InternatIonal Forum on aeroelastIcIty & structural DynamIcs 2013

IFASD Scientific Committee Conference
<strong>InternatIonal</strong> <strong>Forum</strong> on
aeroelastIcIty & structural
DynamIcs 2013
24 – 26 JuNE 2013 / BRISTOL, uK
Sponsored by:
BOOK YOUR PLACE AT WWW.AEROSOCIETY.COM/EVENTS

SuNDAy 23 JuNE 2013
18.00 – 20.00 – pre-Registration – Bristol Marriott Royal
pROGRAMME / DAY 1 – MONDAY 24 JUNE
08:00
08:30
08:45
09:30
10:00
10:30
11:00
11:30
12:00
Main Lecture Theatre parallel 1 parallel 2 parallel 3 parallel 4
Registration
Welcome – Opening of
IFASD 2013
Keynote 1: Future
Research Challenges
for the Loads and
Aeroelastics Discipline in
the Civil Aviation Industry
Tom Wilson, Head of
Technical Capability for
Aircraft Loads, Airbus
Operations Ltd
Networking & Coffee Break
SESSION 1:
AEROELASTIC
pREDICTION
WORKShOp 1
1A) Lessons Learned
from the Aeroelastic
prediction Workshop
Dr Jennifer Heeg,
Research Engineer, NASA
Langley Research Center
1B) Analysis of First
AIAA Aeroelastic
prediction Workshop
Results of unforced
and Oscillating
hIRENASD Wing
Bart Eussen, Senior
R&D Engineer, NLR
1C) Static and Dynamic
Aeroelastic Simulations
of hIRENASD Model
Dr Hitoshi Arizono, Associate
Senior Researcher, Japan
Aerospace Exploration
Agency Jointly presented
with Computational
Aeroelastic Analysis in Time
and Frequency Domain using
Non-Linear and Linearized
Euler/Navier-Stokes-
Methods Mark Foerster,
Research Engineer /
Scientific Employee, Institute
of Aerodynamics and Fluid
Mechanics, TU München
1D) Collaborative
hIRENASD Analyses to
Eliminate Variations in
Computational Results
Pawel Chwalowski,
Senior Aerospace
Engineer, NASA
1E) prediction of Aeroelastic
Response of the
hIRENASD Configuration
based on TRANAIR
Dr Gautam SenGupta,
Technical Fellow, The Boeing
Company. Jointly presented
with Integration of
Modal Structural Solver into
an unstructured Grid Flow
Solver for Efficient Fluid-
Structure Simulations with
Application to AepW hIRE-
NASD Test Case. Lawrence
Brase Jr, Technical Fellow,
Structures Technology, The
Boeing Company
Networking & Coffee Break
SESSION 2:
AEROELASTIC
ANALySIS 1
2A) Aircraft Aeroelastic
Stability and Response
during Wake penetration
Dr Sudha U.P.V, Scientist,
Aeronautical Development
Agency
2B) Nonlinear Flutter
Analysis for the Scaled
F-35 with horizontal Tail
Free-play
Ping-Chih Chen,
President, ZONA
Technology Inc.
