strong>of</strong> new structures as well as
Section 20: Dynamics and control 359<br />
the modification <strong>of</strong> existing structures. For these reasons, this paper presents a simulation model<br />
<strong>of</strong> a laboratory truck crane [1].<br />
The simulation model has been worked out using the SolidWorks and Matlab-Simulink programs.<br />
In the SolidWorks program, a parametric geometrical model (CAD model) has been worked<br />
out. Next, thanks to the existence <strong>of</strong> an interface between the above-mentioned programs, the<br />
CAD model has been converted into an XML physical model and implemented in the Matlab-<br />
Simulink environment. In the Matlab-Simulink package, the model has been verified and supplemented<br />
by signal sources, executive and measuring elements.<br />
This simulation model allows the creation <strong>of</strong> advanced kinematic simulations (e.g. motion<br />
trajectories, components <strong>of</strong> velocity and acceleration <strong>of</strong> the end <strong>of</strong> boom) for any configuration<br />
<strong>of</strong> the analysed system based on control functions, which are responsible for the realization <strong>of</strong><br />
movements <strong>of</strong> two telescopic boom members, rotation and slope <strong>of</strong> the telescopic boom.<br />
[1] L. Tomski, W. Chwalba:, System for testing the vibration <strong>of</strong> a truck-crane model, Proceedings<br />
<strong>of</strong> Conference RResearch Methods <strong>of</strong> Labour-Machines“, Papers <strong>of</strong> Construction Equipment<br />
Research Institute 1-3 91 (1989), 206 – 214 (in Polish).<br />
The dynamics study <strong>of</strong> load carried by the two-member grab system<br />
Pawel Warys, Dawid Cekus (Częstochowa University <strong>of</strong> Technology) Schedule<br />
This paper presents the formulation <strong>of</strong> the theoretical and calculation model which enables the<br />
simulation <strong>of</strong> the motion <strong>of</strong> a load carried by a forest crane [2]. The lifted load and carrying<br />
system have been modeled as a 3D rigid body. The application <strong>of</strong> such a load model results in<br />
the simplification and improvement <strong>of</strong> the calculation algorithm. The equations <strong>of</strong> the coupled<br />
motion <strong>of</strong> the system load-machine elements have been derived.<br />
During lift different dynamics effects occur. Consequently, the position <strong>of</strong> a carried load is<br />
sometimes difficult to control [1]. The kinematic model presented enables the analysis <strong>of</strong> the basic<br />
motion <strong>of</strong> the load as a response <strong>of</strong> the system to operational control <strong>of</strong> the forest crane. In order<br />
to determine the motion parameters, it is assumed that all system elements are rigid. The lifted<br />
load is also treated as a rigid body that moves as the result <strong>of</strong> the movement <strong>of</strong> the suspension<br />
point <strong>of</strong> load and the dynamic interactions generated during the motion <strong>of</strong> the system.<br />
The primary focus <strong>of</strong> the dynamic model is to describe the movement <strong>of</strong> load as a body in threedimensional<br />
space. This model allows calculation <strong>of</strong> the movement <strong>of</strong> a load under the influence<br />
<strong>of</strong> kinematic effects and further the free motion <strong>of</strong> the load as a result <strong>of</strong> the previous forced<br />
motion. In the next step, the dynamic model is modified to permit the mathematical description<br />
<strong>of</strong> additional displacements resulting from the finite stiffness <strong>of</strong> various machine elements.<br />
The sample numerical calculations have been derived using the Matlab system. The initial<br />
problem has been solved by the Runge-Kutta method. The numerical program has been developed<br />
based on the presented model which allows analysis <strong>of</strong> the motion <strong>of</strong> load arising from crane<br />
operating mechanisms.<br />
[1] B. Posiadala: Influence <strong>of</strong> crane support system on motion <strong>of</strong> the lifted load, Mechanism and<br />
Machine Theory, 32 (1997), 9-20.<br />
[2] P. Warys: Modeling and investigation <strong>of</strong> dynamics <strong>of</strong> the forest crane, PhD Thesis, Czestochowa<br />
University <strong>of</strong> Technology, 2011, 97-128.
360 Section 21: Mathematical image processing<br />
Section 21: Mathematical image processing<br />
Organizers: Tobias Preusser (Jacobs University Bremen), Gabriele Steidl (<strong>Universität</strong> Kaiserslautern)<br />
S21.1: Mathematical Image Processing I Tue, 13:30–15:30<br />
Chair: Gabriele Steidl S1|03–110<br />
Convex Relaxation Techniques in Image Analysis<br />
Daniel Cremers (TU München) Schedule<br />
Numerous image analysis problems correspond to non-convex energies, giving rise to suboptimal<br />
solutions and <strong>of</strong>ten strong dependency on appropriate initialization. In my presentation, I will<br />
show how problems like image segmentation, multiview stereo reconstruction and optic flow<br />
estimation can be formulated as variational problems. Subsequently, I will introduce methods <strong>of</strong><br />
convexification which allow to compute globally optimal or near-optimal solutions. The resulting<br />
algorithms provide robust solutions, independent <strong>of</strong> initialization. Parallel GPU implementations<br />
allow for acceptable runtimes.<br />
A Convex Shape Prior and Shape Matching Based on the Gromov-Wasserstein Distance<br />
Bernhard Schmitzer, Christoph Schnoerr (<strong>Universität</strong> Heidelberg) Schedule<br />
We present a novel convex shape prior functional with potential for application in variational<br />
image segmentation. Based on the Gromov-Wasserstein distance an approximation is derived that<br />
takes the form <strong>of</strong> an optimal transport problem with relaxed constraints. The approach inherits<br />
the ability to incorporate vast classes <strong>of</strong> geometric invariances beyond rigid isometries and is<br />
apt for processing additional (non-geometric) feature information within the same framework.<br />
The resulting functional can be minimized by standard linear programming methods and yields<br />
a unique assignment <strong>of</strong> a given shape template to a given image. Numerical experiments are<br />
reported that illustrate key aspects <strong>of</strong> the approach, and open problems are outlined.<br />
Nonconvex TV q -Models in Image Restoration: Analysis and a Trust-Region Regularization<br />
Based Superlinearly Convergent Solver<br />
Tao Wu (<strong>Universität</strong> Graz), Michael Hintermüller (HU Berlin) Schedule<br />
A nonconvex variational model is introduced which contains the ℓ q -“norm”, q ∈ (0, 1), <strong>of</strong> the<br />
gradient <strong>of</strong> the image to be reconstructed as the regularization term together with a least-squares<br />
type data fidelity term which may depend on a possibly spatially dependent weighting parameter.<br />
Hence, the regularization term in this functional is a nonconvex compromise between the<br />
minimization <strong>of</strong> the support <strong>of</strong> the reconstruction and the classical convex total variation model.<br />
In the discrete setting, existence <strong>of</strong> a minimizer is proven, a Newton-type solution algorithm is<br />
introduced and its global as well as locally superlinear convergence is established. The potential<br />
indefiniteness (or negative definiteness) <strong>of</strong> the Hessian <strong>of</strong> the objective during the iteration is<br />
handled by a trust-region based regularization scheme. The performance <strong>of</strong> the new algorithm<br />
is studied by means <strong>of</strong> a series <strong>of</strong> numerical tests. For the associated infinite dimensional model<br />
an existence result based on the weakly lower semicontinuous envelope is established and its<br />
relation to the original problem is discussed.<br />
An Estimation Theoretical View on Ambrosio-Tortorelli Image Segmentation<br />
Kai Krajsek, Ines Dedovic, Hanno Scharr (Forschungszentrum Jülich) Schedule
Section 21: Mathematical image processing 361<br />
In this contribution, we consider the Ambrosio-Tortorelli (AT) functional for image segmentation<br />
from an estimation theoretical point <strong>of</strong> view. The Mumford-Shah (MS) functional is maybe<br />
the most well-known constraint used for image segmentation. A major difficulty in using it is<br />
the handling <strong>of</strong> inner image borders as lines, being circumvented by Ambrosio and Tortorellis<br />
approximation. They introduce a smooth edge indicator function instead <strong>of</strong> the original line-like<br />
edge indicator. The AT approach contains the Mumford-Shah functional as the limit <strong>of</strong> a certain<br />
parameter. Unlike many other approaches, e.g. using level-sets, open boundaries can be handled<br />
easily. Using such a functional, image segmentation is understood to be joint image regularization<br />
and edge-map reconstruction.<br />
Previous approaches consider AT segmentation as a deterministic optimization problem by minimizing<br />
the energy functional, resulting in a single point estimate, i.e. the maximum-a-posteriori<br />
(MAP) estimate. We adopt a wider estimation theoretical view-point. Instead <strong>of</strong> minimizing an<br />
energy functional in the original formulation, we interpret the AT functional as the energy <strong>of</strong> a<br />
posterior probability density function and derive an effective block-Gibbs-sampler for approximating<br />
the minimum mean square and the minimum medium estimator. The merit <strong>of</strong> our approach<br />
is multi-fold: First, sampling from the posterior PDF allows to apply different types <strong>of</strong> estimators<br />
and not only the MAP estimator. Second, sampling allows to estimate higher order statistical<br />
moments like the variance as a confidence measure. Third, our approach is not prone to get<br />
trapped into local minima as other AT image reconstruction approaches, but our approach is<br />
asymptotically statistical optimal.<br />
Nonlinear eigenproblems for high-dimensional data analysis<br />
Simon Setzer, Matthias Hein (<strong>Universität</strong> des Saarlandes) Schedule<br />
In many fields such as machine learning, computer vision and exploratory data analysis, a major<br />
goal is the development <strong>of</strong> solutions for the automatic and efficient extraction <strong>of</strong> knowledge from<br />
data. A great number <strong>of</strong> important methods for data analysis are based on eigenproblems. While<br />
linear eigenproblems are standard tools in many applications, e.g., in the form <strong>of</strong> the principal<br />
component analysis or spectral clustering, they are limited in their modeling capabilities. In this<br />
talk, we will discuss nonlinear eigenproblems since they significantly extend the modeling freedom.<br />
In particular, the important principles <strong>of</strong> sparsity and robustness can be incorporated. After<br />
an introduction <strong>of</strong> the framework, we will present recent results on an important application <strong>of</strong><br />
nonlinear eigenproblems, namely tight relaxations <strong>of</strong> balanced graph cuts. Moreover, an efficient<br />
algorithm - a generalization <strong>of</strong> the inverse power method - is introduced for the resulting nonconvex<br />
and nonsmooth optimization problems.<br />
S21.2: Mathematical Image Processing II Tue, 16:00–18:00<br />
Chair: Tobias Preusser S1|03–110<br />
Analysis <strong>of</strong> Space-Discrete Image Filters Involving Inverse Diffusion<br />
Martin Welk (UMIT Hall) Schedule<br />
Discontinuity-enhancing image filters based on nonlinear diffusion PDEs are well established in<br />
image processing. Promising candidates for such filters, however, involve negative diffusivities that<br />
pose challenges for their analysis and numerical treatment. Spatial discretisations <strong>of</strong> these PDEs<br />
can be analysed using ODE systems. In some cases, they give rise to interesting nonstandard<br />
numerical methods for the image filters in question. In the talk, recent results in this area will be<br />
presented.<br />
Robust Nonlinear PDEs for Multiscale Morphological Image Analysis<br />
El Hadji S. Diop, Jesus Angulo (Mines ParisTech) Schedule
362 Section 21: Mathematical image processing<br />
In many image processing and computer vision tasks (e.g. data compression, feature detection, motion<br />
analysis/detection, multiband frequency analysis, . . . ), it is important to perform a multiscale analysis<br />
i.e. analyze the image at multiple spatial scales. Owing to that fact, mathematical morphology [1] appeared<br />
as a powerful tool in multiscale analysis [2], mainly due to its nonlinearity aspects, shape and<br />
geometry description properties. Let E = Z 2 or a subset <strong>of</strong> Z 2 . Morphological operators can be defined<br />
by combination and/or duality <strong>of</strong> the elementary dilation operation defined for any function f : E → ¯ R,<br />
by: (f ⊕b)(x) = ∨y∈E[f(y)+b(x−y)] (1), where ∨ represents the supremum, and b : R 2 → ¯ R is a concave<br />
structuring function (ST) that could be flat i.e. b = 0 in a convex bounded set B and −∞ outside, or<br />
non flat i.e. a general concave function. For t ≥ 0, one can define then a multiscale dilation (or erosion)<br />
by replacing b by the family <strong>of</strong> multiscale ST (bt)t≥0 defined for t > 0 by bt(x) = tb(x/t), and for t = 0<br />
by 0 for x = 0 and −∞ otherwise. In the case <strong>of</strong> flat ST, this is equivalent to consider sets Bt = tB.<br />
Alternatives to perform multiscale continuous flat dilation (erosion) by using PDEs were proposed [3-4]:<br />
∂ut = ±�∇u�, u(x, 0) = f(x) (2), with (+) (resp. (−)) for the multiscale dilation (resp. erosion). Despite<br />
various and successful applications, it is clear that neither the discrete (1) nor the continuous (2)<br />
formulations are robust in a noisy environment. Indeed, in that case, taking the supremum as in (1) will<br />
definitely lead to wrong values, while hyperbolic PDE (2) will blow up. The main reason is that all image<br />
pixels are treated in a same global way. To avoid that, adapted morphological filters based on image<br />
edges were proposed by means <strong>of</strong> spatially-variant shape kernels [5] or bilateral ST [6]. Using a PDE approach,<br />
an adaptive method was presented in [7] by multiplying the image gradient with a space-variant<br />
matrix, in order to enhance coherence <strong>of</strong> flow-like structures. Herein, we overcome these drawbacks by<br />
providing more robust and more adaptive PDEs, as well as corresponding operators. We first proposed<br />
Gaussian regularized versions <strong>of</strong> (2): ∂ut = ±�∇uσ�, u(x, 0) = f(x) (3). Second proposed PDEs are<br />
locally adaptive, and account intrinsic image features: ∂ut = ±g(�∇uσ�)�∇u�, u(x, 0) = f(x) (4), where<br />
g is either increasing or decreasing. PDEs (3) and (4) are implemented using different numerical schemes<br />
and a proposed one.<br />
[1] J. Serra, Image Analysis and Mathematical Morphology (AP, 1982).<br />
[2] P. Soille, Morphological Image Analysis (Springer-Verlag, England, 1999).<br />
[3] L. Alvarez, F. Guichard, P. -L. Lions, and J. -M. Morel, Arch. Rational Mech. Anal. 123, 199-257<br />
(1993).<br />
[4] G. Sapiro, R. Kimmel, D. Shaked, B. B. Kimia, and A. M. Bruckstein, Pattern Recognition 26 (1993),<br />
1363-1372.<br />
[5] R. Lerallut, E. Decencière, and F. Meyer, IVC 25 (2007), 395-404.<br />
[6] J. Angulo, in: ISMM, LNCS 6671 (Italy, July 2011), pp. 212–223.<br />
[7] M. Breuβ, B. Benedi, and J. Weickert, in: LNCS 4487 (Ger., 2007), pp. 515-522<br />
Volumetric Nonlinear Anisotropic Diffusion on GPUs<br />
Arjan Kuijper (Fraunh<strong>of</strong>er IGD/TU <strong>Darmstadt</strong>), Andreas Schwarzkopf, Thomas Kalbe, Michael<br />
Goesele (TU <strong>Darmstadt</strong>) Schedule<br />
We present an efficient implementation <strong>of</strong> volumetric nonlinear anisotropic image diffusion on<br />
modern programmable graphics processing units (GPUs). We avoid the computational bottleneck<br />
<strong>of</strong> a time consuming eigenvalue decomposition in R 3 . Instead, we use a projection <strong>of</strong> the Hessian<br />
matrix along the surface normal onto the tangent plane <strong>of</strong> the local isodensity surface and solve for<br />
the remaining two tangent space eigenvectors. We derive closed formulas to achieve this resulting<br />
in efficient GPU code. We show that our most complex volumetric nonlinear anisotropic diffusion
Section 21: Mathematical image processing 363<br />
gains a speed up <strong>of</strong> more than 600 compared to a CPU solution.<br />
Image analysis <strong>of</strong> four-dimensional data from fluorescence microscopy<br />
Hendrik Dirks (<strong>Universität</strong> Münster) Schedule<br />
The image analysis <strong>of</strong> four-dimensional data from fluorescence microscopy is a challenging task,<br />
in particular in living probes. We discuss advanced image processing techniques to tackle this<br />
issue, from denoising <strong>of</strong> Poisson distributed data using a total variation model to optical flow and<br />
particle models for the analysis <strong>of</strong> intracellular flow.<br />
Our focus lies on the movement <strong>of</strong> proteins in developmental neurobiology such as the polarization<br />
<strong>of</strong> the axon from previously unspecific neurites. The transport properties obtained by<br />
imaging can be used to identify certain proteins and their role in development.<br />
Quantitative X-ray tomography with X-ray tubes<br />
Stefan Günther, Stefan Odenbach (TU Dresden) Schedule<br />
X-ray tomography is used to generate three-dimensional models <strong>of</strong> opaque objects from projections<br />
at various angles. This non-destructive method is increasingly applied in non-medical diagnostic,<br />
where a spatial resolution <strong>of</strong> some micrometers is possible. Laboratory tomography setups with<br />
a high availability are equipped with X-ray tubes as radiation source, which emit polychromatic<br />
radiation. The non-linear attenuation <strong>of</strong> polychromatic radiation causes beam hardening artifacts<br />
and is a significant problem for a quantification. Using precise fabricated wedges, it is possible to<br />
determine a corrective function to compensate the non-linearity for single material systems. For<br />
multi material systems a system <strong>of</strong> equations has to be solved to decompose the projection data.<br />
The result <strong>of</strong> this decomposition is a linear information about each material independent from<br />
the photon energy. It will be shown, how this calibration method was applied for a cone beam<br />
geomety to get tomograms without beam hardening artifacts.<br />
Hyperelasticity in Correspondence Problems<br />
Jan Modersitzki (University <strong>of</strong> Lübeck Institute <strong>of</strong> Mathematics and Image Computing Maria-<br />
Goeppert-Str. 1a, 23562 Lübeck), Lars Ruthotto (University <strong>of</strong> Lübeck Institute <strong>of</strong> Mathematics<br />
and Image Computing Maria-Goeppert-Str. 1a, 23562 Lübeck) Schedule<br />
Image registration is one <strong>of</strong> the challenging problems in image processing. Given are two images<br />
that are taken for example at different times, from different devices or perspectives. The goal is<br />
to determine a reasonable transformation, such that a transformed version <strong>of</strong> one <strong>of</strong> the images is<br />
similar to the second one. The problem is typically phrased in a variational setting for the wanted<br />
transformation and regularization is a key issue.<br />
In this talk, we present an introduction to hyperelastic image registration which is motivated<br />
by an applications from cardiac PET imaging. More specifically, we present a hyperelastic<br />
regularizer and we show that this regularizer enables the recovery <strong>of</strong> large and highly non-linear<br />
transformations. We also show that this regularization results in diffeomorphic mappings. The<br />
price to be paid is a non-convex but polyconvex objective function.<br />
We also present a stable and efficient numerical implementation. This implementation is based<br />
on the discretize then optimize paradigm and uses a sophisticated computation <strong>of</strong> the discrete<br />
analogues <strong>of</strong> the three invariants <strong>of</strong> the transformation tensor: lengths, areas and volumes. We<br />
show several numerical examples that illustrate the potential <strong>of</strong> the hyperelastic regularizer. We<br />
also show the mass-preserving registration <strong>of</strong> cardiac PET images, where hyperelastic regularization<br />
is mandatory.