2C) Identification of
Aeroelastic parameters
of helicopter Tail Rotor
Structures
Dr David Zimcik, Group
Leader Aeroacoustics
and Structural Dynamics,
National Research Council
Canada
2D) Application of the
Quadratic Mode Method
to the Aeroelastic
Analysis of Joined-Wing
Configurations
Dr Louw van Zyl, Principal
Researcher, Council for
Scientific and Industrial
Research of South Africa
2E) Wing Flutter Bench
Investigation using
Aerodynamic Force
Simulation
Prof Vsevolod Smyslov,
Chief Scientist, TsAGI
& P. Karkle, G. Lysejkin &
V. Pronin
Networking & Coffee Break
SESSION 3:
FLAppING WINGS
3A) Flapping Wing
Aeroelasticity using a
Corotational FEM and a
3D panel Method
Riccardo Gori, PhD
Student, University
Roma Tre
3B) Kinematic and
unsteady Aerodynamic
Modelling, Numerical
Simulation and parametric
Study of Flapping Wing
Ornithopter
Prof Dr Harijono
Djojodihardjo, Professor
of Aerospace Engineering,
University Putra Malaysia
3C) Simulation of Bird
Wing Flapping using the
unsteady Vortex Lattice
Method
Dr Norizham Abdul Razak,
Post Doctoral Researcher,
University of Liege
3D) A Calculus of
Variations Approach
for Manoeuvrability-
Optimum Wing
Kinematics of Flapping
MAVs Near hover
Prof Muhammad Hajj,
Professor, Virginia Tech
3E) Aeroelastic
Optimisation of
Membrane prestress on
a Flapping Wing
Prof Mayuresh Patil,
Associate Professor,
Virginia Tech
Networking & Coffee Break
SESSION 4:
OpTIMISATION 1
4A) Aeroelastic
Stochastic Optimisation,
the Mass Grid Model
Case
Rémi Arnaud, PhD
Student, ONERA
4B) The Role of
Optimisation Tools in a
Real-Life Wing Redesign
to Avoid Flutter
Torsten Bråmå, Technical
Fellow, Saab AB
4C) Confident Aircraft
Design and Development
using Robust Aeroelastic
Analysis
Dr Martin Leijonhufvud,
Senior Aeronautical
Engineer, Saab
Aeronautics
4D) Combined Optimisation
and Design of Experiment
procedures in Order to
Estimate MLGD Interface
Loads under unsteady
Aerodynamic Vibrations
Edoardo Menga,
Component Loads &
Aerolelasticity R&T –
EGLCRG Coordinator,
Airbus Operations SL &
Abarca-Lopez Ramon
4E) Aeroelastic
Sensitivities in Wing
Structural Optimisation
– An Industrial Approach
Paul Kealy, Loads and
Aeroelastics Engineer,
Airbus Operations Ltd
Networking & Coffee Break
SESSION 5:
ROTATING SySTEMS /
TuRBOMAChINERy 1
5A) An Adaption of the
p-Method to Analyse the
Aerodynamic Damping
in Tubomachinery
Considering Modal Coupling
Detlef Korte, Representative
Aeroelasticity, MTU Aero
Engines GmbH
5B) Dynamic Loads on the
Aircraft due to Engine
Imbalance at Blade Off
Prof Oleg Kuznetsov,
Principal Scientist, TsAGI
& Regina Leontieva,
Engineer, TsAGI
5C) Dealing with
harmonics and Noise
for Advanced Dynamic
Identification of In-Flight
helicopter Data
Ir Simone Manzato, Test
RTD Research Engineer,
LMS International
5D) probabilistic
Investigations of Mode
Localisation and power
Flow in a Mistuned,
Generic Rotor
Dipl.-Ing Gerrit Sinapius,
Research Assistant, DLR
5E) Aerodynamic Loading
on Bird-Damaged Fan
Blades and its Effect on
Aeroelastic Response
Eric Muir, PhD Candidate,
The University of Michigan

pROGRAMME / DAY 1 – MONDAY 24 JUNE (cont)
12:30
13:30
14:00
14:30
15:00
15:30
16:30
17:00
17:30
18:30
Main Lecture Theatre parallel 1 parallel 2 parallel 3 parallel 4