364 Section 21: Mathematical image processing<br />
S21.3: Mathematical Image Processing III Wed, 13:30–15:30<br />
Chair: Brigitte Forster-Heinlein S1|03–110<br />
Higher Order Multiphase Image Segmentation and Registration<br />
Stephen Keeling (<strong>Universität</strong> Graz) Schedule<br />
Based upon successes with higher order regularization for image restoration using the Graz developed<br />
Total Generalized Variation (TGV), we seek to develop counterparts for image segmentation<br />
and registration. For segmentation, an image approximation is conceived in terms <strong>of</strong> a sum <strong>of</strong><br />
multiple phase functions which are supported on disjoint sets. The boundaries <strong>of</strong> these supports<br />
define the image edges, and each phase function is smoothed independently on connected components<br />
<strong>of</strong> its support with higher order regularization. By contrast, familiar piecewise constant<br />
segmentations correspond to a very strong first order regularization applied simultaneously to all<br />
connected components <strong>of</strong> the support <strong>of</strong> each phase function. Advantages <strong>of</strong> the proposed segmentation<br />
approach will be elucidated with computational examples. After defining the edge set<br />
in terms <strong>of</strong> the phase function decomposition, images are registered in a contrast invariant fashion<br />
by registering their edge sets. Registration <strong>of</strong> edge sets is performed by transforming each edge set<br />
to a diffuse surface using blurring, and then by registering the diffuse surfaces with progressively<br />
less blurring. Results will be shown for an epicardial matching problem in which Purkinje Fibers<br />
<strong>of</strong> one epicardium are to be mapped to the other. Convergence and discretization issues will also<br />
be addressed.<br />
Inverse source problems and the windowed Fourier transform<br />
Roland Griesmaier, Martin Hanke, Thorsten Raasch (<strong>Universität</strong> Mainz) Schedule<br />
The reconstruction <strong>of</strong> time-harmonic acoustic or electromagnetic sources from measurements <strong>of</strong><br />
the corresponding radiated wave is an ill-posed inverse problem with fascinating applications in<br />
science and technology. We present a new approach to this problem, observing that the windowed<br />
Fourier transform <strong>of</strong> the far field <strong>of</strong> the radiated wave is related to an exponential Radon<br />
transform with purely imaginary exponent <strong>of</strong> a smoothed approximation <strong>of</strong> the source. Based<br />
on this observation we present a filtered backprojection algorithm to recover information on the<br />
unknown source. We discuss this algorithm, consider numerical results, and comment on possible<br />
extensions <strong>of</strong> the reconstruction method to inverse scattering problems.<br />
Adaption <strong>of</strong> Prony’s method for non-standard bases<br />
Thomas Peter, Gerlind Plonka-Hoch (<strong>Universität</strong> Göttingen) Schedule<br />
classification: 41A30, 94A12<br />
Within the last years, there has been an increasing interest in exploiting sparsity <strong>of</strong> solutions in<br />
suitable bases or frames. If a signal f can be represented with M basis functions in a certain basis<br />
B, one could ask, if a number N(M, B) <strong>of</strong> functional values F (f, k), k = 1, . . . , N <strong>of</strong> f is sufficient<br />
to represent the complete signal f. Thereby N(M, B) is only dependent on the order <strong>of</strong> sparsity<br />
M <strong>of</strong> f and the used basis B.<br />
For trigonometric functions this problem can be solved by the Prony-method. In this talk we want<br />
to discuss how this approach can be adapted to other bases. Further we discuss the question <strong>of</strong><br />
what kind <strong>of</strong> functional F will be sufficient to ensure an exact representation <strong>of</strong> f.<br />
Adaptive Total Variation Regularization<br />
Frank Lenzen, Florian Becker, Stefania Petra, Christoph Schnörr (<strong>Universität</strong> Heidelberg) Schedule<br />
For several variational denoising methods, locally adaptive extensions have been proposed in li-
Section 21: Mathematical image processing 365<br />
terature. Most approaches determine adaptivity either by examining the noisy input data in a<br />
preprocessing step or by estimating additional variables along with the denoised image during the<br />
optimization process.<br />
In our work, we model the adaptivity to directly depend on the unknown solution <strong>of</strong> the<br />
optimization problem. We refer to this approach as ’solution-dependent adaptivity’. Our extension<br />
has a significant impact on the theoretical and numerical aspects <strong>of</strong> the optimization process. In<br />
particular, instead <strong>of</strong> a convex optimization problem, which would be obtained with standard<br />
adaptivity, we end up with a quasi-variational inequality to be solved.<br />
In our talk, we will address these theoretical and numerical aspects in detail and provide several<br />
applications <strong>of</strong> solution-dependent adaptivity.<br />
Discrepancies and Halftoning<br />
Manuel Gräf, Daniel Potts (TU Chemnitz), Gabriele Steidl (TU Kaiserslautern) Schedule<br />
The notion <strong>of</strong> discrepancy was originally introduced for measuring the uniformity <strong>of</strong> point distributions.<br />
In this talk we recapitulate some well-known facts in the theory <strong>of</strong> discrepancies, cf. the<br />
book <strong>of</strong> Drmota and Tichy [1], and the relation to the process <strong>of</strong> halftoning an image [2]. In its<br />
generality discrepancy may considered as a notion <strong>of</strong> similarity between two different measures.<br />
In the setting <strong>of</strong> image processing we think <strong>of</strong> an image as a certain measure which we aim to<br />
approximate by a discrete measure. The support <strong>of</strong> the latter measure is given by the stippling<br />
points, which create the halftoning <strong>of</strong> the image. The approximation is achieved by minimizing a<br />
certain discrepancy between these two measures. For a large number <strong>of</strong> points the minimization<br />
<strong>of</strong> the discrepancy is a serious challenge and requires fast algorithms. For that reason we present<br />
an algorithm which is based on the nonlinear conjugate gradient method. The efficiency <strong>of</strong> the<br />
algorithm and the quality <strong>of</strong> the resulting halftoning is demonstrated by several examples.<br />
[1] M. Drmota and R. F. Tichy. Sequences, Discrepancies and Applications. Springer, Berlin,<br />
1997.<br />
[2] M. Gräf, D. Potts, and G. Steidl. Quadrature Errors, Discrepancies and their Relations to<br />
Halftoning on the Torus and the Sphere. Preprint 2011-5, Fakultät für Mathematik, TU<br />
Chemnitz, 2011.<br />
S21.4: Mathematical Image Processing IV Wed, 16:00–18:00<br />
Chair: Martin Welk S1|03–110<br />
Parameterization <strong>of</strong> all (1, 2, 3)-generalized inverses with an application to scattered<br />
data approximation<br />
Dominik Stahl (Fraunh<strong>of</strong>er ITWM), Tobias Damm (<strong>Universität</strong> Bayreuth) Schedule<br />
In our talk we present a method to approximate scattered data based on the lifting scheme.<br />
A central task in the algorithm is the solution <strong>of</strong> a rank-deficient linear least squares problem<br />
minx∈R n �Ax − b�2. The minimal-norm solution, obtainable by the Moore-Penrose-inverse, turns<br />
out to be not a good choice here, since it produces artifacts at the boundary <strong>of</strong> the given domain.<br />
Using extra information on the matrix A, we suggest the construction <strong>of</strong> a different generalized<br />
inverse A ♯ which is much more appropriate to our problem and yields better solutions. Moreover,<br />
our construction leads to a parameterization <strong>of</strong> all (1, 2, 3)-generalized inverses <strong>of</strong> an arbitrary<br />
matrix A. We compare these with respect to their approximation properties in the scattered data<br />
approximation problem.
366 Section 21: Mathematical image processing<br />
Geodesics in shell space<br />
Behrend Heeren (<strong>Universität</strong> Bonn), Martin Rumpf Schedule<br />
The representation and deformation <strong>of</strong> thin shells has been a topic <strong>of</strong> recent research in analysis<br />
as well as in applications ranging from computer graphics to material sciences. Shells are thin,<br />
flexible structures with a high ratio <strong>of</strong> width to thickness which are mathematically represented<br />
by surfaces. Elastic energies resulting from the deformation <strong>of</strong> shells can be described by classical<br />
strain energies or by bending energies if the deformation is solely isometric. We use these<br />
results to introduce a notion <strong>of</strong> time-discrete shortest paths in the space <strong>of</strong> shells, i.e. our timediscrete<br />
geodesic is defined via a variational approach based on elastic matching deformations.<br />
The corresponding deformation energy captures tangential strain as well as general bending.<br />
In order to compute time-discrete geodesics the shells are discretized by parameterized triangular<br />
meshes. We introduce discrete counterparts <strong>of</strong> geometric objects, e.g. the second fundamental<br />
form, by using concepts from Discrete Differential Geometry. The minimization <strong>of</strong> the objective<br />
functional is performed by means <strong>of</strong> hierarchical meshes. Our computational results emphasize in<br />
particular the impact <strong>of</strong> the bending energy on the regularization <strong>of</strong> the geodesic path.<br />
Data de-noising via adaptive wavelet transforms on paths<br />
Dennis Heinen, Gerlind Plonka-Hoch (<strong>Universität</strong> Göttingen) Schedule<br />
De-noising is an important problem in image processing as well as in the situation <strong>of</strong> higher dimensional<br />
data. Consider, we are given a set <strong>of</strong> D-dimensional points (possibly on a non-uniform<br />
grid). Furthermore, suppose there are function values, perturbated by an additive Gaussian noise,<br />
defined on these points.<br />
Our de-noising method works as follows: We successively construct certain path vectors<br />
through the point set. We start from a random point and the choice <strong>of</strong> every following point<br />
depends on the proximity to the previous point on the path and the corresponding function values.<br />
Subsequently, we apply a one-dimensional wavelet shrinkage procedure along the constructed<br />
path vectors.<br />
The method is closely related to the easy path wavelet transform (EPWT) in image approximation<br />
by Plonka (2009) and to the generalized tree-based wavelet transform by Ram et al<br />
(2011). Moreover there is a relation to the diffusion maps framework in dimensionality reduction<br />
(see e.g. Coifman and Lafon (2006)), where random walks on a weighted graph <strong>of</strong> a given data<br />
set are employed.<br />
This talk will explain the proposed data de-noising method with its modifications and also<br />
feature some numerical results.<br />
Tight wavelet frames <strong>of</strong> splines <strong>of</strong> fractional order<br />
Brigitte Forster (TU München), Ole Christensen (Technical University <strong>of</strong> Denmark), Peter Massopust<br />
(Helmholtz Zentrum München) Schedule<br />
Schoenberg’s piecewise polynomial B-splines are traditionally used for multiresolution analyses in<br />
signal and image processing. In recent years, generalizations <strong>of</strong> these function families to fractional<br />
and complex order have been developed, which allow for a better adaptation <strong>of</strong> the analyzing<br />
basis to the image and signal analysis model at hand. Up to now, mainly wavelet bases or the<br />
undecimated wavelet transform have been used. We contribute to the theory in providing a novel<br />
family <strong>of</strong> tight multi-wavelet frames generated by splines <strong>of</strong> fractional order. Our approach is<br />
based on the unitary extension principle and yields closed form high-pass and low-pass filters—<br />
ideal for a fast and simple implementation in Fourier domain.<br />
Image Inpainting and Sparse Approximation<br />
Emily King (<strong>Universität</strong> Bonn), Gitta Kutyniok, Xiaosheng Zhuang (TU Berlin) Schedule
Section 21: Mathematical image processing 367<br />
One main problem in data processing is the reconstruction <strong>of</strong> missing data. In the situation <strong>of</strong><br />
image data, this task is typically termed image inpainting. Recently, inspiring algorithms using<br />
sparse approximations and ℓ1 minimization have been developed and have, for instance, been<br />
applied to seismic images. The main idea is to carefully select a representation system which<br />
sparsely approximates the governing features <strong>of</strong> the original image – curvilinear structures in case<br />
<strong>of</strong> seismic data. The algorithm then computes an image, which coincides with the known part <strong>of</strong><br />
the corrupted image, by minimizing the ℓ1 norm <strong>of</strong> the representation coefficients.<br />
In this talk, we will develop a mathematical framework to analyze why these algorithms<br />
succeed and how accurate inpainting can be achieved. We will first present a general theoretical<br />
approach. Then we will focus on the situation <strong>of</strong> images governed by curvilinear structures, in<br />
which case we analyze both wavelets as well as shearlets as the chosen representation system. Using<br />
the previously developed general theory and methods from microlocal analysis, under certain<br />
conditions on the size <strong>of</strong> the missing parts we will prove that such images can be arbitrarily well<br />
reconstructed.
368 Section 22: Scientific computing<br />
Section 22: Scientific computing<br />
Organizers: Peter Bastian (<strong>Universität</strong> Heidelberg), Axel Voigt (TU Dresden)<br />
S22.1: Particle Methods Tue, 13:30–15:30<br />
Chair: Axel Voigt S1|03–104<br />
Construction and analysis <strong>of</strong> variational multirate integrators<br />
Sina Ober-Blöbaum (TU München/<strong>Universität</strong> Paderborn), Sigrid Leyendecker (<strong>Universität</strong><br />
Erlangen-Nürnberg) Schedule<br />
Variational integrators [2] are based on a discrete variational formulation <strong>of</strong> the underlying<br />
system. The resulting integrators are symplectic and momentum preserving and have an excellent<br />
long-time energy behavior. For the integration <strong>of</strong> systems on different time scales, multirate<br />
methods have been developed [1], where the slow part <strong>of</strong> the system is integrated with a relatively<br />
large step size while the fast part is integrated with a small time step to save function evaluations<br />
and decrease integration time.<br />
In this talk, the construction and an analysis <strong>of</strong> a variational multirate integrator [3] are<br />
presented. Based on a derivation in closed form via a discrete variational principle on a time<br />
grid consisting <strong>of</strong> macro and micro time nodes the resulting integrator is symplectic and momentum<br />
preserving. Its performance and approximation order depending on different discretization<br />
schemes are demonstrated by numerical examples.<br />
[1] C. W. Gear and R. R. Wells, Multirate linear multistep methods. BIT 24 (1984) 484–502.<br />
[2] J. E. Marsden and M. West, Discrete mechanics and variational integrators, Acta Numerica<br />
10 (2001), 357–514.<br />
[3] S. Leyendecker and S. Ober-Blöbaum, A variational approach to multirate integration for<br />
constrained systems, In Proceedings <strong>of</strong> Multibody Dynamics, ECCOMAS Thematic Conference,<br />
Brussels, Belgium, 4-7 July 2011<br />
Molecular dynamics simulation <strong>of</strong> liquid-liquid equilibria using molecular models<br />
adjusted to vapor-liquid equilibrium data<br />
Stefan Eckelsbach, Zhongning Wei, Thorsten Windmann, Jadran Vrabec (<strong>Universität</strong> Paderborn)<br />
Schedule<br />
For the design and optimization <strong>of</strong> chemical process engineering applications, knowledge on vaporliquid<br />
(VLE) and liquid-liquid equilibria (LLE) is crucial. Typically, these thermodynamic properties<br />
are determined by experiment and described by empirical correlations that are subsequently<br />
employed to model distillation or extraction columns. Because <strong>of</strong> the effort that is associated with<br />
the respective experiments, there is significant interest in predictive approaches to VLE and LLE<br />
data. There are numerous fluid mixtures for which both types <strong>of</strong> data are required simultaneously.<br />
However, empirical correlations are not capable to cover VLE and LLE consistently such that<br />
different models and/or different parameters have to be used for a given mixture [1].<br />
Molecular modeling and simulation is a modern approach for the prediction <strong>of</strong> thermodynamic<br />
properties. Being based on mathematical representations <strong>of</strong> the intermolecular interactions, it has<br />
strong predictive capabilities as it adequately covers structure, energetics and dynamics on the<br />
microscopic scale that govern the fluid behavior on the macroscopic scale. In preceding work,
Section 22: Scientific computing 369<br />
molecular models (force fields) were developed to accurately describe pure substance VLE data<br />
and successfully assessed with respect to VLE data <strong>of</strong> multicomponent mixtures [2]. In the present<br />
work, the capability <strong>of</strong> those models to predict the LLE data is studied for the binary mixture<br />
nitrogen + ethane. Systems containing 20000 particles, starting from a random distribution <strong>of</strong><br />
the species, are simulated by molecular dynamics (MD) and phase separation is observed with<br />
a direct method. The calculations are made with the massively parallel MD code ls1 mardyn [3]<br />
that is developed in our group. The program scales linearly with the particle number and has a<br />
very good parallel effciency up to thousands <strong>of</strong> computing cores. It is shown that LLE data can<br />
be determined in this way and that molecular models are capable to consistently cover VLE and<br />
LLE data in good agreement with experiments.<br />
[1] E. Hendriks, et al., Ind. Eng. Chem. Res. 49 (2010), 11131.<br />
[2] J. Stoll, et al., AIChE J. 49 (2003), 2187.<br />
[3] M. Buchholz, et al., J. Comput. Sci. 2 (2011), 124.<br />
Adapting Molecular Dynamics for the Simulation <strong>of</strong> a Lightweight Material<br />
Tobias Steinle, Andrea Walther, Jadran Vrabec (<strong>Universität</strong> Paderborn) Schedule<br />
Increasing awareness <strong>of</strong> climate change and limited fossil fuel supply have the emphasized need for<br />
highly efficient cars and machines. Lightweight materials play an important role in this endeavor.<br />
A problem with these materials is that vibration, for example, caused by an engine, is more likely<br />
to occur than with a traditional solid material <strong>of</strong> the same dimensions.<br />
The Fraunh<strong>of</strong>er Institute for Manufacturing Technologies and Advanced Materials in Dresden<br />
has developed a new kind <strong>of</strong> material that uses embedded hollow spheres filled with particles to<br />
quickly suppress such vibrations. By converting kinetic energy to heat through friction, arising<br />
from the collisions <strong>of</strong> the particles with each other and the hull <strong>of</strong> the sphere, a high dampening<br />
factor is achieved. Thus, wear, tear and noise are reduced.<br />
To numerically simulate the behavior <strong>of</strong> the particles, we use an adapted molecular dynamics<br />
method. These methods are able to simulate large numbers <strong>of</strong> particles, but use a series <strong>of</strong> assumptions<br />
that require changes, such as reflective boundary conditions. The static simulation<br />
volume <strong>of</strong> molecular simulations is adapted to allow for a deformation <strong>of</strong> the hull <strong>of</strong> the sphere.<br />
Additionally, friction and gravity are introduced.<br />
Some results <strong>of</strong> these dynamic simulations are presented.<br />
Hybrid GPU Accelerated Mesoscopic Particle Simulation<br />
Katrin Fischer, Georg-Peter Ostermeyer (TU Braunschweig) Schedule<br />
During the past few years, the performance enhancement <strong>of</strong> existing algorithm implementations<br />
through massive parallelization on modern graphics processing units (GPU) based on NVIDIA’s<br />
Compute Unified Device Architecture (CUDA) has become very popular in a large variety <strong>of</strong> applications.<br />
Particle methods e.g. are dedicated for parallelization because <strong>of</strong> their basic algorithmic<br />
structure. The neighbourhood search, the computation <strong>of</strong> interaction forces and the final state<br />
update via time integration can be parallelized directly among the particles.<br />
In order to evaluate the potential <strong>of</strong> such a GPU implementation compared to the single CPU<br />
execution, a parallel and hybrid implementation with OpenMP and CUDA has been developed<br />
for a special particle method, the so-called mesoscopic particle method. This method takes into<br />
account mechanical as well as thermodynamical degrees <strong>of</strong> freedom. On the basis <strong>of</strong> the hybrid
370 Section 22: Scientific computing<br />
implementation, the performance <strong>of</strong> different types <strong>of</strong> execution architectures (sequential on single<br />
CPU core, parallel on multi-core CPU, parallel on GPU) can be determined and compared.<br />
This talk gives an introduction to the developed parallel and hybrid mesoscopic particle implementation<br />
as well as some performance results for different CPUs and different generations <strong>of</strong><br />
NVIDIA GPUs.<br />
Counting Droplets: A solver for the droplet population balance equation<br />
Timo Wächtler (TU Kaiserslautern), Jörg Kuhnert (Fraunh<strong>of</strong>er Institut für Techno- und Wirtschaftsmathematik),<br />
Menwer Attarakih (CAPE The University <strong>of</strong> Jordan), Axel Klar (TU Kaiserslautern)<br />
Schedule<br />
Liquid-Liquid-Extractions is one <strong>of</strong> the basic operations in chemical engineering and the simulation<br />
<strong>of</strong> those processes provides several numerical difficulties. From the point <strong>of</strong> CFD, a dispersive<br />
flow has to be resolved numerically. Assuming, that the droplets <strong>of</strong> the dispersed phase <strong>of</strong> this<br />
flow are distributed statistically, one can formulate an equation for the distribution function<br />
f = f(t, x, v) for the droplets depending on time, space and the droplet volume<br />
∂tf + ∇x · (vdf − D∇xf) = + 1/2 ·<br />
�<br />
vmax<br />
0<br />
− f(t, x, v)<br />
ω(v − v ′ , v ′ )f(t, x, v − v ′ )f(t, x, v ′ )dv ′<br />
�<br />
vmax<br />
− Γ(v) · f(t, x, v) +<br />
v<br />
ω(v, v ′ )f(t, x, v ′ )dv ′<br />
�<br />
vmax<br />
v<br />
Γ(v ′ ) · β(v|v ′ )f(t, x, v ′ )dv ′ .<br />
The droplet information is transported due to the droplet velocity vd and diffusion D. The right<br />
hand side represents the births and deaths <strong>of</strong> droplets due to aggregation and breakage events. This<br />
contribution will present a moment based numerical method to deal with the kind <strong>of</strong> equations<br />
above and is going to involve this method in a two-phase flow simulation using the Finite Pointset<br />
Method. The presentation will be closed with an exposition <strong>of</strong> 2D test problems for special cases<br />
<strong>of</strong> (1).<br />
[1] T. Wächtler, J. Kuhnert, M.M. Attarakih et. al<br />
The Normalized Qudrature Method <strong>of</strong> Moments coupled with Finite Pointset Method<br />
Proc. <strong>of</strong> the International Conference on Particle-based method Fundamentals and Applications<br />
Barcelona, Spain, 26-28 October 2011<br />
[2] C.Drumm, S.Tiwari, J.Kuhnert, H.-J. Bart, Finite pointset method for simulation <strong>of</strong> the<br />
liquid-liquid flow field in an extractor, Computers & Chemical Engineering 32 (2008), 2946-<br />
2957<br />
S22.2: PDE Applications and Fast Solvers Tue, 16:00–18:00<br />
Chair: Jörg Wensch S1|03–104<br />
Parallel simulation <strong>of</strong> s<strong>of</strong>t biological tissue<br />
Oliver Rheinbach, (TU Chemnitz), Sarah Brinkhues, Axel Klawonn, Jörg Schröder (<strong>Universität</strong><br />
Duisburg-Essen) Schedule<br />
(1)
Section 22: Scientific computing 371<br />
Numerical simulation <strong>of</strong> s<strong>of</strong>t biological tissue based on patient specific data is demanding with<br />
respect to the modeling, the discretization, as well as the solution <strong>of</strong> the arising nonlinear elasticity<br />
problems. In this talk, we present our approach to a s<strong>of</strong>tware environment composed <strong>of</strong> a nonlinear<br />
finite element code (FEAP) and a parallel domain decomposition solver (FETI-DP method). We<br />
also present parallel results obtained on a Cray XT6m.<br />
Comparison <strong>of</strong> variational and non-variational multigrid methods based on nonnested<br />
meshes<br />
Thomas Dickopf, Rolf Krause (University <strong>of</strong> Lugano) Schedule<br />
This talk is about two classes <strong>of</strong> multigrid methods based on non-nested meshes for the fast<br />
solution <strong>of</strong> partial differential equations on complicated domains. For finite element discretizations<br />
with unstructured meshes in 3D, these methods combine the flexibility <strong>of</strong> algebraic multigrid<br />
methods with the efficiency <strong>of</strong> geometric multigrid methods by a flexible choice <strong>of</strong> the coarse<br />
meshes. We present a detailed performance analysis comparing the variational setting, where the<br />
coarse spaces are built by recursively considering the ranges <strong>of</strong> suitable prolongation operators in<br />
the next finer space, and the non-variational (“auxiliary space”) setting. In particular, numerical<br />
studies <strong>of</strong> specially designed mesh hierarchies, which are structured but non-nested, provide new<br />
insight into the dependence <strong>of</strong> the convergence on the mesh size ratios.<br />
A Three-Dimensional Panel Method for the Simulation <strong>of</strong> Sheet Cavitation in Marine<br />
Propeller Flows<br />
M. Bauer, M. Abdel-Maksoud (TU Hamburg) Schedule<br />
This paper presents the development and application <strong>of</strong> a three-dimensional panel method based<br />
on potential theory for the modeling and simulation <strong>of</strong> sheet cavitation on marine propellers.<br />
In potential theory the governing equations are derived from the assumption that the flow is<br />
irrotational, incompressible and inviscid combined with adequate boundary conditions on the<br />
body and cavity surface. The resulting boundary value problem is solved numerically by means<br />
<strong>of</strong> a panel method where the body surface is discretized into flat quadrilateral elements. The<br />
advantage <strong>of</strong> the developed panel method is its short computation time which allows for a wide<br />
rage <strong>of</strong> parameter variations in the design procedure.<br />
The present work is motivated by the difficulties which occur in the propeller flow under cavitating<br />
conditions. Cavitation is a physical effect where the pressure falls below the vapour pressure such<br />
that a vapour region occurs in the flow. Cavitation influences the flow characteristics on propeller<br />
blades significantly and can lead to a decrease <strong>of</strong> propeller thrust or in sever cases cause material<br />
damages on propeller blades. The most relevant features <strong>of</strong> the cavitation model are described in<br />
the first part <strong>of</strong> the paper. The model is implemented in the in-house boundary element code -<br />
panMARE - which is based on a first-order panel method and is able to simulate potential flows<br />
in marine applications [1].<br />
In the second part <strong>of</strong> the paper the model is validated by representative two- and three-dimensional<br />
examples. Validation studies refer to the results obtained by other authors, e.g. published in [2].<br />
To demonstrate the abilities <strong>of</strong> the developed method a marine propeller is simulated under<br />
cavitating conditions and the influence <strong>of</strong> cavitation on propeller’s performance is outlined.<br />
[1] J. Hundemer, M. Abdel-Maksoud, Prediction <strong>of</strong> tip vortex cavitation inception on marine<br />
propellers at an early design stage, 7th International Symposium on Cavitation, Ann Arbor,<br />
(2009).<br />
[2] A. K. Singhal, M. M. Athavale, H. Li, Y. Jiang, Mathematical Basis and Validation <strong>of</strong> the<br />
Full Cavitation Model, Journal <strong>of</strong> Fluids Engineering, Vol. 124, (2002), p. 617-624.
372 Section 22: Scientific computing<br />
Simulation <strong>of</strong> Non-Newtonian Fluid Flow<br />
A. Naumann, J. Wensch (TU Dresden) Schedule<br />
The simulation <strong>of</strong> non-Newtonian fluids is a challenging task in computational rheology. The<br />
dynamics <strong>of</strong> the fluid are described by the Navier-Stokes equations. Whereas Newtonian fluids<br />
have constant viscosity, in non-Newtonian fluids a variety <strong>of</strong> models for the viscous terms are<br />
available. Viscosity may depend on the shear rate or even on the deformation history. The latter<br />
leads to models for the stress-strain rate relation analogous to viscous solids. The corresponding<br />
evolution equations <strong>of</strong>ten constitute a stiff problem.<br />
The proposed numerical scheme is based on finite elements with a semi-Lagrangian discretization<br />
<strong>of</strong> the advection operator The combination <strong>of</strong> a transport process and stiff reaction terms<br />
requires special care to avoid restrictive stepsize limitations.<br />
Stability analysis <strong>of</strong> solid-state lasers regarding thermal lensing effect<br />
Thomas Graupeter, Christoph Pflaum (<strong>Universität</strong> Erlangen) Schedule<br />
The thermal lensing effect in the crystal influences the stability <strong>of</strong> solid-state lasers. The deformation<br />
<strong>of</strong> the end faces <strong>of</strong> the crystal and the temperature dependence <strong>of</strong> the refraction index<br />
causes this effect. The photoelastic effect produced by thermal induced stress in the crystal has<br />
also an influence. For high power lasers and for lasers with a radially polarized laser beam the<br />
analysis <strong>of</strong> the photoelastic effect is important. We use FE model to calculate the deformation,<br />
heat and stress distribution in the laser crystal with high accuracy in this work. Using the calculated<br />
stress distribution we also simulated the refraction index anisotropy with respect to the<br />
crystal orientation. We can study stability <strong>of</strong> laser resonators for both radially and azimuthally<br />
polarized laser beam, as a result <strong>of</strong> our simulation.<br />
S22.3: Efficient Numerical Schemes for Nonlinear Mechanics Thu, 13:30–15:30<br />
Chair: Peter Bastian S1|03–104<br />
On the superlinear convergence in computational elasto-plasticity<br />
Christian Wieners (KIT) Schedule<br />
We consider the convergence properties <strong>of</strong> return algorithms for a large class <strong>of</strong> rate-independent<br />
plasticity models. Based on recent results for semismooth functions, we can analyze these algorithms<br />
in the context <strong>of</strong> semismooth Newton methods guaranteeing local superlinear convergence.<br />
This recovers results for classical models but also extends to general hardening laws, multi-yield<br />
plasticity, and to several non-associated models. The superlinear convergence is also numerically<br />
shown for a large-scale parallel simulation <strong>of</strong> Drucker-Prager elasto-plasticity and an example for<br />
the modified Cam-clay model.<br />
Dual weighted residual error control for frictional contact problems<br />
Andreas Rademacher (TU Dortmund), Andreas Schröder (HU Berlin) Schedule<br />
Frictional contact problems play an important role in the modeling <strong>of</strong> mechanical engineering processes,<br />
for instance in forming processes. Variational formulations <strong>of</strong> contact problems are given,<br />
e.g., via the introduction <strong>of</strong> Lagrange multipliers capturing the geometrical and frictional contact<br />
conditions. A low-order finite element dicsretization <strong>of</strong> such mixed approaches is described in [1],<br />
where the displacement field is discretized by the usual low-order conforming ansatz and the Lagrange<br />
multipliers via piecewise constant functions on coarsened boundary meshes ensuring the<br />
stability <strong>of</strong> the mixed method.
Section 22: Scientific computing 373<br />
In the simulation <strong>of</strong> engineering processes, adaptive methods based on a posteriori error estimates<br />
become more and more indispensable, because they automatically solve the given problem<br />
as accurate as needed while minimizing the overall numerical effort. One <strong>of</strong> the most popular<br />
techniques from the last decades to derive error estimates for user-defined, probably non-linear<br />
error measures (quantities <strong>of</strong> interest) is known as the dual weighted residual method (DWR). It<br />
relies on representing the error in terms <strong>of</strong> the solution <strong>of</strong> a dual problem. This note focusses on<br />
the application <strong>of</strong> the DWR method for quasi static contact problems. In extension <strong>of</strong> the results<br />
presented in [2,3], the error is measured with respect to quantities <strong>of</strong> interest in the displacement<br />
field as well as in the Lagrange multipliers to control the error <strong>of</strong> the contact forces directly.<br />
Using a mixed dual problem, one obtains the general residuals <strong>of</strong> the DWR method and a term<br />
for the error in the contact conditions, which are numerically evaluated by suitable interpolation<br />
techniques. Numerical results substantiate the applicability <strong>of</strong> the presented techniques.<br />
[1] A. Schröder, H. Blum, H. Kleemann, A. Rademacher, Mixed FEM <strong>of</strong> higher-order for contact<br />
problems with friction, J. Num. Anal. & Model. 8 (2011) 302-323.<br />
[2] A. Rademacher, Adaptive finite element methods for nonlinear hyperbolic problems <strong>of</strong> second<br />
order, Dissertation, <strong>Technische</strong> <strong>Universität</strong> Dortmund, 2009.<br />
[3] A. Schröder, A. Rademacher, Goal-oriented error control in adaptive mixed FEM for Signorini’s<br />
problem, Comput. Methods Appl. Mech. Engng. 200 (2011) 345-355.<br />
A posteriori control <strong>of</strong> modeling and discretization errors in finite elastoplasticity<br />
André Große-Wöhrmann, Heribert Blum (TU Dortmund) Schedule<br />
The concept <strong>of</strong> adaptive error control for finite element Galerkin discretizations has more recently<br />
been extended from the pure treatment <strong>of</strong> the discretization errors [1], [3] also to the<br />
control <strong>of</strong> modeling errors [5]. These techniques can be employed for a rigorous justification <strong>of</strong><br />
the local choice <strong>of</strong> the model out <strong>of</strong> a given hierarchy with increasing complexity. In the present<br />
paper the concept is exemplified by a hierarchy <strong>of</strong> elastoplasticity models [2] including kinematic<br />
(Armstrong-Frederick-) hardening, scalar- and tensor-valued damage [6] and a Taylor model <strong>of</strong><br />
polycrystals. Significant reduction <strong>of</strong> the computational complexity shall be achieved by a proper<br />
choice <strong>of</strong> the model in different subdomains, automatically chosen by the error estimators. The<br />
method is applied to finite element simulations [4] <strong>of</strong> metal forming.<br />
This project is supported by the Deutsche Forschungsgemeinschaft (DFG) under grant SFB-TR<br />
73 ”Sheet-Bulk Metal Forming”(https://www.tr-73.de)<br />
[1] M. Ainsworth, J. T. Oden: A Posteriori Error Estimation in Finite Element Analysis, Wiley<br />
2000.<br />
[2] F. Armero, C. Zambrana-Rojas: Volume-preserving energy-momentum schemes for isochoric<br />
multiplicative plasticity, Comput. Methods Appl. Mech. Engrg. 196 (2007) 4130-4159.<br />
[3] R. Becker, R. Rannacher: An optimal control approach to a posteriori error estimation in finite<br />
element methods, Acta Numerica, Vol. 10, pp. 1-102, edited by A. Iserles, Ed., Cambridge<br />
Univ. Press, 2002.<br />
[4] W. Bangerth, R. Hartmann and G. Kanschat: deal.II Differential Equations Analysis Library,<br />
Technical Reference: http:// www.dealii.org.
374 Section 22: Scientific computing<br />
[5] M. Braack, A. Ern: A posteriori control <strong>of</strong> modeling errors and discretization errors, Multiscale<br />
Model. Simul. Vol. 1, No. 2, pp 221-238, 2003.<br />
[6] A. Menzel, P. Steinmann, A theoretical and computational framework for anisotropic continuum<br />
damage mechanics at large strains, Int. J, Solids Structures 38 (2001) 9505-9523.<br />
On the dynamic behaviour <strong>of</strong> fluid-saturated soil within the framework <strong>of</strong> elastoplasticity<br />
Maik Schenke, Bernd Markert, Wolfgang Ehlers (<strong>Universität</strong> Stuttgart) Schedule<br />
Phenomena related to porous media dynamics, such as wave propagation and liquefaction, are encountered<br />
in many engineering applications, especially, in geomechanics and earthquake engineering.<br />
Drawing our attention to fluid-saturated granular materials with heterogeneous microstructures,<br />
the modelling is carried out within a continuum-mechanical framework by exploiting the<br />
well-established macroscopic Theory <strong>of</strong> Porous Media (TPM) together with thermodynamically<br />
consistent constitutive equations. In this regard, the solid skeleton is described within the<br />
framework <strong>of</strong> elasto-plasticity [1, 2].<br />
The underlying equations are discretised and implemented into the coupled porous-media finiteelement<br />
solver PANDAS. A general interface to the well-established Abaqus finite-element package<br />
allows for a straight-forward usage <strong>of</strong> PANDAS material models within Abaqus, thereby exploiting<br />
the advantages <strong>of</strong> Abaqus, such as the graphical user interface, the contact algorithms and the<br />
possibility to deal with large problems through parallelisation. Moreover, the coupling introduces<br />
a convenient environment to define new material models through PANDAS. In conclusion, the<br />
interface allows to define complex intial-boundary-value problems through Abaqus, but involves<br />
state-<strong>of</strong>-the-art material models <strong>of</strong> PANDAS.<br />
The underlying interface will be used to analyse the wave propagation, through fluid-saturated<br />
soils, which is caused by transient loading conditions as they occur, for instance, during<br />
earthquakes or geotechnical installation processes.<br />
[1] Y. Heider, B. Markert, W. Ehlers, Dynamic wave propagation in infinite saturated porous<br />
media half spaces. Comput. Mech., DOI 10.1007/s00466-011-0647-9<br />
[2] W. Ehlers, O. Avci, Stress-dependent hardening and failure surfaces <strong>of</strong> dry sand. Int. J.<br />
Numer. Anal. Meth. Geomech., in press 2011.<br />
Cosserat rod and string models for viscous jets in rotational spinning processes<br />
Walter Arne (<strong>Universität</strong> Kassel), Nicole Marheineke (<strong>Universität</strong> Erlangen-Nürnberg), Raimund<br />
Wegener (Fraunh<strong>of</strong>er Institut für Techno- und Wirtschaftsmathematik) Schedule<br />
We present asymptotic Cosserat rod and string models for the simulation <strong>of</strong> slender viscous jets.<br />
In the set-up <strong>of</strong> rotational spinning processes we examine the models analytically and numerically<br />
with respect to their applicability/validity and efficiency. The string models are asymptotic limits<br />
<strong>of</strong> the rod in terms <strong>of</strong> a vanishing slenderness parameter (slender-body theory). They consist <strong>of</strong><br />
smaller systems <strong>of</strong> equations, but as a result <strong>of</strong> a singular asymptotic perturbation their applicability<br />
is restricted to certain parameter regimes – in contrast to the complexer and hence superior<br />
Cosserat rod. We investigate the existence regimes <strong>of</strong> two string models that differ in the closure<br />
conditions, determine their transition hyperplane numerically and present analytical results for
Section 22: Scientific computing 375<br />
low and high Reynolds number limits.<br />
S22.4: Scientific Computing Thu, 16:00–18:00<br />
Chair: Peter Bastian S1|03–104<br />
Computing roots for the analytic modeling <strong>of</strong> guided waves in acoustic waveguides<br />
Andrea Walther, Fabian Bause, Bernd Henning (<strong>Universität</strong> Paderborn) Schedule<br />
Computer aided simulation <strong>of</strong> guided acoustic waves in single- or multilayered waveguides is an<br />
essential tool for several applications <strong>of</strong> acoustics and ultrasonics (i.e. pipe inspection, noise reduction).<br />
To simulate wave propagation in geometrically simple waveguides (plates or rods), one<br />
may employ the analytical global matrix method [1]. This requires the computation <strong>of</strong> all roots <strong>of</strong><br />
the determinate <strong>of</strong> a certain submatrix. The evaluation <strong>of</strong> all real or even complex roots is actually<br />
the methods most concerning restriction. Previous approaches based on so called mode-tracers<br />
which use the physical phenomenon that solutions (roots) appear in a certain pattern (waveguide<br />
modes) and thus use known solutions to limit the root finding algorithms searchspace with respect<br />
to consecutive solutions. As the limitation <strong>of</strong> the searchspace might be unstable in some cases,<br />
we propose to replace the mode-tracer with a suitable version <strong>of</strong> an interval Newton method<br />
based on Intlab [2]. To apply this interval based method, we extended the interval and derivative<br />
computation provided by Intlab such that corresponding information is also available for Bessel<br />
functions used in the circular model (rods) <strong>of</strong> acoustic waveguides. We present numerical results<br />
<strong>of</strong> a simple acoustic waveguide and discuss extensions required for more realistic scenarios.<br />
[1] Pavlakovic, B., Lowe, M. J. S.: Disperse: A System for Generating Dispersion Curves. Users<br />
Manual. Non-Destructive Testing Laboratory, Imperial College London, 2003<br />
[2] INTLAB - INTerval LABoratory, http://www.ti3.tu-harburg.de/rump/intlab/<br />
Discrete Willmore Flow on surfaces using Subdivision<br />
Sara Grundel (MPI Magdeburg), Thomas Yu, Jingmin Chen (Drexel University) Schedule<br />
Gradient flows on surfaces play a role in a wide range <strong>of</strong> applications, for example in biological<br />
modeling, computer graphics and shape optimization. We present a new approach to compute<br />
a discrete gradient flow by using a newly developed C 2 smooth subdivision algorithm. We will<br />
briefly present the subdivision algorithm and how we can use it to compute any gradient flow. We<br />
will study the discrete Willmore flow and its application in detail. One <strong>of</strong> the advantages <strong>of</strong> this<br />
subdivision approach is that it can be refined adaptively very easily. In this approach the surface<br />
is given explicitly as a triangular mesh.<br />
Flow Modeling in Rock Fracture for Long Time Simulation <strong>of</strong> Geothermal Reservoirs<br />
Georg-Peter Ostermeyer, Tarin Srisupattarawanit (Institute <strong>of</strong> Dynamics and Vibrations) Schedule<br />
The exploitation <strong>of</strong> geothermal power is an energy source with great potential for the future.<br />
But the exploration and development <strong>of</strong> deep geothermal energy is connected with high cost and<br />
risk, these require a reliable numerical prediction. The analysis <strong>of</strong> geothermal reservoir is usually<br />
interested in long time physical properties (e.g. 50-100 years). Typical CFD simulation tool could<br />
be used somehow, but the computational effort may be limited due to incompatibility <strong>of</strong> small<br />
scale heterogeneities.<br />
Here we developed flow modeling in rock fracture, which describe the different characteristic<br />
flow in different dimension. The fluid flow in tube is described by one dimensional flow (1D flow),
376 Section 22: Scientific computing<br />
while flow in rock fracture is modeled as two dimensional flow (2D flow) on fracture plane. The<br />
1D flow in tube and 2D flows in fracture are coupled to represent three dimensional flows in<br />
reservoirs. The solution <strong>of</strong> coupling system (1D and 2D flow) is obtained by iterative procedure,<br />
while the flow inside 2D fracture is calculated by cellular automaton. This algorithm is relatively<br />
fast for calculating flow inside geothermal reservoir, especially for long time physical flow.<br />
Kombinierte Identifikation von Material- und Geometrieparametern bei strukturierten<br />
Probekörpern<br />
Hans Wulf (TU Chemnitz), Dirk Schellenberg (Deutsches Institut für Kautschuktechnologie), Jörn<br />
Ihlemann (TU Chemnitz ) Schedule<br />
Aus experimentell ermittelten inhomogenen Feldgrößen können Materialparameter mit Hilfe eines<br />
Optimierungsverfahrens gewonnen werden, das FEM-Berechnungen als Unterroutine verwendet.<br />
In der Regel werden dabei die Materialparameter innerhalb des Probekörpers als konstant vorrausgesetzt.<br />
Diese Annahme ist nicht immer gerechtfertigt. Ortsabhängige Materialparameter<br />
treten beispielsweise in Bauteilen nach Massivumformung aufgrund lokal unterschiedlicher Kornfeinung<br />
oder in mehrphasigen biologischen Geweben auf. In diesem Fall muss statt eines einzelnen<br />
Parametersatzes eine Verteilung von Parametern über dem Ort ermittelt werden.<br />
Ein einfaches Beispiel stellt ein aus zwei Arten biologischer Gewebe bestehender Probekörper<br />
dar. Es wird dabei angenommen, dass das betrachtete Gebiet sich in zwei zusammenhängende<br />
Bereiche mit konstantem Materialverhalten unterteilen lässt. Allerdings ist die Form der Gebiete,<br />
speziell die Grenzfläche zwischen den Gebieten, unbekannt. Als St<strong>of</strong>fgesetz wird ein einfaches<br />
Gesetz für poröse Materialien verwendet. Das Ziel der Identifikation besteht darin, die Materialparametersätze<br />
in beiden Gebieten sowie die Form der Gebiete zu bestimmen. Die Form der<br />
Grenzfläche zwischen den Gebieten wird mit einem Non-Rational Uniform B-Spline (NURBS)<br />
parametrisiert. Außerdem wird ein Verfahren für die Generierung von entsprechend angepassten<br />
FEM-Netzen vorgestellt. Insgesamt sollen 6 Materialparameter und 5 Geometrieparameter bestimmt<br />
werden. Es wird ein Algorithmus gezeigt, welcher beide Parameterarten gleichzeitig in<br />
einer kombinierten Optimierung identifiziert.<br />
Um das Verfahren zu testen, wurden zwei Indentationsversuche simuliert und die Reaktionskraft<br />
am Indenter sowie die Verformung der Außenkontur berechnet. Die Resultate wurden<br />
mit einem additiven Gaußschen Rauschen von 5% belegt und werden als synthetische Messwerte<br />
verwendet. Auf Basis dieser Daten werden alle 11 Parameter mit einer einzelnen gekoppelten<br />
Optimierung identifiziert.<br />
The synthesis <strong>of</strong> adequate mathematical description as special inverse problem<br />
Yu.Menshikov (Dnepropetrovsk University, Ukraine) Schedule<br />
The main problem <strong>of</strong> mathematical modeling is the construction (synthesis) <strong>of</strong> mathematical<br />
model (MM) <strong>of</strong> motion <strong>of</strong> real dynamic system which in aggregate with model <strong>of</strong> external load<br />
(MEL) gives the adequate to experimental observations the results <strong>of</strong> mathematical modeling.<br />
Such pair (MM+MEL) was named as adequate mathematical description. In paper one way <strong>of</strong><br />
solution <strong>of</strong> such problem was considered which based on identification method <strong>of</strong> external loads.<br />