Networking Lunch
SESSION 6:
AEROELASTIC
pREDICTION
WORKShOp 2
6A) Reduced Order
Modelling of Nonlinear,
Transient Aerodynamics
of the hIRENASD Wing
Dipl.-Ing Klemens
Lindhorst, Research
Assistant, TU
Braunschweig
6B) Investigation of
Experimental uncertainty
& Computational Variation
for the hIRENASD data
sets of the Aeroelastic
prediction Workshop
Prof Melike Nikbay,
Associate Professor,
Istanbul Technical University
6C) Computation of the
unsteady Aerodynamics
of the Rectangular
Supercritical Wing
for the Aeroelastic
prediction Workshop
Dr David Schuster,
NASA Technical Fellow
for Aerosciences, NASA
Engineering and Safety
Center
6D) The Validation of
Aeroelastic Simulations
using STAR-CCM+
Coupled to Abaqus
Alan Mueller, CD-Adapco
Refreshments and
poster Sessions
SESSION 11:
AEROELASTIC
pREDICTION
WORKShOp 3
11A) Comparison of
Aeroelastic Solutions on
the hIRENASD Model
Anne-Sophie Sens,
Research Scientist,
ONERA
11B) Numerical
prediction and post-
Test Numerical Analysis
of the ASDMAD Wind
Tunnel Tests in ETW
Prof Dr.-Ing Josef
Ballmann, RET Professor
& ITAM Consultant,
ITAM GmbH
11C) Structural
Responses of the
ASDMAD Wing
Model Taking into
Consideration Actual
Wind Tunnel Flow
Conditions
Dr.-Ing. Athanasios
Dafnis, Aachen University,
Chair and Institute
of Aerospace and
Lightweight Structures
Networking Lunch
SESSION 7:
ExpERIMENTAL
METhODS 1
7A) An Actively
Controlled Air Support
System for Ground
Vibration Testing
Dr Louw van Zyl, Principal
Researcher, Council for
Scientific and Industrial
Research of South Africa
7B) New Excitation
and Measurement
Techniques to Integrate
GVT and Flight Flutter
Testing
Prof Tim De Troyer,
Lecturer, Vrije Universiteit
Brussel
7C) A New and Time
Efficient procedure for
the Identification of
Modal parameters on
Aircrafts
Dr.-Ing Yves Govers, Team
Leader Modal Testing and
Model Validation, German
Aerospace Center (DLR)
7D) Design and
Construction of
Aeroelastic Wind Tunnel
Models
Prof Ulf Ringertz,
Professor, Kungliga
Tekniska Högskolan
Refreshments and
poster Sessions
SESSION 12:
MORphING
12A) Towards
Biomimetic Morphing
of Aircraft Wings:
Feedback Control of
Aerofoil Section Shape
Dr Ranjan Vepa, Lecturer,
Queen Mary, University of
London
12B) Chiral-Rib
Structures For
Morphing Wings
Dr Giuseppe Quaranta,
Assistant Professor, Dept.
of Aerospace Science and
Technology, University
of Milan
12C) Structural and
Flight performance
Analysis of an Aircraft
with Morphing high Lift
Devices
Shijun Guo, Reader
Aeroelasticity and
Composite Structures,
Cranfield University
Networking Lunch
SESSION 8:
CONTROL
8A) Control of
Resonating FWMAV
Structures using
Repeated Eigenvalues
Hugo Peters, PhD
Researcher, Delft
University of Technology
8B) Nonlinear Control
of a Flexible Aeroelastic
System
Dr Shakir Jiffri, Research
Associate, University of
Liverpool
8C) Design of a Winglet
Control Device for Active
Load Alleviation
Dr Andreas Wildschek,
Research Engineer,
EADS Innovation Works
& Martin Herring,
Research Engineer, EADS
Innovation Works
8D) Active Control for
Flutter Suppression:
An Experimental
Investigation
Prof John Mottershead,
Alexander Elder Professor
of Applied Mechanics,
University of Liverpool
Refreshments and