These problems are inverse problems and they have typical properties <strong>of</strong> incorrect problems.<br />
The regularization methods are being used for obtaining the stable solutions. But there are some<br />
features. For example, the size <strong>of</strong> error <strong>of</strong> approximate solution <strong>of</strong> inverse problem has not essential<br />
importance for future use. The error <strong>of</strong> MM has not to be taken into account under calculations in<br />
these problems. It is necessary the use <strong>of</strong> special filtration <strong>of</strong> initial data for decrease <strong>of</strong> influence<br />
<strong>of</strong> uncontrollable inaccuracy into initial data.<br />
For expansion <strong>of</strong> area <strong>of</strong> use <strong>of</strong> approximate solution the method <strong>of</strong> choice <strong>of</strong> special operator
Section 22: Scientific computing 377<br />
was suggested. The different variants <strong>of</strong> choice <strong>of</strong> MEL which are depending from final goals <strong>of</strong><br />
mathematical modeling (modeling <strong>of</strong> given motion <strong>of</strong> system, different estimation <strong>of</strong> responses<br />
<strong>of</strong> dynamic system, modeling <strong>of</strong> best forecast <strong>of</strong> system motion, the most stable model to small<br />
change <strong>of</strong> initial data, unitary model) are considered.<br />
In paper some real calculations <strong>of</strong> adequate mathematical descriptions <strong>of</strong> real dynamic systems<br />
were executed using <strong>of</strong> which give adequate results <strong>of</strong> mathematical modeling.<br />
Failpro<strong>of</strong> GRID-enabled framework for large-scale computations in mechanics<br />
Andrei V. Zinchenko (Institute <strong>of</strong> Transport Systems and Technologies, NAS <strong>of</strong> Ukraine), Sergei<br />
N. Kodak (Dnepropetrovsk National University) Schedule<br />
Last time the Grid computing is gaining a lot <strong>of</strong> attention within the scientific community. Unlike<br />
to chemistry, molecular biology and nuclear physics applications, Grid technologies just have<br />
been finding their way in fields <strong>of</strong> mechanical engineering, material modeling, computational fluid<br />
dynamics. Due to intensive enough data exchange between nodes the Grid implementation <strong>of</strong><br />
PDE based mechanical problems in some cases is really difficult especially in scavenging Grid<br />
infrastructure.<br />
Based <strong>of</strong> ideas <strong>of</strong> BOINC open source projects authors have developed VALERIA Grid middleware<br />
capable for implementation in scavenging or computational Grid environment. The distinctive<br />
features <strong>of</strong> developed middleware are the dynamic topology scan, failover procedure and<br />
automatic reconfiguration <strong>of</strong> computational resources based on keep-alive tests. The failover procedure<br />
is specially designed to be time-effective and suitable for use inside iteration <strong>of</strong> distributed<br />
PDE solvers with message passing interface.<br />
VALERIA middleware consists <strong>of</strong> control router hosted configuration, topology and cryptographic<br />
engines and the control interface. Router maintains communication with hierarchy <strong>of</strong><br />
computational clusters or nodes as well as the database server provides initial data and results<br />
storage. For redundancy VALERIA Grid infrastructure could be configured with several backup<br />
routers. The primary router also hosts job control and dispatch service. Computational nodes<br />
must have loader s<strong>of</strong>tware installed capable <strong>of</strong> executing piece <strong>of</strong> distributed code. Loaders are<br />
now available for Win32 and Linux environments.<br />
First attempts to implement the finite volume PDE solver showed essential limitations <strong>of</strong> scavenging<br />
Grid for the fluid mechanics problems. Distributed CFD code requires huge memory allocations<br />
on computational nodes. This fact induced lots <strong>of</strong> node reconfigurations and significantly<br />
slowed down the calculation speed in our experiments. Finally we have moved from scavenging<br />
to computational Grid infrastructure.<br />
Overall performance was tested on a cluster consists <strong>of</strong> four SONY PlayStation3 computational<br />
nodes with Linux installed. The prime calculation tests gave 470 times speed up in comparison<br />
with Athlon X2 2,5GHz. The next step will be computational experiments with distributed PDE<br />
solvers.
378 Section 23: Applied operator theory<br />
Section 23: Applied operator theory<br />
Organizers: Jussi Behrndt (TU Graz), Carsten Trunk (TU Ilmenau)<br />
S23.1: Spectral Theory in Hilbert and Krein Spaces Tue, 13:30–15:30<br />
Chair: Carsten Trunk S1|03–107<br />
Dirac-Krein operators on star graphs<br />
Vadim Adamyan (Odessa National I.I. Mechnikov University) Schedule<br />
The talk focuses on the description <strong>of</strong> the spectrum <strong>of</strong> a self-adjoint Dirac-Krein differential<br />
operator<br />
�<br />
0<br />
H = −<br />
1<br />
�<br />
−1 d<br />
0 dx +<br />
�<br />
p(x)<br />
q(x)<br />
�<br />
q(x)<br />
,<br />
−p(x)<br />
on an n-pointed compact star graph Γ, where p(x), q(x) are continuous real-valued functions on<br />
the edges <strong>of</strong> Γ. The operator H is considered as a perturbation <strong>of</strong> the orthogonal sum H(12) <strong>of</strong> the<br />
self-adjoint Dirac-Krein operators on the disjoint edges <strong>of</strong> Γ, defined on two-component vector<br />
functions with zero first component at one end point and zero second component at the other<br />
end point <strong>of</strong> each edge <strong>of</strong> Γ; the domain <strong>of</strong> H is assumed to consist <strong>of</strong> all vector functions the<br />
first components <strong>of</strong> which coincide at the unique vertex <strong>of</strong> the star graph where all edges touch,<br />
while the boundary conditions at the pendent ends <strong>of</strong> all edges are the same as for H(12). As a<br />
main tool we use Krein’s resolvent formula for the resolvent kernels (Green’s functions) <strong>of</strong> H(12)<br />
and H. We prove that the set <strong>of</strong> common eigenvalues <strong>of</strong> H and H(12) coincides with the set <strong>of</strong><br />
multiple eigenvalues <strong>of</strong> H(12), but their multiplicities as eigenvalues <strong>of</strong> H decreases by one. We<br />
also prove that the sets <strong>of</strong> simple eigenvalues <strong>of</strong> H and the set <strong>of</strong> all eigenvalues <strong>of</strong> H(12) interlace.<br />
The asymptotic behaviour <strong>of</strong> the number <strong>of</strong> eigenvalues <strong>of</strong> H, multiplicities taken into account,<br />
on spectral intervals (−Λ, 0) and (0, Λ) as Λ → ∞ is derived.<br />
The talk is based on a joint work with Heinz Langer and Christiane Tretter.<br />
Spectral functions <strong>of</strong> products <strong>of</strong> selfadjoint operators<br />
Tomas Ya. Azizov, Mikhail Denisov (Voronezh State University), Friedrich Philipp (TU Berlin)<br />
Schedule<br />
Given two possibly unbounded selfadjoint operators A and G such that the resolvent sets <strong>of</strong> AG<br />
and GA are non-empty, it is shown that the operator AG has a spectral function on R with<br />
singularities if there exists a polynomial p �= 0 such that the symmetric operator Gp(AG) is<br />
non-negative. We apply this result to weighted Sturm-Liouville problems.<br />
Variation <strong>of</strong> discrete spectra <strong>of</strong> non-negative operators in Krein spaces<br />
Jussi Behrndt (TU Graz), Leslie Leben (TU Ilmenau), Friedrich Philipp (TU Berlin) Schedule<br />
Considered is an additive perturbation <strong>of</strong> a bounded non-negative operator A in a Krein space<br />
with a likewise bounded non-negative operator C from a Schatten-von Neumann ideal <strong>of</strong> order<br />
p, such that ker C = ker C 2 and 0 is not a singular critical point <strong>of</strong> C. We show a qualitative<br />
result on the variation <strong>of</strong> the discrete spectra <strong>of</strong> the unperturbed and perturbed operator, that<br />
is, given a finite union ∆ <strong>of</strong> open intervals with 0 /∈ ∆, there exist enumerations (αn) and (βn) <strong>of</strong><br />
the discrete eigenvalues <strong>of</strong> A and B := A + C in ∆ such that<br />
(βn − αn) ∈ ℓ p .
Section 23: Applied operator theory 379<br />
Sign preserving Perturbations <strong>of</strong> Eigenvalues<br />
Roland Möws (TU Ilmenau), Jussi Behrndt (TU Graz), Carsten Trunk (TU Ilmenau) Schedule<br />
We consider two operators A and B which are self-adjoint in a Krein space (K, [·, ·]) and whose<br />
resolvent difference is one-dimensional, i.e.<br />
dim ran � (A − λ) −1 − (B − λ) −1� = 1, λ ∈ ρ(A) ∩ ρ(B).<br />
It is well-known that the algebraic eigenspace corresponding to a real discrete eigenvalue <strong>of</strong> A<br />
(or B), equipped with [·, ·], is a Krein space. The main result is the following: Assume that there<br />
exists a domain Ω ⊂ C in which A (or, equivalently, B) has similar spectral properties as a<br />
definitizable operator and that A satisfies a certain minimality condition. Moreover, let λ1 and λ2<br />
be two discrete eigenvalues <strong>of</strong> A in Ω ∩ R such that (λ1, λ2) ⊂ ρ(A) and [·, ·] is positive definite on<br />
both ker(A−λ1) and ker(A−λ2). Then there exists a (discrete) eigenvalue µ <strong>of</strong> B in (λ1, λ2) such<br />
that [·, ·] is not negative definite on the algebraic eigenspace corresponding to µ. In particular, if<br />
µ is a simple eigenvalue with a corresponding eigenvector f, then [f, f] > 0.<br />
The result is applied to a class <strong>of</strong> Sturm-Liouville problems with an indefinite weight function.<br />
Zeros <strong>of</strong> Nevanlinna functions with one negative square<br />
Henrik Winkler (TU Ilmenau) Schedule<br />
A generalized Nevanlinna function Q(z) with one negative square has precisely one generalized<br />
zero <strong>of</strong> nonpositive type in the closed extended upper halfplane. The fractional linear transformation<br />
defined by Qτ(z) = (Q(z) − τ)/(1 + τQ(z)), τ ∈ R ∪ {∞}, is a generalized Nevanlinna<br />
function with one negative square. Its generalized zero <strong>of</strong> nonpositive type α(τ) as a function <strong>of</strong> τ<br />
defines a path in the closed upper halfplane. Various properties <strong>of</strong> this path are studied in detail.<br />
A perturbation approach to differential operators with indefinite weights<br />
Jussi Behrndt (TU Graz), Friedrich Philipp (TU Berlin), Carsten Trunk (TU Ilmenau) Schedule<br />
In many situations differential operators with indefinite weight functions can be regarded as perturbations<br />
<strong>of</strong> nonnegative selfadjoint operators in Krein spaces. In this talk we first provide an<br />
abstract result on bounded additive perturbations and apply it afterwards to Sturm-Liouville and<br />
second order elliptic partial differential operators with indefinite weights on unbounded domains.<br />
S23.2: Partial Differential Operators Tue, 16:00–18:00<br />
Chair: Sergey Belyi S1|03–107<br />
Weak Neumann implies Stokes<br />
Horst Heck (TU <strong>Darmstadt</strong>) Schedule<br />
When studying the Navier-Stokes equations, one <strong>of</strong> the basic models in fluid dynamics, a thorough<br />
understanding <strong>of</strong> the (linear) Stokes equation is very helpful. In particular, the property<br />
<strong>of</strong> maximal L p -regularity is a very powerful tool in order to treat the nonlinear equation. In this<br />
presentation we show that the existence <strong>of</strong> the Helmholtz projection in L q (Ω) is sufficient for the<br />
maximal L p -regularity <strong>of</strong> the Stokes operator, provided the domain Ω ⊂ R n is smooth enough.<br />
The presented result is a joint work with M. Geissert, M. Hieber, and O. Sawada.<br />
Schrödinger operators with interactions on hypersurfaces<br />
Vladimir Lotoreichik (TU Graz) Schedule
380 Section 23: Applied operator theory<br />
In the talk we plan to present a new approach to the definition <strong>of</strong> self-adjoint Schrödinger operators<br />
with δ and δ ′ interactions on hypersurfaces. This approach uses operator extension theory via quasi<br />
boundary triples. Within our approach we prove results concerning spectral and scattering theory<br />
<strong>of</strong> Schrödinger operators with interactions on hypersurfaces.<br />
A comparison with the approach based on quadratic forms will be given. The quadratic form<br />
for δ ′ interactions was not constructed so far and the question <strong>of</strong> its construction was posed as<br />
an open problem by Pavel Exner in 2008. In the talk it will be also presented our solution <strong>of</strong> that<br />
problem.<br />
The talk is based on a joint work with Jussi Behrndt (Graz University <strong>of</strong> Technology) and<br />
Matthias Langer (University Strathclyde).<br />
Spectra <strong>of</strong> selfadjoint elliptic differential operators, Robin-to-Dirichlet maps, and an<br />
inverse problem <strong>of</strong> Calderón type<br />
Jussi Behrndt, Jonathan Rohleder (TU Graz) Schedule<br />
In this talk we consider selfadjoint operator realizations <strong>of</strong> an elliptic differential expression <strong>of</strong> the<br />
form<br />
n� ∂ ∂<br />
Lu = − ajk u + au<br />
∂xj ∂xk<br />
j,k=1<br />
on a bounded or unbounded domain Ω with certain local or nonlocal Robin type boundary conditions.<br />
We will discuss the connections between the behaviour <strong>of</strong> a corresponding Robin-to-Dirichlet<br />
maps on the boundary <strong>of</strong> Ω at its discontinuities and the point, absolutely continuous, and singular<br />
continuous spectra <strong>of</strong> the operator realization. As an application, we present a mild uniqueness<br />
result for the Calderón or Gelfand inverse problem corresponding to L.<br />
Selfadjoint elliptic differential operators on domains with non-compact boundary<br />
Christian Kühn (TU Berlin) Schedule<br />
We consider a uniformly elliptic differential expression L <strong>of</strong> second order on an open set Ω in R n<br />
with a non-compact boundary. We show selfadjointness <strong>of</strong> a class <strong>of</strong> realizations <strong>of</strong> L in L 2 (Ω).<br />
The talk is based on a joint work with J. Behrndt.<br />
Extensible quasi boundary triples and applications<br />
Till Micheler (TU Berlin), Jussi Behrndt (TU Graz) Schedule<br />
We study extensions <strong>of</strong> symmetric operators in Hilbert spaces via a generalization <strong>of</strong> boundary<br />
triple methods and also discuss applications to elliptic partial differential operators on smooth<br />
and rough domains.<br />
S23.3: Applied Operator Theory and Linear Systems Wed, 13:30–15:30<br />
Chair: Andras Batkai S1|03–107<br />
The Elusive Drude-Born-Fedorov Model for Chiral Electromagnetic Media.<br />
Rainer Picard, Henrik Freymond (TU Dresden) Schedule<br />
In a Hilbert space operator setting, covering a comprehensive class <strong>of</strong> evolutionary equations, as<br />
a particular application various aspects <strong>of</strong> material laws for Maxwell’s equations are discussed.<br />
In particular, the Drude-Born-Fedorov model for electromagnetic waves in chiral media is investigated<br />
and well-posedness is shown.<br />
Well-posedness and conservativity for linear control systems (Part 1)<br />
Marcus Waurick (TU Dresden) Schedule
Section 23: Applied operator theory 381<br />
We discuss a class <strong>of</strong> linear control problems in a Hilbert space setting. The aim is to show that<br />
these control problems fit in a particular class <strong>of</strong> evolutionary equations such that the discussion<br />
<strong>of</strong> well-posedness becomes easily accessible. We exemplify our findings by a system with unbounded<br />
control and observation operator.<br />
Well-posedness and conservativity for linear control systems (Part 2)<br />
Sascha Trostorff (TU Dresden) Schedule<br />
Using the results obtained in part 1 <strong>of</strong> the talk, we study conservativity <strong>of</strong> a certain class <strong>of</strong> linear<br />
control problems. For this purpose we require additional regularity properties <strong>of</strong> our solution<br />
operator in order to allow pointwise evaluations <strong>of</strong> our solution. We apply the results to the linear<br />
control system with unbounded observation and control operators mentioned in the first part <strong>of</strong><br />
the talk.<br />
On energy conditions for electromagnetic diffraction by apertures<br />
Matthias Kunik (<strong>Universität</strong> Magdeburg), Norbert Gorenflo (TFH Berlin) Schedule<br />
The diffraction <strong>of</strong> light is considered for a plane screen with an open bounded aperture. The<br />
corresponding solution behind the screen is given explicitly in terms <strong>of</strong> the Fourier transforms<br />
<strong>of</strong> the tangential components <strong>of</strong> the electric boundary field on the screen. All components <strong>of</strong> the<br />
electric as well as the magnetic field vector are considered. We introduce solutions with global<br />
finite energy behind the screen and describe them in terms <strong>of</strong> two boundary potential functions.<br />
This new approach leads to a decoupling <strong>of</strong> the vectorial boundary equations on the screen in the<br />
case <strong>of</strong> global finite energy. For the physically admissible solutions, i.e. the solutions with local<br />
finite energy, we derive a characterisation in terms <strong>of</strong> the electric boundary fields.<br />
Approximation methods for a class <strong>of</strong> perturbed paired convolution equations<br />
Michał A. Nowak (AGH University <strong>of</strong> Science and Technology, Krakow) Schedule<br />
We consider approximation methods for some class <strong>of</strong> perturbed paired convolution equations (or,<br />
in general, singular equations). Effective error estimates, and simultaneously, decaying properties<br />
for solutions are obtained in terms <strong>of</strong> some smooth spaces. The talk is based on a joint work with<br />
Petru A. Cojuhari.<br />
Hamiltonians and Riccati equations for unbounded control and observation operators<br />
Christian Wyss, Birgit Jacob (<strong>Universität</strong> Wuppertal), Hans Zwart (University <strong>of</strong> Twente, The<br />
Netherlands) Schedule<br />
We consider the control algebraic Riccati equation<br />
A ∗ X + XA − XBB ∗ X + C ∗ C = 0<br />
for the case that A is normal with compact resolvent, B ∈ L(U, H−s) and C ∈ L(Hs, Y ), 0 ≤ s ≤ 1.<br />
Here Hs ⊂ H ⊂ H−s are the usual fractional domain spaces corresponding to A. Under certain<br />
additional assumptions on A, B and C we show the existence <strong>of</strong> infinitely many solutions X <strong>of</strong><br />
the Riccati equation using invariant subspaces <strong>of</strong> the Hamiltonian operator matrix<br />
� �<br />
∗<br />
A −BB<br />
T =<br />
.<br />
−C ∗ C −A ∗<br />
The first problem is here to make sense <strong>of</strong> T as an operator on H × H, because BB ∗ and C ∗ C<br />
map from Hs to H−s. Our main tools are then Riesz bases <strong>of</strong> eigenvectors <strong>of</strong> T and indefinite<br />
inner products. In general the solutions X will be unbounded, but we also obtain conditions for<br />
bounded solutions.