poster Sessions
SESSION 13:
uNCERTAINTy 1
13A) uncertainties in
Control Surface Freeplay
and Structural
properties and their
Effect on Flutter and
LCO
Dr Dale Pitt, Boeing
Technical Fellow, The
Boeing Company
13B) uncertainty
Quantification for
Aeroelastic Analyses of
Semi-Span Supersonic
Transport (S4T) Wing
via Model Reduction
Techniques
Pinar Acar, Research
Assistant, Istanbul
Technical University
13C) uncertainty
Management Application
to Target Design Load
Setting, An Airbus
Industrial use Case
Example
Simon Coggon, Ground
Loads Modelling Expert,
Airbus
Networking Lunch
SESSION 9:
LOADS 1
9A) Ground Dynamic
Loads Calculations
Strategies for Civilian
and Military Aircrafts
Vincent Jacques,
Structural Dynamics
Engineer, Dassault
Aviation
9B) A Method for
Application of Frequency
Domain-based Load
Sources to Full-scale
Aircraft Fatigue Tests
Dr Chance McColl,
Director of Engineering –
Marietta, Technical Data
Analysis, Inc. (TDA)
9C) Robust performance
Analysis Applied to
Loads Computation of a
Flexible Aircraft
Dipl.-Ing Andreas
Knoblach, Research
Associate, German
Aerospace Center (DLR),
Institute of System and
Control
9D) Modelling Of
Aerodynamic Loads
On Flexible Bodies For
Ground Loads Analysis
Dr Yves Lemmens, Senior
Research Engineer, LMS
International
Refreshments and
poster Sessions
SESSION 14:
CERTIFICATION 1
14A) Aeroelastic
Certification of Light
Sport Aircraft According
“LTF” Regulation
Dr Jiri Cecrdle, Senior
Scientist, Aeronautical
Research and Test
Institute (VZLU)
14B) Transonic Flutter
Wind Tunnel Tests of
high Aspect Ratio Wing
Dr Carlos Bones,
Engineer, EMBRAER
S.A & Dr Olympio Mello,
Engineer, EMBRAER
S.A & Dr Breno Castro,
Engineer, EMBRAER S.A
14C) Stick-to-Stress
Real-Time Simulator
Innovation
Ping-Chih Chen,
President, ZONA
Technology, Inc. & Dr
Ned Lindsley, Research
Engineer, Air Force
Research Laboratory
(AFRL/VASD)
CLOSE OF DAy ONE – WELCOME DRINKS RECEpTION – SS GREAT BRITAIN
Networking Lunch
SESSION 10:
STRuCTuRAL
DyNAMICS
10A) Analytical Model
of Structural Damping
properties at Riveted
Lap Joint
Shigeru Machida, Senior
Researcher, Japan
Aerospace Exploration
Agency
10B) Development of
a Structural Model of
the CRM Configuration
for Aeroelastic and
Loads Analysis
Thomas Klimmek, Research
Scientist, German
Aerospace Centre (DLR),
Institute of Aeroelasticity
10C) Structural Dynamic
Response of a Wing Box
Aeroelastic Model
Dr Emanuela Bocchio,
Aeroelasticity Specialist,
Alenia Aermacchi
10D) Modal Analysis
in a Three Dimensional
Continuous-Time
State-Space unsteady
Aerodynamic Model
Noud Werter, PhD
Candidate, Delft
University of Technology
Refreshments and
poster Sessions
SESSION 15:
LOADS 2
15A) high Fidelity
Simulation of Novel
Loads Control Devices
Dr John Pattinson,
Research Engineer,
EADS Innovation Works
& Martin Herring,
Research Engineer, EADS
Innovation Works
15B) Validation
Environment for
Structural Loads
Monitoring Algorithm
Dipl.-Ing Thorben Herfeld,
Development Engineer,
DMecS Development of
Mechatronic Systems
GmbH & Co. KG
15C) Load Analysis
Method of Very Flexible
Wing/propeller System
Xie Changchuan, Master
Graduate Student,
Beihang University &
Zhang Lijuan, Master
Graduate Student,
Beihang University