382 Section 23: Applied operator theory<br />
S23.4: Applied Operator Theory Wed, 16:00–18:00<br />
Chair: Jussi Behrndt S1|03–107<br />
Shape Preservation <strong>of</strong> Evolution Equations<br />
András Bátkai (Loránd Eötvös University Budapest) Schedule<br />
Motivated by positivity-, monotonicity-, and convexity preserving differential equations, we introduce<br />
a definition <strong>of</strong> shape preserving operator semigroups and analyze their fundamental properties.<br />
In particular, we prove that the class <strong>of</strong> shape preserving semigroups is preserved by<br />
perturbations and taking limits. These results are applied, among others, to partial delay differential<br />
equations.<br />
Sectorial realizations <strong>of</strong> Stieltjes functions<br />
Sergey Belyi (Troy University) Schedule<br />
A class <strong>of</strong> Stieltjes functions with a special condition is considered. We show that a function<br />
belonging to this class can be realized as the impedance function <strong>of</strong> a singular L-system with<br />
a sectorial state-space operator. We provide an additional condition on a given function from<br />
this class so that the state-space operator <strong>of</strong> the realizing L-system is α-sectorial with the exact<br />
angle <strong>of</strong> sectoriality α. Then these results are applied to L-systems based upon a non-self-adjoint<br />
Schrödinger operator.<br />
The talk is based on a joint work with Yu. Arlinskiĭ and E. Tsekanovskiĭ.<br />
On trace norm estimates<br />
Johannes Brasche (TU Clausthal) Schedule<br />
Let E and P be nonnegative quadratic forms in a Hilbert space H and suppose that E and the<br />
sum E + bP is densely defined and closed for every b > 0. Let Hb be the selfadjoint operator<br />
associated to E + bP . We present estimates for the trace norm <strong>of</strong><br />
(Hb + 1) −1 − lim<br />
b ′ (Hb ′ + 1)−1<br />
−→∞<br />
In particular, we present a criterion in order that these trace norms tend to zero with maximal<br />
rate, i.e. as fast as O(1/b). We illustrate our results with the aid <strong>of</strong> point interaction Hamiltonians.<br />
On determining the domain <strong>of</strong> the adjoint operator<br />
Michal Wojtylak (Jagiellonian University, Cracow) Schedule<br />
A theorem that is <strong>of</strong> aid in computing the domain <strong>of</strong> the adjoint operator will be presented. It may<br />
serve e.g. as a criterion for selfadjointness <strong>of</strong> a symmetric operator, for normality <strong>of</strong> a formally<br />
normal operator or for H–selfadjointness <strong>of</strong> an H–symmetric operator.<br />
Parabolic Variational and Quasi-Variational Inequalities with Gradient Constraints<br />
Carlos N. Rautenberg (<strong>Universität</strong> Graz), Michael Hintermüller (HU Berlin) Schedule<br />
A class <strong>of</strong> nonlinear parabolic quasi-variational inequality (QVI) problems with gradient type<br />
constraints in function space is considered. Problems <strong>of</strong> this type arise, for instance, in the mathematical<br />
modelization <strong>of</strong> superconductors and elasto-plasticity. The paper addresses existence,<br />
regularity and approximation results based on monotone operator theory, Mosco convergence and<br />
C0 semigroup methods. Numerical tests involving the p-Laplacian operator with several nonlinear<br />
constraints are provided.
Section 23: Applied operator theory 383<br />
On a class <strong>of</strong> quadratic operator pencils with normal coefficients<br />
Friedrich Philipp (TU Ilmenau), Vladimir Strauss (Universidad Simón Bolívar, Caracas),<br />
Carsten Trunk (TU Ilmenau) Schedule<br />
A standard description <strong>of</strong> damped small oscillations <strong>of</strong> a continuum or <strong>of</strong> small oscillations <strong>of</strong> a<br />
pipe carrying steady-state fluid is done via<br />
T ¨z + R ˙z + V z = 0, (1)<br />
where z is a function with values in a Hilbert space and V and R are unbounded operators. A<br />
classical approach is to investigate solutions <strong>of</strong> the form u(t) = e tλ φ0, and to transform, under<br />
some additional assumptions, the equation in (1) into<br />
L(λ)φ0 := (λ 2 I + λE + F )φ0 = 0<br />
with bounded operators E and F . We will investigate the operator polynomial L with the coefficients<br />
E = AC and F = C 2 , where C is a bounded normal operator in a Hilbert space H and A<br />
is a bounded selfadjoint operator which commutes with C. If there exists a bounded operator Z1<br />
which is an operator root, i.e., a solution <strong>of</strong><br />
Z 2 + ACZ + C 2 = 0,<br />
then L(λ) = λ 2 + λAC + C 2 decomposes into linear factors<br />
L(λ) = (λI − � Z1)(λI − Z1),<br />
where � Z1 = −AC − Z1.<br />
In our talk we will give sufficient conditions for the existence <strong>of</strong> an operator root. For this we<br />
will investigate the companion operator (or linearizer) <strong>of</strong> the operator polynomial L which turns<br />
out to be a normal operator in some Krein space. We will then apply recent results from the<br />
spectral theory <strong>of</strong> normal operators in Krein spaces.
384 Section 24: History <strong>of</strong> mechanics<br />
Section 24: History <strong>of</strong> mechanics<br />
Organizers: Lothar Gaul (<strong>Universität</strong> Stuttgart), Erwin Stein (Leibniz <strong>Universität</strong> Hannover)<br />
S24.1: Analysis <strong>of</strong> deformation, friction, damage and failure Thu, 13:30–15:30<br />
Chair: Erwin Stein S1|03–223<br />
On the History <strong>of</strong> the Mechanical Theory <strong>of</strong> Material Modelling<br />
Albrecht Bertram (<strong>Universität</strong> Magdeburg) Schedule<br />
We consider the last 50 years <strong>of</strong> development <strong>of</strong> material theory which are characterized by<br />
radical disputes and changes <strong>of</strong> paradigms. We are still far from being able to consider this as a<br />
finalized and practical theory. Two main lines <strong>of</strong> approaches shall be demonstrated, namely the<br />
history or heredity functionals, and the inner-variables or state theories. Since both approaches<br />
suffer from fundamental deficiencies, none <strong>of</strong> them really achieved global acceptance. And for a<br />
long time it remained unclear how the two lines could be mutually related.<br />
This was changed in 1972 by Nolls New Theory <strong>of</strong> Simple Materials [1], in which a third<br />
approach was suggested, and one <strong>of</strong> the former sets could be imbedded into the other. The gain<br />
<strong>of</strong> generality was, however, accompanied by a loss <strong>of</strong> simplicity, so that this theory is used only<br />
by very few singu-lar groups within our community.<br />
During the last 40 to 50 years many new flowering branches <strong>of</strong> material theory like finite<br />
plasticity, viscoplasticity, or continuum damage mechanics have been successfully created, but<br />
a globally ac-cepted general theory is still lacking. The tree <strong>of</strong> material theory has gained an<br />
overwhelming variety <strong>of</strong> branches, while its trunk still remains conceptually unclear. If we enlarge<br />
our frame and include thermodynamics into our considerations, then we have to state that also<br />
here the lack <strong>of</strong> a general theory leads to undesirable effects like, e.g., that for each and every<br />
new constitutive model the thermodynamical consistency has to proven anew without being able<br />
to just refer to a general representation. There remains still a good deal <strong>of</strong> work to be done.<br />
[1] Noll, W.: A new mathematical theory <strong>of</strong> simple materials. Arch. Rational Mech. Anal. 48,<br />
1-50 (1972)<br />
Einige Bemerkungen zur Geschichte der Plastizitätstheorie<br />
Otto T. Bruhns (<strong>Universität</strong> Bochum) Schedule<br />
Die Geschichte der Materialgleichungen und damit auch die Entwicklung der heutigen Materialtheorie<br />
als einer Methode zur Beschreibung des Verhaltens von Materialien ist eng mit der<br />
Entwicklung der Kontinuumstheorie auf der einen Seite sowie mit der beginnenden Industrialisierung<br />
gegen Ende des 19. Jahrhunderts verknüpft.<br />
Während einerseits durch Cauchy, Euler, Leibniz u.a. Begrifflichkeiten wie das Kontinuum,<br />
Spannungen und Verzerrungen, deformierbare Körper eingeführt und die mathematischen Methoden<br />
zu ihrer Beschreibung bereitgestellt wurden, hat erst der Druck der Industrialisierung mit<br />
dem Bedürfnis nach immer neueren, zugleich aber auch verlässlich sicheren, Entwicklungen dazu<br />
geführt, dass neben der Beschreibung eines elastischen Verhaltens fester Körper auch dem realen<br />
Verhalten im Zustand des Versagens eher entsprechende Modelle wie z.B. das eines elastischplastischen<br />
Verhaltens eingeführt wurden.<br />
Vor diesem Hintergrund will der Vortrag in die Geschichte der Plastizitätstheorie einführen<br />
und dabei schlaglichtartig auch die Beiträge des Darmstädter Absolventen Heinrich Hencky beleuchten,<br />
der vor nicht ganz 100 Jahren hier seine wissenschaftliche Laufbahn begonnen hat.
Section 24: History <strong>of</strong> mechanics 385<br />
Prandtl-Tomlinson-Model: History and Applications in Friction, Plasticity and Nano<br />
Technologies<br />
Valentin L. Popov (TU Berlin) Schedule<br />
One <strong>of</strong> the most popular models in nano tribology widely used as the basis for many investigations<br />
<strong>of</strong> frictional mechanisms on the atomic scale is the so-called TTomlinson model“. The name<br />
TTomlinson modelïs, however, historically incorrect: The paper by Tomlinson that is <strong>of</strong>ten cited<br />
in this context [1] did not contain the model known as the TTomlinson modeländ suggests an<br />
adhesive contribution to friction. In reality it was Ludwig Prandtl who suggested in 1928 this<br />
model to describe the plastic deformations in crystals [2]. Following some other researchers we<br />
therefore call this model the PPrandtl-Tomlinson-Model“, while the truly correct name should<br />
be just Prandtl model. The original paper by Ludwig Prandtl was written in German and was<br />
not accessible for a long time for the largest part <strong>of</strong> international tribological community. In this<br />
paper, Ludwig Prandtl considered not only the simplest deterministic form <strong>of</strong> the model consisting<br />
<strong>of</strong> a point mass driven in a periodic potential, but also the influence <strong>of</strong> thermal fluctuations.<br />
He was the first ttribologist“who came to the conclusion that thermal fluctuations should lead<br />
to a logarithmic dependency <strong>of</strong> the frictional force on velocity. The success <strong>of</strong> the model as well<br />
as its variations and generalizations is due to the fact that it is the simplest usable model <strong>of</strong> a<br />
tribological system. Results concerning the basic properties <strong>of</strong> the Prandtl-Tomlinson-Model are<br />
scattered over many publications and are summarized shortly in [3]. Extensions and variations<br />
<strong>of</strong> the Prandtl model are widely used for understanding such processes as plasticity, including<br />
dislocations (Frenkel-Kontorowa model), elastic instabilities, control <strong>of</strong> friction by chemical and<br />
mechanical means as well as in designing <strong>of</strong> nano drives and handling <strong>of</strong> single molecules.<br />
[1] G.A. Tomlinson, Phil. Mag, 1929, v.7, p.905.<br />
[2] L. Prandtl, Ein Gedankenmodell zur kinetischen Theorie der festen Körper. ZAMM, 1928,<br />
Vol. 8, p. 85-106..<br />
[3] V.L. Popov. Contact Mechanics, Springer, 2011.<br />
Some Remarks on the History <strong>of</strong> Fracture Mechanics<br />
Dietmar Gross (TU <strong>Darmstadt</strong>) Schedule<br />
After a short overview on the history <strong>of</strong> fracture mechanics, some important milestones are considered<br />
in detail. They include among others Griffith’s energy criterion and Irwin’s concept <strong>of</strong><br />
K-factors. Enlightened is also the context <strong>of</strong> these early developments with the state <strong>of</strong> the art <strong>of</strong><br />
solid mechanics at that time.<br />
On Fröhlich’s Result for Boussinesqs Problem<br />
A.P.S. Selvadurai, William Scott Pr<strong>of</strong>essor and James McGill Pr<strong>of</strong>essor (McGill University)<br />
Schedule<br />
Boussinesqs solution to the action <strong>of</strong> a concentrated normal force on the surface <strong>of</strong> an isotropic<br />
elastic halfspace has been a problem <strong>of</strong> fundamental interest to theory <strong>of</strong> elasticity with applications<br />
to contact mechanics and specifically geomechanics. Boussinesqs solution can be obtained<br />
in a variety <strong>of</strong> ways starting with Kelvins solution to the problem <strong>of</strong> the interior loading <strong>of</strong> an<br />
infinite space by concentrated force. The linearity <strong>of</strong> the governing equations lends itself to the<br />
additional procedures based on integral transform techniques and potential theory. An extension<br />
to Boussinesqs result was proposed in by O.K. Fröhlich in 1937. The concentration factor introduced<br />
by Fröhlich is visualized as a procedure for examining the pattern <strong>of</strong> load transfer from
386 Section 24: History <strong>of</strong> mechanics<br />
surface loads to the interior <strong>of</strong> the halfspace. The historical details that lead to the introduction<br />
<strong>of</strong> the concentration factor are scant although it is widely used in the area <strong>of</strong> soil mechanics problems<br />
associated with tillage induced soil compaction. The purpose <strong>of</strong> this paper is to examine<br />
the concentration factor in terms <strong>of</strong> geomechanics <strong>of</strong> an elastic continuum and to identify the<br />
precise conditions that are satisfied by the distribution <strong>of</strong> stresses and strains that accommodate<br />
the concentration factor.<br />
S24.2: Interaction <strong>of</strong> experiment, theory and numerics Thu, 16:00–18:00<br />
Chair: Lothar Gaul S1|03–223<br />
Experimentierkunst in der Mikromechanik<br />
Dierk Raabe (MPI Düsseldorf) Schedule<br />
Der Vortrag gibt einen Überblick über die Entwicklung der Experimentierkunst in der Mikromechanik.<br />
Zwei Gebiete werden vorgestellt. Zum Ersten wird die Entwicklung mikromechanischer<br />
Versuche besprochen beginnend mit einfachen Eindringversuchen bis hin zu in-situ Zugversuchen<br />
innerhalb eines Elektronenmikroskops. Zum Zweiten werden die strukturanalytischen Verfahren<br />
der Abbildung von Gitterfehlern von der optischen Mikroskopie über Raster- und Transmissionselektronenmikroskopie<br />
bis hin zur atomaren Analytik dargestellt.<br />
Parameter Identification in Continuum Mechanics: From Hand-Fitting to Stochastic<br />
Modelling<br />
Rolf Mahnken, Kai-Uwe Widany, Nicole Nörenberg (<strong>Universität</strong> Paderborn) Schedule<br />
The correct determination <strong>of</strong> material parameters for constitutive equations is an important issue<br />
for predictive simulation, both in industry and research. Its history is strongly related to the<br />
achievements in constitutive modelling beginning with the celebrated Hooke’s law. This contribution<br />
addresses various topics on parameter identification on the basis <strong>of</strong> experimental data.<br />
Starting from hand-fitting procedures different identification procedures illustrated by simple examples<br />
are outlined. Then particular aspects <strong>of</strong> the least squares approach are illustrated such<br />
as optimization, local minima, sensitivity analysis, consequences <strong>of</strong> instabilities. Uniform small<br />
strain problems and non-uniform large strain problems are considered. For the latter, finite element<br />
results are incorporated into the optimization process, where for efficiency and reliability<br />
the concept <strong>of</strong> goal oriented error estimators for adaptive mesh refinement is considered. Main<br />
shortcomings <strong>of</strong> experimental data are scattering and measurement errors on the one side, and<br />
limited repetitions <strong>of</strong> experiments on the other side, which ensues an uncertainty to the predictive<br />
simulations. In order to obtain a broader range <strong>of</strong> experimental data for statistically distributed<br />
material parameters the concept <strong>of</strong> stochastic modelling is outlined. The different concepts and<br />
methodologies are illustrated by various examples in the field <strong>of</strong> continuum mechanics.<br />
Gibbs–Appell Equations <strong>of</strong> Motion: History and Perspective<br />
Ulrike Zwiers (Hochschule Bochum) Schedule<br />
The so-called Gibbs–Appell equations <strong>of</strong> motion, independently discovered and developed by the<br />
American physicist Josiah Willard Gibbs (1839–1903) and the French mathematician Paul Émile<br />
Appell (1855–1930) in the late 19th century, represent presumably the simplest and most versatile<br />
formulation <strong>of</strong> analytical mechanics discovered so far. Based on Gauss’ principle <strong>of</strong> least<br />
constraints and the use <strong>of</strong> quasi-coordinates, the approach is applicable to both holonomic and<br />
nonholonomic systems, including variable mass systems and systems subject to high-order nonholonomic<br />
constraints.<br />
Despite their elegance and wide field <strong>of</strong> applicability, many textbooks on engineering mecha-
Section 24: History <strong>of</strong> mechanics 387<br />
nics present the Gibbs-Appell equations only as contents <strong>of</strong> secondary importance, provided that<br />
they are covered at all. The contribution at hand discusses the advantages but also the disadvantages<br />
associated with the Gibbs-Appell approach by means <strong>of</strong> illustrative examples and in view<br />
<strong>of</strong> its historical development and recent advances.<br />
Historic development <strong>of</strong> the knowledge <strong>of</strong> shock and blast waves<br />
Torsten Döge, Norbert Gebbeken (<strong>Universität</strong> der Bundeswehr München) Schedule<br />
The historic development <strong>of</strong> the scientific knowledge <strong>of</strong> shock and blast waves is given. The overview<br />
starts in the 17 th century and goes to the first half <strong>of</strong> the 20 th century. Groundbreaking works<br />
<strong>of</strong> outstanding scientists, like Galilei, Torricelli, Pascal, von Guericke, Boyle, Hooke,<br />
Newton, Daniel Bernoulli, Euler, Lagrange, Gay-Lussac, Poisson, Laplace, Navier,<br />
Carnot, Mayer, Stokes, Thomson, Clausius, Maxwell, Riemann, Boltzmann,<br />
Rankine, Hugoniot, Mach, Rayleigh, Taylor, Bethe and Weyl, and their relations are<br />
presented and discussed.<br />
Especially the development <strong>of</strong> sound wave velocity, equation <strong>of</strong> state for gases, balance equations<br />
and the occurrence <strong>of</strong> discontinuities (shocks) is regarded.