pROGRAMME / DAY 2 – TUESDAY 25 JUNE
07:45
08:15
09:00
09:30
10:00
10:30
11:00
11:30
12:00
13:30
14:00
14:30
15:00
15:30
Main Lecture Theatre parallel 1 parallel 2 parallel 3
Registration
Keynote 2: Dewey Hodges,
Professor of Aerospace
Engineering, Georgia Institute
of Technology
Networking & Coffee Break
SESSION 16: hIGhLy FLExIBLE
AIRCRAFT
16A) Critical Flight Loads on
the Geometrically Nonlinear
Dynamics of Very Flexible
Aircraft
Dr Joseba Murua, Lecturer
in Aerospace Engineering,
University of Surrey
16B) Reduced-Order Aeroelastic
Models for the Dynamics of
Manoeuvring Flexible Aircraft
Henrik Hesse, PhD Research
Student, Imperial College London
16C) In-Flight Aeroelastic
System Identification of high-
Aspect-Ration Motor Glider
Alexander Köthe, Research Coworker,
Berlin Institute
of Technology
16D) Condensation of Large
Finite-element Models for
Wing Load Analysis with
Geometrically-nonlinear
Effects
Dr Rafael Palacios, Senior
Lecturer, Imperial College London
16E) preliminary Flight Test
Correlations of the x-hALE
Aeroelastic Experiment
Prof Carlos Cesnik, Professor
of Aerospace Engineering,
University of Michigan
Networking Lunch
SESSION 20: OpTIMISATION 2
20A) Design and Aeroelastic
Assessment of a Forward
Swept Wing Aircraft
Dr Wolf Krueger, Head of Division
Loads Analysis and Design,
German Aerospace Center (DLR),
Institute of Aeroelasticity
20B) On the use of Tow-
Steered Composites for
Aeroelastic Tailoring
Olivia Stodieck, PhD Researcher
in Aerospace Engineering,
University of Bristol
20C) The Needs to Incorporate
Aeroelastic Aspects into the
Conceptual Design process
Dipl.-Ing Johannes Schweiger,
Conceptual Design Analysis,
Cassidian
20D) Multidisciplinary
Optimisation of Flexible
Aircraft in Flight with
Superimposed Static and
Dynamic Aeroelastic Loads
Ogmundur Petersson, Specialist,
Cassidian Air Systems
Networking & Tea Break
Networking & Coffee Break
SESSION 17: COMpuTATIONAL
AEROELASTICITy 1
17A) Forced Motion Simulations
using a Linear Frequency
Domain Solver For a Generic
Transport Aircraft
Reik Thormann, Scientist, DLR,
Institute of Aeroelasticity
17B) Forced Response
Calculation using TWIN
Approach
Dr Majid Mesbah, Researcher,
Cenaero
17C) A Reduced-Order Model
for Aeroelastic Studies on
Circulation Controlled Wings
Dipl.-Ing Ian Krukow, Research
Assistant, TU Braunschweig
17D) Roll Damping Derivative from
Wind Tunnel Forced-Oscillation
Tests and Generalised Lifting –
Surface Aerodynamic Theory
Anthony Pototzy, Aeroelasticity
Branch, NASA Langley Research
Center
17E) Efficient Identification of
Aerodynamic and Aeroelastic
Models using Coupled CSD-
CFD Simulations
Taehyoun Kim, Associate
Professor, National University of
Singapore
Networking Lunch
SESSION 21: COMpuTATIONAL
AEROELASTICITy 2
21A) Role of Mach Number
Freeze in Transonic Flutter
Prof Oddvar Bendiksen,
Professor, University of
California
21B) Influence of Transitional
Flows at Transonic Mach
Numbers on the Flutter Speed
of a Laminar Airfoil
Michael Fehrs, Research Assistant,
(DLR) – Institute of Aeroelasticity
21C) Time Integration Schemes’
Influence on partitioned
Method for the Fluid–Structure
Coupling procedure
Guillaume Bénéfice, PhD
Student, Ecole Centrale Lyon
21D) Extension of the Non-
Linear harmonic Method to
Flow Computation Around
Moving and Deforming
Structures
Francois Debrabandere,
Development Engineer, Numeca
International
Networking & Tea Break
Networking & Coffee Break
SESSION 18:
LOADS 3
18A) New Method for
horizontal Tail plane Buffeting
Loads prediction
Raul Calderon, Engineer/PhD
Student in Aerodynamics, Airbus
Operations S.A.S
18B) A New Methodology for the
Estimation of Structural Load
Level due to Complex unsteady
Aerodynamic Excitation
Hadrien Mamelle, Structural
Dynamics Engineer, Dassault
Aviation
18C) use of Linearized CFD for
unsteady Aerodynamics for
Gust Loads
Guillermo Jenaro, HO Dynamic
Loads, Airbus Operations GmbH &
Jörg Hasselbring , Dynamic Loads
Engineer, Airbus Operations GmbH
18D) Continuous Turbulence
Design Loads Calculation in
presence of Non-linear Controls
Prof Sergio Ricci, Associate
Professor, University of Milan
18E) Identification of unsteady
Aerodynamic Loads using
Aeroelastic Response and
Kalman Filter
Prof Luiz Góes, Professor,
ITA - Aeronautical Institute of
Technology & Roberto Gil A da
Silva, Professor, ITA – Aeronautical
Institute of Technology
Networking Lunch
SESSION 22: FLuTTER
22A) A Consistent Strip Theory
for T-tail Flutter Computations
Prof Pablo Garcia-Fogeda,
Professor of Aeroelasticity, EIAE-
UPM
22B) T-Tail Flutter:
potential-flow Modelling and
Experimental Validation
Dr Joseba Murua, Lecturer
in Aerospace Engineering,
University of Surrey
22C) Experimental and
Computational Investigation
of a Full Aircraft Flutter at
Transonic Speeds
Prof Qian Wei, Senior Engineer,
Shenyang Aircraft Design &
Research Institute
Networking & Tea Break
Networking & Coffee Break
SESSION 19:
NONLINEARITy 1
19A) Analysis for a Threedimensional
Structurally
Nonlinear Wing with a Control
Surface
Prof SangJoon Shin, Associate
Professor, Seoul National
University
19B) Nonlinear Analysis of the
Influence of Aircraft Dynamics
on Nose Landing Gear Shimmy
Nandor Terkovics, PhD Student,
University of Bristol
19C) Nonlinear Aeroelastic
Response of a flat panel.
A Normal Form Approach
Marco Eugeni, PhD Student,
University of Rome “La Sapienza”
19D) Nonlinear Dynamic
Analysis of an F-16 Aircraft
using GVT Data
Simone Manzato, RTD Test
Research Engineer,
LMS International
19E) Application of Nonlinear
Geometrical Effects to the
Analysis of Structural Loads
using Fast Evaluation Methods
Dr.-Ing Moriz Dirk Scharpenberg,
Flight Physics Engineer, Airbus
Networking Lunch
SESSION 23: NONLINEARITy 2
23A) Instability of Aeroelastic
Systems with Softening
Nonlinearity
Xiaojun Wei, PhD Student,
University of Liverpool
23B) Limit-Cycle Oscillations of
Supercritical Airfoils
Anna Van Rooij, PhD Candidate,
German Aerospace Center (DLR)
23C) Identification of Structural
Non-linear Stiffness and
Damping parameters using the
Restoring Force Surface Method
Dr Marc Boeswald, Head of
Department of Structural
Dynamics, German Aerospace
Center (DLR)
23D) Limit-Cycle-Oscillation
Simulations of Aerostability
Windtunnel Experiments
Bernd Stickan, Development
Engineer, Airbus
Networking & Tea Break

pROGRAMME / DAY 2 – TUESDAY 25 JUNE (cont)
16:00
16:30
17:00
17:30
19:00
Main Lecture Theatre parallel 1 parallel 2 parallel 3