388 List <strong>of</strong> Participants<br />
List <strong>of</strong> Participants<br />
A<br />
Aßmann, Ute S19.4 Wed 16:20–16:40<br />
Abali, B. Emek S6.6 Wed 15:10–15:30<br />
Abdelrahman, Mahmoud S14.3 Wed 14:10–14:30<br />
Abdulaziz, Ali S11.5 Thu 14:30–14:50<br />
Abels, Helmut S14.3 Wed 15:10–15:30<br />
Adamyan, Vadim S23.1 Tue 13:30–13:50<br />
Afendikov, Andrey S14.4 Wed 17:00–17:20<br />
Agias<strong>of</strong>itou, Eleni S6.11 Thu 16:20–16:40<br />
Aigner, Mario S9.2 Tue 17:40–18:00<br />
Akindeinde, Saheed Ojo S19.3 Wed 14:50–15:10<br />
Aksel, Nuri<br />
Al-Baldawi, Ammar S9.5 Thu 15:10–15:30<br />
AL-Kinani, Raad S6.8 Wed 16:20–16:40<br />
Alber, Hans-Dieter Me3 Mon 17:40–18:00<br />
Alber, Oliver S5.3 Wed 17:40–18:00<br />
Albrecht, Daniel S2.1 Tue 15:10–15:30<br />
Aldudak, Fettah S10.2 Tue 17:00–17:20<br />
Alexandru Marius, Rizescu S16.2 Tue 17:40–18:00<br />
Alin-Cosmin, Tot S12.3 Wed 14:30–14:50<br />
Allaire, Gregoire Plenary Fri 08:30–09:30<br />
Altenbach, Holm<br />
Altmann, Robert S18.4 Wed 13:30–13:50<br />
Alves de Sousa, Ricardo Yr Me2 Tue 11:20–11:40<br />
Amirtham , Rajagopal S8.8 Thu 17:40–18:00<br />
Ams, Alfons<br />
Ansorge, Rainer<br />
Antos, Pavel S10.3 Wed 14:10–14:30<br />
Arghir, Mariana S2.4 Wed 16:00–16:40<br />
Arne, Walter S22.3 Thu 15:10–15:30<br />
Arnold, Martin S1.6 Thu 13:30–14:10<br />
Arrieta, Andres S4.4 Wed 16:40–17:00<br />
Arslan, Eray S4.7 Thu 16:00–16:40<br />
Asmus, Andreas S12.2 Tue 16:40–17:00<br />
Avakian, Artjom<br />
Avsarkisov, Victor S10.2 Tue 16:20–16:40<br />
Awrejcewicz, Jan S1.3 Tue 17:40–18:00<br />
Aydin, Aycan Özlem S6.2 Tue 14:30–14:50<br />
B<br />
Bátkai, András S23.4 Wed 16:00–16:20<br />
Böhlke, Thomas Me1 Mon 17:15–17:40<br />
Böl, Markus
List <strong>of</strong> Participants 389<br />
Böttcher, Kai S13.3 Wed 17:40–18:00<br />
Bühler, Stefan S12.1 Tue 14:10–14:30<br />
Bürger, Raimund S18.2 Tue 16:00–16:20<br />
Baars, Albert<br />
Baaser, Herbert<br />
Babolian, Maziar<br />
Bach, Karolina S5.4 Thu 13:50–14:10<br />
Baier, Tobias Me2 Mon 17:20–17:40<br />
Balke, Herbert<br />
Ballmann, Josef Prandtl Mon 13:30–14:30<br />
Balzani, Claudio S3.3 Wed 15:10–15:30<br />
Balzani, Daniel S3.2 Tue 16:00–16:20<br />
Bamer, Franz S4.6 Thu 14:10–14:30<br />
Banas, Lubomir S18.7 Thu 13:50–14:10<br />
Banuls, Maria Carmen S17.1 Tue 13:30–14:10<br />
Baodong, Shi S6.1 Tue 14:50–15:10<br />
Bare, Zoufine S8.7 Thu 15:10–15:30<br />
Bargmann, Swantje S8.1 Tue 14:10–14:30<br />
Barnard, Richard S19.2 Tue 17:00–17:20<br />
Baron, Eugeniusz S8.8 Thu 17:00–17:20<br />
Bartel, Thorsten S6.5 Wed 13:30–14:10<br />
Bartels, Alexander S6.4 Tue 17:20–17:40<br />
Barthold, Franz-Joseph S19.3 Wed 14:10–14:30<br />
Bastian, Peter<br />
Bauer, Marcus S12.1 Tue 14:30–14:50<br />
Bauer, Maria S22.2 Tue 16:40–17:00<br />
Baum, Ann-Kristin S20.1 Tue 13:30–13:50<br />
Bayerschen, Eric<br />
Becker, Christian S1.4 Wed 14:50–15:10<br />
Becker, Christian S7.1 Tue 13:30–13:50<br />
Becker, Wilfried<br />
Beckmann, Carla S8.3 Tue 17:40–18:00<br />
Behn, Carsten S2.2 Tue 17:40–18:00<br />
Behnke, Ronny S6.4 Tue 17:00–17:20<br />
Behrndt, Jussi S23.1 Tue 15:10–15:30<br />
Beitelschmidt, Michael S1.7 Thu 16:00–16:20<br />
Belyi, Sergey S23.4 Wed 16:20–16:40<br />
Benner, Peter<br />
Berezhnyi, Maksym S8.2 Tue 17:40–18:00<br />
Berger, Thomas Yr Ma2 Tue 10:00–10:25<br />
Berthelsen, Rolf<br />
Bertram, Albrecht S24.1 Thu 13:30–14:10<br />
Betsch, Peter<br />
Beyn, Wolf-Juergen S17.2 Tue 16:40–17:00<br />
Bian, Xin Yr Me3 Tue 10:40–11:00<br />
Bidier, Sami
390 List <strong>of</strong> Participants<br />
Bientinesi, Paolo<br />
Billmaier, Maximilian S4.1 Tue 14:50–15:10<br />
Birk, Sebastian S17.5 Thu 13:30–13:50<br />
Birken, Philipp S18.3 Wed 13:30–13:50<br />
Bisch<strong>of</strong>f, Stefan S12.2 Tue 16:00–16:20<br />
Bloßfeld, Wolfgang Moritz S7.1 Tue 13:50–14:10<br />
Bluhm, Joachim<br />
Boeck, Thomas S11.6 Thu 16:00–16:20<br />
Boettcher, Konrad S11.4 Wed 16:00–16:20<br />
Boger, Markus S11.2 Tue 17:20–17:40<br />
Bolea Albero, Antonio S2.6 Thu 16:40–17:00<br />
Bolten, Matthias S17.6 Thu 16:40–17:00<br />
Borin, Dmitry S13.3 Wed 17:20–17:40<br />
Borsch, Sebastian S6.4 Tue 16:20–16:40<br />
Bothe, Dieter<br />
Boukellif, Ramdane S3.3 Wed 14:50–15:10<br />
Boyaci, Aydin S5.2 Wed 15:10–15:30<br />
Bozovic, Nemanja S17.5 Thu 13:50–14:10<br />
Bröcker, Christoph S6.6 Wed 13:30–13:50<br />
Brändli, Silvan S7.3 Tue 16:00–16:20<br />
Brüls, Olivier Plenary Tue 08:30–09:30<br />
Brands, Dominik<br />
Brasche, Johannes S23.4 Wed 16:40–17:00<br />
Braun, Julian S14.1 Tue 14:10–14:30<br />
Braun, Stefan S9.2 Tue 17:20–17:40<br />
Breiten, Tobias S17.4 Wed 16:00–16:20<br />
Bremer, Hartmut<br />
Brenner, Andreas S18.1 Tue 15:10–15:30<br />
Brommundt, Eberhard S5.1 Tue 13:30–13:50<br />
Bronowicki, Przemyslaw Max S11.4 Wed 17:20–17:40<br />
Brouwer, Jens S18.1 Tue 13:30–13:50<br />
Bruhns, Otto S24.1 Thu 14:10–14:30<br />
Brylka, Barthel S6.8 Wed 16:40–17:00<br />
Buchacz, Andrzej S7.8 Thu 17:20–17:40<br />
Buerger, Johannes Yr Ma3 Tue 10:20–10:40<br />
Bui, Tinh Quoc S3.4 Wed 16:00–16:20<br />
Burlayenko, Vyacheslav S3.4 Wed 16:40–17:00<br />
C<br />
Canfield, Peter S11.4 Wed 17:40–18:00<br />
Cantrak, Djordje S10.3 Wed 13:30–13:50<br />
Carvalho Leite, Alexandre S20.2 Tue 17:20–17:40<br />
Caylak, Ismail S6.2 Tue 15:10–15:30<br />
Cekus, Dawid S20.6 Thu 17:20–17:40<br />
Chan, Allan<br />
Chaudhry, Aqeel Afzal
List <strong>of</strong> Participants 391<br />
Chen, Zhaoyu S6.4 Tue 16:40–17:00<br />
Chiroiu, Veturia S12.4 Wed 16:20–16:40<br />
Christian, Boehm S19.2 Tue 17:40–18:00<br />
Cibis, Thomas Martin S14.2 Tue 17:00–17:20<br />
Cimarelli, Andrea S13.4 Thu 13:30–13:50<br />
Clanet, Christoph Plenary Wed 08:30–09:30<br />
Class, Andreas G. S10.3 Wed 14:50–15:10<br />
Clever, Debora S19.5 Thu 14:10–14:30<br />
Conti, Sergio<br />
Cremers, Daniel S21.1 Tue 13:30–14:10<br />
Cvetkovic, Ljiljana<br />
Czarnecka, Sylwia<br />
D<br />
Döge, Torsten S24.2 Thu 17:20–17:40<br />
Düll, Wolf-Patrick S14.4 Wed 16:40–17:00<br />
Düster, Alexander<br />
Dally, Tim S6.5 Wed 14:10–14:30<br />
Dargazany, Roozbeh S6.4 Tue 17:40–18:00<br />
Daschiel, Gerti S13.2 Wed 14:50–15:10<br />
De Angelis, Elisabetta S10.1 Tue 13:30–13:50<br />
de Payrebrune, Kristin S5.2 Wed 13:50–14:10<br />
de Silva, Tina S4.4 Wed 17:20–17:40<br />
Debeleac, Carmen S14.2 Tue 16:40–17:00<br />
Denk, Robert<br />
Denzer, Ralf S7.2 Tue 13:50–14:10<br />
Dereich, Steffen S15.1 Wed 14:50–15:10<br />
Dickopf, Thomas S22.2 Tue 16:20–16:40<br />
Didinska, Evgenia S11.1 Tue 14:50–15:10<br />
Diebels, Stefan<br />
Dieringer, Rolf S4.3 Wed 14:10–14:30<br />
Diop, El Hadji S21.2 Tue 16:20–16:40<br />
Dirks, Hendrik S21.2 Tue 17:00–17:20<br />
Dirksen, Frank Yr Me1 Tue 11:40–12:00<br />
Dittmar, Ina S11.3 Wed 14:10–14:30<br />
Dmitrieva, Irina S14.6 Thu 16:20–16:40<br />
Dobberschütz, Sören S14.6 Thu 16:00–16:20<br />
Dohnal, Fadi<br />
Dolzmann, Georg Plenary Fri 12:00–13:00<br />
Dondl, Patrick<br />
Dostal, Leo S15.1 Wed 13:30–13:50<br />
Dreyer, Michael<br />
Dreyer, Wolfgang<br />
Duchmann, Alexander S13.4 Thu 13:50–14:10<br />
Dumitrache, Alexandru S9.1 Tue 14:50–15:10<br />
Dumitrescu, Horia S9.3 Wed 14:30–14:50
392 List <strong>of</strong> Participants<br />
Duong, Xuan Thang S7.3 Tue 17:20–17:40<br />
E<br />
Eberhard, Peter S1.4 Wed 13:30–14:10<br />
Eberhardt, Oliver S6.11 Thu 16:00–16:20<br />
Eckelsbach, Stefan S22.1 Tue 14:10–14:30<br />
Eckstein, Manuel<br />
Ehlers, Wolfgang<br />
Ehret, Alexander S2.5 Thu 13:30–14:10<br />
Eichfelder, Gabriele S16.3 Wed 13:30–13:50<br />
Eidel, Bernhard S8.2 Tue 16:00–16:20<br />
Eisenschmidt, Kathrin S11.1 Tue 13:30–13:50<br />
El Jarbi, Mustapha S16.2 Tue 16:20–16:40<br />
Emamy, Nehzat S11.2 Tue 16:00–16:20<br />
Emmrich, Etienne<br />
Engert, Sonja S13.5 Thu 16:20–16:40<br />
Engwer, Christian Yr Me3 Tue 10:20–10:40<br />
Erbts, Patrick S7.3 Tue 16:40–17:00<br />
Ergenzinger, Christian S1.7 Thu 16:20–16:40<br />
Espig, Mike S17.1 Tue 14:30–14:50<br />
Ethiraj, Gautam S7.6 Wed 17:20–17:40<br />
F<br />
Faßbender, Heike<br />
Fabregat-Traver, Diego S17.3 Wed 14:30–14:50<br />
Fahlbusch, Nina-Carolin S4.4 Wed 17:00–17:20<br />
Farwig, Reinhard<br />
Faulwasser, Timm Yr Ma3 Tue 11:40–12:00<br />
Feng, Fan S18.5 Wed 16:00–16:20<br />
Fidlin, Alexander<br />
Fiege, Sabrina S16.4 Wed 16:40–17:00<br />
Fischer, Katrin S22.1 Tue 14:50–15:10<br />
Flaßkamp, Kathrin S20.3 Wed 14:30–14:50<br />
Fleischhauer, Robert S8.8 Thu 16:20–16:40<br />
Flockerzi, Dietrich<br />
Fornasier, Massimo S17.3 Wed 13:30–13:50<br />
Forster-Heinlein, Brigitte S21.4 Wed 17:00–17:20<br />
Fouego, Marcisse S19.5 Thu 14:50–15:10<br />
Franke, Matthias S20.4 Wed 16:00–16:20<br />
Franze, Andreas S5.4 Thu 14:30–14:50<br />
Friedmann, Elfriede S13.2 Wed 14:30–14:50<br />
Friedmann, Elfriede S14.5 Thu 15:10–15:30<br />
Fritzen, Felix Yr Me2 Tue 11:00–11:20<br />
Frohnapfel, Bettina S13.2 Wed 15:10–15:30<br />
Frommer, Andreas S17.4 Wed 17:40–18:00<br />
Frunzulica, Florin S9.3 Wed 14:10–14:30
List <strong>of</strong> Participants 393<br />
Fuchs, Vilmar S7.7 Thu 13:30–13:50<br />
Furer, Dmytro S15.2 Wed 16:00–16:20<br />
G<br />
Göllner, Thea S16.1 Tue 15:10–15:30<br />
Götschel, Sebastian S19.1 Tue 15:10–15:30<br />
Götz, Marco Yr Me1 Tue 10:20–10:40<br />
Günther, Andreas S19.1 Tue 13:30–14:10<br />
Günther, Christina S6.1 Tue 15:10–15:30<br />
Garl<strong>of</strong>f, Jürgen S17.6 Thu 16:20–16:40<br />
Gatti, Davide S13.1 Tue 13:50–14:10<br />
Gaul, Lothar<br />
Gaulke, Diana S11.4 Wed 17:00–17:20<br />
Gaus, Nicole S5.1 Tue 14:50–15:10<br />
Gautam, Sachin Singh<br />
Gawinecki, Jerzy S14.1 Tue 14:50–15:10<br />
Gehring, Nicole S20.5 Thu 13:50–14:10<br />
Geissert, Matthias S14.3 Wed 13:30–13:50<br />
Gekle, Stephan S11.6 Thu 16:20–16:40<br />
Gellmann, Roman S7.4 Tue 16:20–16:40<br />
Georgiev, Ivan<br />
Georgievskii, Dimitri S6.6 Wed 14:50–15:10<br />
Germain, Sandrine S6.11 Thu 16:40–17:00<br />
Gerzen, Nikolai Yr Me1 Tue 10:40–11:00<br />
Ghareeb, Nader S20.5 Thu 15:10–15:30<br />
Gippert, Sabrina S18.4 Wed 13:50–14:10<br />
Gitter, Kurt S13.3 Wed 17:00–17:20<br />
Gizewski, Carsten S9.6 Thu 17:20–17:40<br />
Glavas, Vedran S8.1 Tue 14:50–15:10<br />
Gligor, Anamaria S2.4 Wed 16:40–17:00<br />
Gluege, Rainer S8.5 Wed 16:40–17:00<br />
Gobbert, Matthias S17.3 Wed 14:50–15:10<br />
Goldmann, Joseph S7.6 Wed 16:40–17:00<br />
Gompper, Gerhard Me2 Mon 16:20–16:40<br />
Gondhalekar, Ravi Yr Ma3 Tue 11:20–11:40<br />
Goodarzi, Mehdi S6.1 Tue 13:30–13:50<br />
Gorb, Yuliya S14.5 Thu 14:30–14:50<br />
Gottschalk, Hanno S15.2 Wed 16:40–17:00<br />
Gräf, Manuel S21.3 Wed 15:10–15:30<br />
Grüne, Lars S20.3 Wed 13:30–13:50<br />
Graf, Matthias S4.8 Thu 17:20–17:40<br />
Graf, Wolfgang<br />
Graichen, Knut S20.3 Wed 13:50–14:10<br />
Granados, Albert S7.8 Thu 16:00–16:20<br />
Grasedyck, Lars S17.2 Tue 16:00–16:20<br />
Graupeter, Thomas S22.2 Tue 17:20–17:40
394 List <strong>of</strong> Participants<br />
Gravenkamp, Hauke S12.2 Tue 16:20–16:40<br />
Griesmaeir, Roland S21.3 Wed 14:10–14:30<br />
Griewank, Andreas S16.4 Wed 16:00–16:20<br />
Große-Wöhrmann, Andre S22.3 Thu 14:30–14:50<br />
Groll, Rodion S10.1 Tue 15:10–15:30<br />
Gross, Dietmar S24.1 Thu 14:50–15:10<br />
Grußler, Christian S20.6 Thu 16:20–16:40<br />
Grundel, Sara S22.4 Thu 16:20–16:40<br />
Grundl, Kilian S1.5 Wed 16:00–16:20<br />
Gruttmann, Friedrich<br />
Guenther, Stefan S21.2 Tue 17:20–17:40<br />
Gueven, Ibrahim S7.1 Tue 14:10–14:30<br />
Guhlke, Clemens S6.7 Wed 16:40–17:00<br />
Gundermann, Thomas S13.3 Wed 16:00–16:20<br />
Guran, Ardeshir S5.4 Thu 13:30–13:50<br />
H<br />
Hömberg, Dietmar S19.6 Thu 16:00–16:40<br />
Häberle, Kai S7.5 Wed 14:10–14:30<br />
Hürkamp, André S8.8 Thu 16:40–17:00<br />
Hütter, Geralf S3.3 Wed 14:30–14:50<br />
Habermehl, Kai S16.3 Wed 14:10–14:30<br />
Hackbarth, Axel S20.3 Wed 14:10–14:30<br />
Hackl, Klaus<br />
Haddad Khodaparast, Hamed Yr Me1 Tue 10:00–10:20<br />
Hagedorn, Peter<br />
Hahn, Andreas S11.5 Thu 14:10–14:30<br />
Hahnenkamm, Anton S12.1 Tue 14:50–15:10<br />
Hanisch, Tanja<br />
Hanke, Hauke S8.7 Thu 13:30–13:50<br />
Hankeln, Frederik S6.12 Thu 16:00–16:20<br />
Hardenacke, Volker S3.5 Thu 14:10–14:30<br />
Hardt, Steffen<br />
Hartmaier, Alexander Me3 Mon 17:20–17:40<br />
Hartmann, Dirk Yr Me3 Tue 10:00–10:20<br />
Hartmann, Stefan<br />
Hebel, Jochen S4.2 Tue 16:40–17:00<br />
Heck, Horst S23.2 Tue 16:00–16:20<br />
Hedrih , Katica R. (Stevanovic) S5.2 Wed 14:50–15:10<br />
Heeren, Behrend S21.4 Wed 16:20–16:40<br />
Heffel, Eduard S5.3 Wed 16:00–16:20<br />
Heidlauf, Thomas S2.2 Tue 16:40–17:00<br />
Heiland, Jan Yr Ma2 Tue 11:10–11:35<br />
Heinemann, Christian S3.2 Tue 17:00–17:20<br />
Heinen, Dennis S21.4 Wed 16:40–17:00<br />
Heinz, Sebastian S6.1 Tue 14:30–14:50
List <strong>of</strong> Participants 395<br />
Helbig, Martin S3.1 Tue 15:10–15:30<br />
Held, Alexander S1.1 Tue 14:10–14:30<br />
Helfen, Cecile S8.8 Thu 16:00–16:20<br />
Heller, Dominik<br />
Hellmich, Christian S4.7 Thu 17:20–17:40<br />
Hempel, Nico S6.2 Tue 14:10–14:30<br />
Hempel, Philipp S6.2 Tue 14:50–15:10<br />
Henneberg, Dimitri S8.7 Thu 14:10–14:30<br />
Hertel, Ida S15.2 Wed 16:20–16:40<br />
Hertel, Kai S18.5 Wed 16:20–16:40<br />
Herzog, Roland Ma1 Mon 16:40–17:00<br />
Hesch, Christian S4.1 Tue 13:50–14:10<br />
Hess, Martin S18.5 Wed 16:40–17:00<br />
Hetzler, Hartmut<br />
Higgins, Natalie S12.2 Tue 17:00–17:20<br />
Hildebrand, Felix Me3 Mon 16:40–17:00<br />
Himmel, Martin<br />
Hinze, Michael S11.6 Thu 16:40–17:00<br />
Hladik, Ondrej<br />
Hochbruck, Marlis Plenary Fri 11:00–12:00<br />
Hochlenert, Daniel S5.1 Tue 13:50–14:10<br />
Hochrainer, Thomas S8.6 Thu 13:30–14:10<br />
H<strong>of</strong>acker, Martina S3.4 Wed 16:20–16:40<br />
H<strong>of</strong>fmann, Norbert S12.3 Wed 13:50–14:10<br />
H<strong>of</strong>reither, Clemens S18.1 Tue 14:50–15:10<br />
Hohe, Jörg S8.2 Tue 17:00–17:20<br />
Hollborn, Stefanie S14.6 Thu 16:40–17:00<br />
Holtermann, Raphael S6.3 Tue 17:00–17:20<br />
Homayonifar, Malek S8.6 Thu 14:30–14:50<br />
Horcicka, Michael<br />
Hossain, Mokarram S6.8 Wed 17:20–17:40<br />
Hosseinzadeh, Arash S10.1 Tue 13:50–14:10<br />
Hriberek, Matja S9.6 Thu 17:00–17:20<br />
Hu, Han S4.1 Tue 14:10–14:30<br />
Hu, Miao S11.1 Tue 15:10–15:30<br />
Huckle, Thomas S17.5 Thu 15:10–15:30<br />
Huidong, Yang S7.3 Tue 17:00–17:20<br />
Hysing, Johan Shu-Ren<br />
I<br />
Ievdokymov, Mykola S6.7 Wed 17:40–18:00<br />
Ihlemann, Jörn<br />
Ilchmann, Achim S20.1 Tue 13:50–14:10<br />
Iqbal, Naveed S7.7 Thu 13:50–14:10<br />
Itskov, Mikhail S6.4 Tue 16:00–16:20<br />
Ivanović, Dečan S9.1 Tue 14:30–14:50
396 List <strong>of</strong> Participants<br />
J<br />
Jöchen, Katja S8.2 Tue 16:40–17:00<br />
Jänicke, Ralf S7.1 Tue 14:30–14:50<br />
Jablonski, Philipp-Paul S4.1 Tue 13:30–13:50<br />
Jacob, Birgit Plenary Thu 09:30–10:30<br />
Jaegle, Felix S11.2 Tue 17:00–17:20<br />
Jahn, Mischa S7.5 Wed 13:50–14:10<br />
Jakirlic, Suad S9.5 Thu 13:30–14:10<br />
Janda, Oliver<br />
Janez, Lupe S10.4 Wed 17:20–17:40<br />
Jarre, Florian<br />
Jędrysiak, Jarosław S4.3 Wed 13:30–14:10<br />
Jeltsch, Rolf<br />
Jian, Dandan S13.5 Thu 16:00–16:20<br />
John, Michael S9.2 Tue 16:40–17:00<br />
Joná, Pavel S9.1 Tue 14:10–14:30<br />
Joulaian, Meysam S8.5 Wed 16:00–16:20<br />
Judt, Paul S3.3 Wed 14:10–14:30<br />
Juhre, Daniel S8.4 Wed 14:30–14:50<br />
Juhre, Daniel S16.2 Tue 16:00–16:20<br />
Junker, Philipp Me3 Mon 17:00–17:20<br />
Juraszek, Janusz<br />
Juretzka, Carsten<br />
Jurisits, Richard S5.2 Wed 14:30–14:50<br />
K<br />
Körner, Claudia S5.2 Wed 13:30–13:50<br />
Köster, Marius<br />
Kühn, Christian S23.2 Tue 17:00–17:20<br />
Kürschner, Patrick S17.4 Wed 16:20–16:40<br />
Kaźmierczak, Magda S4.6 Thu 14:30–14:50<br />
Kalisch, Jan S8.1 Tue 14:30–14:50<br />
Kaliske, Michael<br />
Kallendorf, Christina S11.5 Thu 13:50–14:10<br />
Kaltenbacher, Barbara<br />
Kaltenbacher, Manfred S12.1 Tue 13:30–14:10<br />
Kamlah, Marc<br />
Kancheva, Elena Vladimirova<br />
Kandler, Ute S17.3 Wed 13:50–14:10<br />
Karabelas, Elias S18.2 Tue 16:20–16:40<br />
Karcher, Christian<br />
Kavaliou, Klim S18.8 Thu 16:00–16:20<br />
Kawohl, Bernd<br />
Kazeev, Vladimir S17.1 Tue 14:10–14:30<br />
Kebriaei, Reza S6.5 Wed 14:50–15:10
List <strong>of</strong> Participants 397<br />
Kecskemethy, Andres<br />
Keeling, Stephen S21.3 Wed 13:30–14:10<br />
Keip, Marc-Andre<br />
Kelbin, Olga S14.3 Wed 13:50–14:10<br />
Keller, Florian Me2 Mon 16:40–17:00<br />
Kern, Dominik S4.8 Thu 16:00–16:20<br />
Khalaquzzaman, Md S8.5 Wed 16:20–16:40<br />
Khan , Muhammad Sabeel S6.3 Tue 16:00–16:20<br />
Khoromskaya, Venera S17.1 Tue 14:50–15:10<br />
Khoromskij, Boris<br />
Khotenko, Olena<br />
Khrabustovskyi, Andrii S8.3 Tue 17:20–17:40<br />
Khromov, Oleg S11.5 Thu 15:10–15:30<br />
Khruslov, Evgen S8.3 Tue 16:00–16:40<br />
Khujadze, George S12.1 Tue 15:10–15:30<br />
Kiefer, Björn S7.6 Wed 16:00–16:40<br />
Kienzler, Reinhold<br />
Kilian, F. Johannes S1.3 Tue 16:20–16:40<br />
Kiryan, Dmitry S1.2 Tue 17:00–17:20<br />
Kitavtsev, Georgy Ma3 Mon 16:30–17:00<br />
Klapproth, Corinna S18.5 Wed 17:00–17:20<br />
Klawonn, Axel S17.5 Thu 14:10–14:30<br />
Klein, Benedikt S9.4 Wed 16:00–16:20<br />
Klinge, Sandra S8.4 Wed 13:30–13:50<br />
Klusemann, Benjamin Yr Me2 Tue 10:40–11:00<br />
Kluwick, Alfred S9.2 Tue 17:00–17:20<br />
Knüppel, Torsten S20.5 Thu 13:30–13:50<br />
Knees, Dorothee S14.1 Tue 14:30–14:50<br />
Knoll, Carsten S20.4 Wed 16:20–16:40<br />
Kobert, Maria S18.1 Tue 13:50–14:10<br />
Koch, David S7.1 Tue 14:50–15:10<br />
Koch, Michael S1.5 Wed 16:40–17:00<br />
Kochmann, Dennis Yr Me2 Tue 10:00–10:20<br />
Koller, Daniela S16.1 Tue 14:30–14:50<br />
Kolling, Stefan<br />
Kollmann, Markus S19.1 Tue 14:50–15:10<br />
Kolmeder, Sebastian S2.3 Wed 14:10–14:30<br />
Kolodziej, Jan Adam S18.4 Wed 14:10–14:30<br />
Kolpakov, Alexander G. S8.3 Tue 17:00–17:20<br />
Koltai, Péter S20.4 Wed 17:40–18:00<br />
Kolupaev, Vladimir A. S6.10 Thu 15:10–15:30<br />
Komo, Christian S14.4 Wed 16:00–16:20<br />
Konchakova, Natalia S3.4 Wed 17:00–17:20<br />
Kondratenko, Yuriy S16.2 Tue 17:20–17:40<br />
Konyukhov, Alexander<br />
Kosmas, Odysseas S18.5 Wed 17:20–17:40
398 List <strong>of</strong> Participants<br />
Kostic, Vladimir S17.3 Wed 14:10–14:30<br />
Kotyczka, Paul S20.4 Wed 16:40–17:00<br />
Kowalczyk, Wojciech<br />
Krämer, Stephan S6.10 Thu 14:50–15:10<br />
Krüger, Melanie S4.1 Tue 14:30–14:50<br />
Krüger, Thomas<br />
Krajsek, Kai S21.1 Tue 14:50–15:10<br />
Kralovec, Christoph S4.3 Wed 14:30–14:50<br />
Krasnov, Dmitry S9.6 Thu 16:00–16:40<br />
Kratochvil, Jan S4.5 Thu 15:10–15:30<br />
Krause, Robert S2.6 Thu 17:00–17:20<br />
Kraynyukova, Nataliya<br />
Kressner, Daniel S17.2 Tue 17:40–18:00<br />
Kreuzer, Edwin<br />
Krichler, Martin S13.3 Wed 16:20–16:40<br />
Krumbein, Andreas S9.1 Tue 13:30–14:10<br />
Kruse, Roland S2.2 Tue 16:00–16:20<br />
Kruse, Sebastian S18.3 Wed 14:10–14:30<br />
Kruzik, Martin<br />
Krysko, Anton S5.1 Tue 14:30–14:50<br />
Kuhl, Ellen S2.6 Thu 16:00–16:40<br />
Kuhlmann, Hendrik Christoph S9.2 Tue 16:00–16:20<br />
Kuhn, Charlotte S3.2 Tue 16:20–16:40<br />
Kuijper, Arjan S21.2 Tue 16:40–17:00<br />
Kummer, Florian S11.3 Wed 13:50–14:10<br />
Kunik, Matthias S23.3 Wed 14:30–14:50<br />
Kunis, Susanne Ma2 Mon 17:30–18:00<br />
Kurz, Armin S13.4 Thu 14:50–15:10<br />
Kurzeja, Patrick S8.4 Wed 14:50–15:10<br />
Kutschke, Andreas S6.10 Thu 14:10–14:30<br />
Kutyniok, Gitta S21.4 Wed 17:20–17:40<br />
Kutyniok, Gitta S17.6 Thu 16:00–16:20<br />
L<br />
Lübke, Martin S11.3 Wed 15:10–15:30<br />
Labisch, Daniel<br />
Lahmer, Tom S7.4 Tue 16:00–16:20<br />
Landgraf, Ralf S6.11 Thu 17:00–17:20<br />
Lang, Holger S1.6 Thu 15:10–15:30<br />
Langer, Ulrich S19.4 Wed 16:00–16:20<br />
Laouar, Roudouane S9.5 Thu 14:50–15:10<br />
Larsson, Ragnar S3.1 Tue 13:30–14:10<br />
Lazar, Markus S6.7 Wed 16:00–16:40<br />
Lazuka, Jaroslaw<br />
Lazzaroni, Giuliano S8.7 Thu 13:50–14:10<br />
Leben, Leslie S23.1 Tue 14:10–14:30
List <strong>of</strong> Participants 399<br />
Lehmann, Eva S6.3 Tue 16:20–16:40<br />
Leithäuser, Christian S19.1 Tue 14:30–14:50<br />
Leitz, Thomas S7.7 Thu 14:10–14:30<br />
Lenh<strong>of</strong>, Bernd S7.2 Tue 14:10–14:30<br />
Lenzen, Frank S21.3 Wed 14:50–15:10<br />
Leyendecker, Sigrid S1.1 Tue 13:30–14:10<br />
Li, Bo Yr Me3 Tue 11:20–11:40<br />
Li, Weiguo S6.12 Thu 17:20–17:40<br />
Liebscher, Martin<br />
Lincke, Anne S19.4 Wed 17:20–17:40<br />
Linder, Christian S3.1 Tue 14:10–14:30<br />
Linke, Julia S13.3 Wed 16:40–17:00<br />
Lion, Alexander S6.2 Tue 13:30–14:10<br />
Litak, Grzegorz<br />
Litvinenko, Alexander Yr Ma1 Tue 10:20–10:40<br />
Lohkamp, Richard S6.3 Tue 17:40–18:00<br />
Lohse, Christian S1.7 Thu 17:20–17:40<br />
Lorenz, Maike S14.4 Wed 17:20–17:40<br />
Lorenz, Michael S5.4 Thu 15:10–15:30<br />
Lotfi, Marjan<br />
Lotoreichik, Vladimir S23.2 Tue 16:20–16:40<br />
Lu, Daixing S7.7 Thu 15:10–15:30<br />
Lu, Shuai S19.6 Thu 16:40–17:00<br />
Lubkoll, Lars S19.6 Thu 17:00–17:20<br />
Luchscheider, Vera S4.6 Thu 13:30–13:50<br />
Ludwig, Hanna<br />
Ludwig, Lars S18.3 Wed 13:50–14:10<br />
Luginsland, Tobias S10.4 Wed 17:00–17:20<br />
Lumei, Calin S12.3 Wed 15:10–15:30<br />
Luttmann, Andreas<br />
Lvov, Ivan S4.7 Thu 17:00–17:20<br />
M<br />
Ma, Chen S11.4 Wed 16:20–16:40<br />
Möws, Roland S23.1 Tue 14:30–14:50<br />
Müller, Björn S11.2 Tue 16:20–16:40<br />
Müller, Matthias<br />
Müller, Ralf S7.2 Tue 13:30–13:50<br />
Müller, Sebastian S3.2 Tue 17:20–17:40<br />
Müller, Viktor S8.2 Tue 17:20–17:40<br />
Müller, Wolfgang S4.4 Wed 16:00–16:40<br />
Müller-Hoeppe, Dana S8.7 Thu 14:30–14:50<br />
Müllner, Markus S9.1 Tue 15:10–15:30<br />
Müllner, Thomas S12.3 Wed 14:10–14:30<br />
Münker, Tobias S17.4 Wed 17:20–17:40<br />
Maas, Ramona S2.2 Tue 17:00–17:20
400 List <strong>of</strong> Participants<br />
Mabuma, J<strong>of</strong>frey S2.1 Tue 14:50–15:10<br />
Mach, Thomas S17.4 Wed 16:40–17:00<br />
Mack, Werner<br />
Mahmood, Saqib S13.4 Thu 13:30–13:50<br />
Mahnken, Rolf S24.2 Thu 16:40–17:00<br />
Maier, Christian S1.5 Wed 16:20–16:40<br />
Majcher, Krzyszt<strong>of</strong> S4.6 Thu 13:50–14:10<br />
Majzner, Michał S6.9 Thu 14:50–15:10<br />
Malessa, Christian S1.5 Wed 17:00–17:20<br />
Maringer, Johannes S15.1 Wed 14:10–14:30<br />
Markert, Bernd<br />
Markert, Richard<br />
Markzac, Rogerio<br />
Marschall, Holger S11.5 Thu 14:50–15:10<br />
Martens, Wolfram S5.1 Tue 15:10–15:30<br />
Marti, Kurt<br />
Materna, Daniel S16.3 Wed 14:30–14:50<br />
Mattern, Steffen S4.2 Tue 16:00–16:20<br />
Matthes, Michael Yr Ma2 Tue 10:45–11:10<br />
Matvienko, Oleg S10.4 Wed 16:40–17:00<br />
Matz, Daniel S9.3 Wed 15:10–15:30<br />
Mauthe, Steffen S6.1 Tue 13:50–14:10<br />
McBride, Andrew Me1 Mon 16:25–16:50<br />
Mehmood, Ahmer<br />
Mehrmann, Volker S20.1 Tue 14:10–14:30<br />
Melcher, Andreas S7.8 Thu 16:20–16:40<br />
Menshikov, Yuri S22.4 Thu 17:20–17:40<br />
Menshykov, Oleksandr S3.4 Wed 17:20–17:40<br />
Menzel, Andreas<br />
Mester, Rudolf<br />
Meysonnat, Pascal S13.1 Tue 13:30–13:50<br />
Michael, Christian S20.2 Tue 16:40–17:00<br />
Micheler, Till S23.2 Tue 17:20–17:40<br />
Miedlar, Agnieszka S17.2 Tue 17:00–17:20<br />
Miehe, Christian Me1 Mon 16:00–16:25<br />
Mielke, Alexander S14.1 Tue 13:30–14:10<br />
Mierzwiczak, Magdalena S18.3 Wed 14:30–14:50<br />
Miller, Urs S5.3 Wed 16:40–17:00<br />
Min, Chen S6.10 Thu 13:50–14:10<br />
Ming, Pingbing Ma3 Mon 17:00–17:30<br />
Mirwaldt, Thomas S1.7 Thu 16:40–17:00<br />
Mladenova, Clementina S1.2 Tue 16:00–16:20<br />
Modersitzki, Jan S21.2 Tue 17:40–18:00<br />
Mohr, Dirk S3.5 Thu 15:10–15:30<br />
Montalvo-Urquizo, Jonathan S4.4 Wed 17:40–18:00<br />
Moran, Sean S8.6 Thu 14:10–14:30
List <strong>of</strong> Participants 401<br />
Morciano, Alessandra<br />
Mosler, Jörn<br />
Mousavi, Roozbeh S11.2 Tue 16:40–17:00<br />
Muhirwa, Luc N. S20.4 Wed 17:00–17:20<br />
Munteanu, Ligia S6.12 Thu 16:20–16:40<br />
Munz, Claus-Dieter<br />
Muravey, Lionid<br />
N<br />
Němec, Tomá S11.1 Tue 13:50–14:10<br />
Nörenberg, Nicole S6.11 Thu 17:20–17:40<br />
Naß, Martin S19.3 Wed 15:10–15:30<br />
Naetar, Wolf S19.5 Thu 15:10–15:30<br />
Nagórko, Wiesław<br />
Nastac, Silviu S14.2 Tue 16:20–16:40<br />
Nastase, Adriana S16.1 Tue 14:10–14:30<br />
Naumann, Andreas S22.2 Tue 17:00–17:20<br />
Naumov, Maxim Ma2 Mon 16:30–17:00<br />
Necasova, Sarka S13.1 Tue 14:10–14:30<br />
Nedelkovski, Igor<br />
Neff, Patrizio<br />
Neitzel, Ira S19.3 Wed 13:30–14:10<br />
Nesenenko, Sergiy<br />
Neumüller, Martin S18.8 Thu 16:40–17:00<br />
Neumann, Rudolf<br />
Nguyen, An Danh S3.5 Thu 13:50–14:10<br />
Niederhöfer, Florian S1.6 Thu 14:10–14:30<br />
Niessner, Herbert S10.3 Wed 14:30–14:50<br />
Nold, Andreas S9.2 Tue 16:20–16:40<br />
Nopparat, Pochai S18.2 Tue 16:40–17:00<br />
Nowak, Michał A. S23.3 Wed 14:50–15:10<br />
O<br />
Ober-Blöbaum, Sina S22.1 Tue 13:30–14:10<br />
Oberhuber, Bernhard S1.3 Tue 16:40–17:00<br />
Odenbach, Stefan<br />
Of, Günther S18.4 Wed 14:30–14:50<br />
Orlik, Julia S8.7 Thu 14:50–15:10<br />
Osman, Muhammad S4.7 Thu 16:40–17:00<br />
Osorio Nesme, Anuhar S9.6 Thu 17:40–18:00<br />
Ostrowski, Piotr S6.9 Thu 15:10–15:30<br />
Ostwald, Richard S6.5 Wed 15:10–15:30<br />
Otten, Denny S18.8 Thu 17:00–17:20<br />
Ozhoga-Maslovskaja, Oksana S3.2 Tue 17:40–18:00<br />
P
402 List <strong>of</strong> Participants<br />
Płaczek, Marek S7.3 Tue 17:40–18:00<br />
Pach, Martin Yr Ma1 Tue 11:20–11:40<br />
Pandey, Anamika S15.1 Wed 14:30–14:50<br />
Pannek, Jürgen Yr Ma3 Tue 10:40–11:00<br />
Pantangi, Pradeep S10.1 Tue 14:10–14:30<br />
Pearson, John Ma1 Mon 16:20–16:40<br />
Pertschik, Konstantin<br />
Peschka, Dirk Me2 Mon 17:40–18:00<br />
Peter, Thomas S21.3 Wed 14:30–14:50<br />
Peters, Ivo Me2 Mon 17:00–17:20<br />
Petrisor , Silviu Mihai S1.7 Thu 17:40–18:00<br />
Pfaff, Sebastian<br />
Pfeiffer, Friedrich<br />
Pham, Thanh Chung S4.6 Thu 14:50–15:10<br />
Philipp, Anne<br />
Philipp, Friedrich S23.1 Tue 13:50–14:10<br />
Picard, Rainer S23.3 Wed 13:30–13:50<br />
Pieper, Konstantin S19.1 Tue 14:10–14:30<br />
Pinnau, Rene S19.2 Tue 17:20–17:40<br />
Pippig, Michael S17.3 Wed 15:10–15:30<br />
Pitsch, Heinz Plenary Thu 08:30–09:30<br />
Plate, Carolin S3.1 Tue 14:50–15:10<br />
Pollak, Thilo S9.4 Wed 17:40–18:00<br />
Poloni, Federico S20.1 Tue 14:50–15:10<br />
Ponsiglione, Marcello Ma3 Mon 16:00–16:30<br />
Popov, Valentin L. S24.1 Thu 14:30–14:50<br />
Potapov, Vadim S4.8 Thu 16:20–16:40<br />
Prange, Corinna S3.3 Wed 13:30–13:50<br />
Prechtl, Gerhard S4.8 Thu 16:40–17:00<br />
Preusser, Tobias<br />
Prieling, Doris S11.4 Wed 16:40–17:00<br />
Prignitz, Rodolphe S18.1 Tue 14:10–14:30<br />
Prill, Dennis S5.3 Wed 17:00–17:20<br />
Probst, Axel S9.3 Wed 13:30–14:10<br />
Procházka, Pavel S13.4 Thu 14:10–14:30<br />
Prohl, Andreas<br />
Prygorniev, Oleksandr S8.5 Wed 17:40–18:00<br />
Prytula, Mykola S12.4 Wed 16:40–17:00<br />
Q<br />
Quarti, Michael S13.2 Wed 14:10–14:30<br />
Quintana-Orti, Enrique S.<br />
R<br />
Röbenack, Klaus S20.3 Wed 15:10–15:30<br />
Röhrle, Oliver S2.3 Wed 15:10–15:30
List <strong>of</strong> Participants 403<br />
Röhrnbauer, Barbara S2.5 Thu 14:30–14:50<br />
Rösch, Arnd<br />
Rösner, Malte S20.6 Thu 16:40–17:00<br />
Rückert, Jens S18.2 Tue 17:00–17:20<br />
Rüffer, Björn S20.4 Wed 17:20–17:40<br />
Rütten, Markus S13.5 Thu 17:40–18:00<br />
Raabe, Dierk S24.2 Thu 16:00–16:40<br />
Rademacher, Andreas S22.3 Thu 14:10–14:30<br />
Rafa, Józef<br />
Raghunath, Rathan<br />
Raguz, Andrija S14.5 Thu 14:50–15:10<br />
Raina, Arun S3.3 Wed 13:50–14:10<br />
Raisch, Jörg Plenary Fri 09:30–10:30<br />
Rammerstorfer, Franz<br />
Ranjbar, Maedeh<br />
Rasool, Raheel S9.4 Wed 17:20–17:40<br />
Rasuo, Bosko S9.3 Wed 14:50–15:10<br />
Rauschenberger, Philipp S11.1 Tue 14:10–14:30<br />
Rautenberg, Carlos S23.4 Wed 17:20–17:40<br />
Ravnik, Jure<br />
Reble, Marcus Yr Ma3 Tue 11:00–11:20<br />
Reese, Stefanie S2.3 Wed 13:30–14:10<br />
Regener, Benjamin S8.5 Wed 17:20–17:40<br />
Reips, Louise S19.6 Thu 17:40–18:00<br />
Reisner, Timo S11.3 Wed 14:30–14:50<br />
Reiss, Julius S9.4 Wed 16:20–16:40<br />
Reiter, Thomas 1 Tue 18:30–18:50<br />
Reiterer, Stefan S19.4 Wed 17:40–18:00<br />
Reshniak, Viktor S18.4 Wed 14:50–15:10<br />
Reuter, Uwe Yr Me1 Tue 11:00–11:20<br />
Rheinbach, Oliver S22.2 Tue 16:00–16:20<br />
Richter, Thomas Yr Me3 Tue 11:40–12:00<br />
Ricken, Tim<br />
Ricoeur, Andreas<br />
Riedeberger, Donald S13.1 Tue 15:10–15:30<br />
Riedlbauer, Daniel S7.5 Wed 14:50–15:10<br />
Rieger, Florian<br />
Rinne, Klaus Friedrich Me2 Mon 16:00–16:20<br />
Rist, Ulrich S13.4 Thu 14:30–14:50<br />
Rohleder, Jonathan S23.2 Tue 16:40–17:00<br />
Rosenbaum, Benjamin Yr Ma1 Tue 10:40–11:00<br />
Rosenthal, Dietmar S2.3 Wed 14:30–14:50<br />
Rosic, Bojana Yr Ma1 Tue 11:00–11:20<br />
Rosteck, Andreas S10.2 Tue 16:00–16:20<br />
Rothe, Steffen S6.8 Wed 17:40–18:00<br />
Rottmann, Matthias S17.6 Thu 17:00–17:20
404 List <strong>of</strong> Participants<br />
Roy, Shyamal S6.12 Thu 17:40–18:00<br />
Rozgic, Marco S16.1 Tue 14:50–15:10<br />
Rozloznik, Miroslav<br />
Rushchitsky, Jeremiah S12.4 Wed 16:00–16:20<br />
Rutzmoser, Johannes S1.1 Tue 15:10–15:30<br />
Ryzhkov, Oleksandr S12.3 Wed 14:50–15:10<br />
S<br />
Sänger, Nicolas S1.3 Tue 17:00–17:20<br />
Sülü, İsmail Yasin S4.5 Thu 14:30–14:50<br />
Saak, Jens S20.1 Tue 15:10–15:30<br />
Saal, Jürgen S14.4 Wed 16:20–16:40<br />
Sachs, Ekkehard Ma1 Mon 17:40–18:00<br />
Sack, Uli S6.7 Wed 17:00–17:20<br />
Sadigh Behzadi, Armin S18.1 Tue 14:30–14:50<br />
Sadigh Behzadi, Shadan S18.3 Wed 14:50–15:10<br />
Sadiki, Amsini S10.1 Tue 14:30–14:50<br />
Salcher, Patrick S4.6 Thu 15:10–15:30<br />
Sander, Manuela<br />
Santarelli, Claudio S10.4 Wed 16:00–16:20<br />
Sauerland, Kim-Henning S8.4 Wed 15:10–15:30<br />
Sawyer, William S17.5 Thu 14:50–15:10<br />
Sbeiti, Mohamad S7.8 Thu 16:40–17:00<br />
Schäfer, Carsten<br />
Schänzel, Lisa S6.8 Wed 16:00–16:20<br />
Schüler, Thorsten S6.6 Wed 14:30–14:50<br />
Schürg, Marco S4.2 Tue 17:00–17:20<br />
Schaal, Christoph S12.2 Tue 17:20–17:40<br />
Schagerl, Martin<br />
Schauer, Marco S12.2 Tue 17:40–18:00<br />
Schauer, Volker S7.8 Thu 17:00–17:20<br />
Schaufler, Alexander S7.1 Tue 15:10–15:30<br />
Scheider, Ingo S3.1 Tue 14:30–14:50<br />
Schenke, Maik S22.3 Thu 14:50–15:10<br />
Scheunemann, Lisa S8.1 Tue 15:10–15:30<br />
Schidlowski, Sergej<br />
Schieche, Bettina S18.8 Thu 17:20–17:40<br />
Schieck, Berthold<br />
Schiehlen, Werner S1.3 Tue 16:00–16:20<br />
Schiela, Anton S19.5 Thu 14:30–14:50<br />
Schillings, Claudia Yr Ma1 Tue 10:00–10:20<br />
Schlömerkemper, Anja S8.1 Tue 13:30–14:10<br />
Schmidt, Bastian S19.4 Wed 16:40–17:00<br />
Schmidt, Bernd<br />
Schmidt, Ingo S7.7 Thu 14:50–15:10<br />
Schmidt, Marcus
List <strong>of</strong> Participants 405<br />
Schmidt, Thomas S2.1 Tue 14:30–14:50<br />
Schmitt, Joachim S6.10 Thu 14:30–14:50<br />
Schmitt, Regina S6.7 Wed 17:20–17:40<br />
Schmitzer, Bernhard S21.1 Tue 14:10–14:30<br />
Schmoll, Robert S1.6 Thu 14:30–14:50<br />
Schneider , Reinhold S17.1 Tue 15:10–15:30<br />
Schneider, Rene S18.6 Wed 16:00–16:20<br />
Schneidt, Andreas S6.5 Wed 14:30–14:50<br />
Schnepp, Johannes S6.12 Thu 17:00–17:20<br />
Scholle, Markus S6.12 Thu 16:40–17:00<br />
Scholz, Andreas S1.1 Tue 14:30–14:50<br />
Scholz, Lena S20.1 Tue 14:30–14:50<br />
Schröder, Dirk<br />
Schröder, Jörg Me1 Mon 16:50–17:15<br />
Schröder, Wolfgang<br />
Schröppel, Christian S18.6 Wed 16:20–16:40<br />
Schulz, Volker Ma1 Mon 16:00–16:20<br />
Schumacher, Katrin<br />
Schuricht, Friedemann<br />
Schwartpaul, Kai S4.5 Thu 14:10–14:30<br />
Schwarz, Alexander S9.4 Wed 16:40–17:00<br />
Schweitzer, Marcel S17.6 Thu 17:40–18:00<br />
Sedlacek, Matous S17.5 Thu 14:30–14:50<br />
Seemann, Wolfgang<br />
Seifried, Robert S20.2 Tue 17:00–17:20<br />
Selig, Tilman<br />
Selvadurai, Patrick S24.1 Thu 15:10–15:30<br />
Sergey, Lurie S6.9 Thu 14:30–14:50<br />
Setzer, Simon S21.1 Tue 15:10–15:30<br />
Shahid, Mubeen S6.3 Tue 17:20–17:40<br />
Shakhno, Stepan S16.4 Wed 16:20–16:40<br />
Shamolin, Maxim V. S1.2 Tue 16:20–16:40<br />
Shan, Wenzhe S8.2 Tue 16:20–16:40<br />
Shevchuk, Illya S11.3 Wed 13:30–13:50<br />
Shneider, Vladimir S3.5 Thu 14:30–14:50<br />
Shuai, Yan S18.2 Tue 17:20–17:40<br />
Shunqi, Zhang S20.2 Tue 16:20–16:40<br />
Shutov, Alexey S6.3 Tue 16:40–17:00<br />
Sichau, Adrian S16.1 Tue 13:30–13:50<br />
Siebert, Ralf S1.1 Tue 14:50–15:10<br />
Siegl, Benjamin<br />
Simeon, Bernd<br />
Simon, Jaan-Willem S6.8 Wed 17:00–17:20<br />
Simon, Moritz S19.4 Wed 17:00–17:20<br />
simoncini, Valeria Ma1 Mon 17:20–17:40<br />
Sinclair, Andrew
406 List <strong>of</strong> Participants<br />
Sindern, Andrea S7.5 Wed 14:30–14:50<br />
Siska, David S18.7 Thu 13:30–13:50<br />
Sittner, Petr Me3 Mon 16:00–16:40<br />
Skopin, Emma S14.3 Wed 14:30–14:50<br />
Sodhani, Deepanshu S8.4 Wed 14:10–14:30<br />
Sokolov, Andriy Yr Me3 Tue 11:00–11:20<br />
Sokolovic, Sonja S17.6 Thu 17:20–17:40<br />
Sommer, Oliver S9.5 Thu 14:10–14:30<br />
Soos, Anna<br />
Souckova, Natalie S13.2 Wed 13:30–13:50<br />
Specht, Steffen S7.2 Tue 15:10–15:30<br />
Spelsberg-Korspeter, Gottfried S5.3 Wed 17:20–17:40<br />
Sprenger, Lisa S13.5 Thu 17:00–17:20<br />
Sprenger, Michael S2.2 Tue 17:20–17:40<br />
Springer, Andreas S19.3 Wed 14:30–14:50<br />
Srisupattarawanit, Tarin S22.4 Thu 16:40–17:00<br />
Stahl, Dominik S21.4 Wed 16:00–16:20<br />
Stark, Sebastian S7.4 Tue 16:40–17:00<br />
Starkov, Konstantin S2.6 Thu 17:20–17:40<br />
Stauch, Christian S20.5 Thu 14:10–14:30<br />
Staufer, Peter S1.3 Tue 17:20–17:40<br />
Stavropoulou, Electra S16.1 Tue 13:50–14:10<br />
Steeger, Karl S4.2 Tue 17:20–17:40<br />
Steidl, Gabriele<br />
Stein, Anika S9.4 Wed 17:00–17:20<br />
Stein, Erwin<br />
Stein, Lukas<br />
Stein, Peter<br />
Steinbach, Olaf S18.7 Thu 14:10–14:30<br />
Steinbrecher, Andreas S18.6 Wed 16:40–17:00<br />
Steindl, Alois S5.2 Wed 14:10–14:30<br />
Steiner, Helfried<br />
Steinrück, Herbert S9.5 Thu 14:30–14:50<br />
Stieler, Marleen<br />
Stilgenbauer, Patrik S15.1 Wed 13:50–14:10<br />
Stingl, Michael S16.3 Wed 13:50–14:10<br />
St<strong>of</strong>fel, Marcus S4.3 Wed 14:50–15:10<br />
Stojanovic, Mirjana<br />
Stokmaier, Markus S16.2 Tue 17:00–17:20<br />
Stoll, Martin S17.2 Tue 17:20–17:40<br />
Strampe, Malte S2.3 Wed 14:50–15:10<br />
Strein, Sabine S10.1 Tue 14:50–15:10<br />
Stroh, Alexander S13.2 Wed 13:50–14:10<br />
Strubel, Jan<br />
Strzodka, Robert Ma2 Mon 17:00–17:30<br />
Sturm, Kevin S19.6 Thu 17:20–17:40
List <strong>of</strong> Participants 407<br />
Sturmat, Maike S2.2 Tue 16:20–16:40<br />
Stykel, Tatjana<br />
Suresh Kumar , Kannan S11.3 Wed 14:50–15:10<br />
Svanadze, Maia M. S6.6 Wed 13:50–14:10<br />
Svanadze, Merab S6.9 Thu 13:30–14:10<br />
Svendsen, Bob Me1 Mon 17:40–18:00<br />
T<br />
Törnig, Willi<br />
Türk, Sebastian S13.1 Tue 14:50–15:10<br />
Takači, Ðurđica S18.7 Thu 14:30–14:50<br />
Takacs, Stefan Ma1 Mon 17:00–17:20<br />
Tao, Wu<br />
Tepes-Bobescu, Alina-Sabina S2.4 Wed 17:00–17:20<br />
Thalhammer, Mechthild S18.8 Thu 16:20–16:40<br />
Thess, Andre S9.6 Thu 16:40–17:00<br />
Thien-Nga, LE<br />
Thomas, Marita S14.1 Tue 15:10–15:30<br />
Thongmoon, Montri<br />
Thongtha, Kaboon S16.2 Tue 16:40–17:00<br />
Timmermann, Julia<br />
Tkachuk, Mykola S8.4 Wed 13:50–14:10<br />
Tobias, Steinle S22.1 Tue 14:30–14:50<br />
Tobiska, Lutz<br />
Todres, Russell S4.8 Thu 17:00–17:20<br />
Travnikov, Vadim S13.5 Thu 16:40–17:00<br />
Trenn, Stephan Yr Ma2 Tue 10:25–10:45<br />
Trenn, Stephan S20.3 Wed 14:50–15:10<br />
Tropea, Cameron<br />
Trostorff, Sascha S23.3 Wed 14:10–14:30<br />
Trunk, Carsten S23.4 Wed 17:40–18:00<br />
Truskinovsky, Lev Plenary Thu 11:00–12:00<br />
Tsedendamba, Sarantuya<br />
Tuchkova, Natalia<br />
Tympel, Saskia S13.5 Thu 17:20–17:40<br />
U<br />
Ulbrich, Heinz<br />
Ulbricht, Volker<br />
Ullmann, Sebastian S20.5 Thu 14:30–14:50<br />
Ulmer, Heike S3.2 Tue 16:40–17:00<br />
Ulz, Manfred S8.6 Thu 14:50–15:10<br />
Unger, Gerhard S18.6 Wed 17:00–17:20<br />
Uribe, David S12.3 Wed 13:30–13:50<br />
Uruba, Vaclav S10.3 Wed 13:50–14:10<br />
Uschmajew, André
408 List <strong>of</strong> Participants<br />
Utz, Tilman S20.5 Thu 14:50–15:10<br />
V<br />
Varnhorn, Werner S14.5 Thu 14:10–14:30<br />
Vasilyev, Vladimir S18.7 Thu 14:50–15:10<br />
Vendl, Alexander S20.6 Thu 17:00–17:20<br />
Vexler, Boris<br />
Villamil, Pedro Daniel S4.5 Thu 14:50–15:10<br />
Vinci, Carlo S7.7 Thu 14:30–14:50<br />
Vladimirov, Ivaylo Yr Me2 Tue 11:40–12:00<br />
Voigt, Axel S11.5 Thu 13:30–13:50<br />
Voigt, Matthias Yr Ma2 Tue 11:35–12:00<br />
von Wagner, Utz S5.4 Thu 14:10–14:30<br />
Vondřejc, Jaroslav S17.4 Wed 17:00–17:20<br />
Vowinckel, Bernhard S10.4 Wed 16:20–16:40<br />
Vu, Duc Khoi S7.4 Tue 17:00–17:20<br />
Vu, Khiêm S6.10 Thu 13:30–13:50<br />
W<br />
Wächtler, Timo S22.1 Tue 15:10–15:30<br />
Wähnert, Philipp Yr Ma1 Tue 11:40–12:00<br />
Wünsche, Michael S7.6 Wed 17:00–17:20<br />
Wackerfuß, Jens<br />
Waclawczyk, Marta S10.2 Tue 16:40–17:00<br />
Waffenschmidt, Tobias S6.9 Thu 14:10–14:30<br />
Wagner, Andreas S4.2 Tue 17:40–18:00<br />
Wagner, Arndt S2.1 Tue 13:30–14:10<br />
Wagner, Nils S4.8 Thu 17:40–18:00<br />
Wagrowska, Monika<br />
Waldherr, Konrad S17.2 Tue 16:20–16:40<br />
Wallaschek, Joerg S5.1 Tue 14:10–14:30<br />
Walther, Andrea S22.4 Thu 16:00–16:20<br />
Walz, Nico-Philipp S1.4 Wed 14:30–14:50<br />
Warys, Pawel S20.6 Thu 17:40–18:00<br />
Wathen, Andy Plenary Mon 14:30–15:30<br />
Waurick, Marcus S23.3 Wed 13:50–14:10<br />
Weber, Martin<br />
Weigand, Bernhard<br />
Weinberg, Kerstin S7.5 Wed 13:30–13:50<br />
Weiss, Jan-Philipp Ma2 Mon 16:00–16:30<br />
Welk, Martin S21.2 Tue 16:00–16:20<br />
Weller, Stephan S11.2 Tue 17:40–18:00<br />
Wendland, Wolfgang S14.5 Thu 13:30–14:10<br />
Wensch, Jörg<br />
Werner, Daniel S2.1 Tue 14:10–14:30<br />
Wessels, Nicola S8.3 Tue 16:40–17:00
List <strong>of</strong> Participants 409<br />
Widany, Kai-Uwe S4.1 Tue 15:10–15:30<br />
Wiendl, Steffen S5.4 Thu 14:50–15:10<br />
Wieners, Christian S22.3 Thu 13:30–14:10<br />
Wiercigroch, Marian S5.3 Wed 16:20–16:40<br />
Willbold, Carina S20.6 Thu 16:00–16:20<br />
Willenberg, Wolfgang S2.5 Thu 15:10–15:30<br />
Willinger, Bettina S14.2 Tue 16:00–16:20<br />
Willner, Kai S4.5 Thu 13:30–14:10<br />
Wimmer, Johannes S4.2 Tue 16:20–16:40<br />
Winkler, Henrik S23.1 Tue 14:50–15:10<br />
Winkler, Max S19.2 Tue 16:40–17:00<br />
Wirowski, Artur S1.2 Tue 16:40–17:00<br />
Woźniak, Czesław S8.8 Thu 17:20–17:40<br />
Wojnarowski, Józef S20.2 Tue 16:00–16:20<br />
Wojtusch, Janis S1.4 Wed 14:10–14:30<br />
Wojtylak, Michal S23.4 Wed 17:00–17:20<br />
Wolf, Stefan S2.5 Thu 14:50–15:10<br />
Wollscheid, Daniel S6.6 Wed 14:10–14:30<br />
Worrack, Holger S6.11 Thu 17:40–18:00<br />
Worthmann, Karl Yr Ma3 Tue 10:00–10:20<br />
Wozniak, Günter<br />
Wu, Tao S8.5 Wed 17:00–17:20<br />
Wu, Tao S21.1 Tue 14:30–14:50<br />
Wulf, Hans S22.4 Thu 17:00–17:20<br />
Wulfingh<strong>of</strong>f, Stephan S6.1 Tue 14:10–14:30<br />
Wyss, Christian S23.3 Wed 15:10–15:30<br />
X<br />
Xu, Baixiang S7.4 Tue 17:20–17:40<br />
Y<br />
Y, L<br />
Yalcinkaya, Tuncay Yr Me2 Tue 10:20–10:40<br />
Yang, Yinping S1.6 Thu 14:50–15:10<br />
Yevdokymov, Dmytro S18.6 Wed 17:20–17:40<br />
Yi, Jeong-Hun S2.6 Thu 17:40–18:00<br />
Yousept, Irwin S19.5 Thu 13:30–14:10<br />
Z<br />
Zäh, Dominic<br />
Zalachas, Nicolas S7.2 Tue 14:30–14:50<br />
Zanger, Florian S14.3 Wed 14:50–15:10<br />
Zapara, Maksim S3.5 Thu 13:30–13:50<br />
Zastrau, Bernd<br />
Zehn, Manfred<br />
Zeiler, Christoph S11.1 Tue 14:30–14:50
410 List <strong>of</strong> Participants<br />
Zeppieri, Caterina Ida Ma3 Mon 17:30–18:00<br />
Zhang, Chuanzeng S3.4 Wed 17:40–18:00<br />
Zhang, Chunli S4.3 Wed 15:10–15:30<br />
Zhang, Xiaoyu S1.7 Thu 17:00–17:20<br />
Zhou, Bei S2.5 Thu 14:10–14:30<br />
Zhu, Peicheng<br />
Ziems, J. Carsten S19.2 Tue 16:00–16:40<br />
Zimmermann, Markus Yr Me1 Tue 11:20–11:40<br />
Zinatbakhsh, Seyedmohammad S7.3 Tue 16:20–16:40<br />
Zinchenko, Andrii S22.4 Thu 17:40–18:00<br />
Zingler, Paul<br />
Zolkiewski, Slawomir S3.5 Thu 14:50–15:10<br />
Zulehner, Walter<br />
Zwecker, Sandro S7.2 Tue 14:50–15:10<br />
Zwiers, Ulrike S24.2 Thu 17:00–17:20