SESSION 24:
GuSTS 1
24A) Gust Loads Alleviation
Based on Model predictive
Control
Hans-Gerd Giesseler, Expert,
Airbus Operations GmbH
24B) high Fidelity Numerical
Simulations for Gust Response
Analysis
Dr Fabien Huvelin, Research
Engineer, ONERA
24C) DLM-Correction Methods
for Aerodynamic Gust
Response prediction
Diliana Dimitrov, Research
Assistant, Institute of
Aeroelasticity, German
Aerospace Center (DLR)
24D) Reduced Order Modelling
for the Gust Response of the
FFAST Wing
Dr Christopher Wales, Research
Associate, University of Bristol
Dinner sponsored by:
SESSION 25:
COMpuTATIONAL
AEROELASTICITy 3
25A) Evaluation of Linear,
Inviscid, and Viscous
Aeroelastic Solutions of the
AGARD 445.6 Wing using
Reduced–Order Modeling and
Root Locus Solutions
Dr Walter Silva, Senior Research
Scientist, NASA Langley
Research Center
25B) Dynamic Stability and
Response Analyses using a
Small-Disturbance CFD Method
Cyrille Vidy, Development
Engineer, Cassidian (EADS
Germany)
25C) Small Disturbance
Navier-Stokes Investigations
of Fighter-Type-Delta-Wing
pitching Oscillations
Dipl.-Ing Alexander Pechloff,
Research Engineer, TU Munich
25D) A 3-D Zero-Lift Drag
prediction including Aeroelastic
Effects
Dr Raymond Kolonay, Aerospace
Engineer, United States Air Force
Research Lab
SESSION 26:
ROTATING SySTEMS /
TuRBOMAChINERy 2
26A) On the use of
Radial Basis Functions to
Numerically predict Flutter in
Turbomachinery
Yannick Rozenberg, Associate
Professor, University Lyon 1
– LMFA
26B) Structural Dynamic
Analysis of a Vertical Axis
Wind Turbine with Troposkien
Geometry
Amin Fereidooni, M.A.Sc
Student, Carleton University
26C) Nodal Energy Weighted
Transformation: A New
Mistuning projection for FladeTM Systems
Colin Fitzner, Graduate Student
Research Assistant, University of
Michigan
26D) Numerical
Investigation of a Contrafan
Aeroelastic Response with
Multichorochronic Boundary
Conditions
Dr Antoine Placzek, Research
Engineer, ONERA
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SESSION 27:
CERTIFICATION 2
27A) Development of a New Tool
for Static Aeroelastic Analysis
Applied on the SAAB Gripen
Fighter Aircraft
Hans Soderberg, Senior
Engineer, SAAB Aeronautics
27B) Flight Test Validation of
Wake Vortex Encounter Loads
Dr Héctor Climent, Head of
Structural Dynamics and
Aeroelasticity, Airbus Military
27C) Flutter Wind Tunnel Tests
for a Regional Aircraft
Hiroyuki Morino, Manager,
Mitsubishi Aircraft Corporation
& Satoshi Yonemoto, Mitsubishi
Heavy Industries, Ltd
27D) Store Ejection
Simulations on a Rafale Aircraft
Guillaume Reinhardt, Engineer,
Dassault Aviation
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SyNOpSIS
The International <strong>Forum</strong> on Aeroelasticity and
Structural Dynamics (IFASD) is the key international
conference for engineers and scientists working in
the fields of Aeroelasticity and Structural Dynamics.
The forum has been running since 1981 and, following
on from the success of IFASD2011 held in Paris, the
2013 <strong>Forum</strong> will be held in Bristol, UK, the centre of
the UK’s aerospace industry
IFASD2013 will be organised by the Royal Aeronautical
Society (RAeS), in collaboration with the Council
of European Aerospace Societies (CEAS) and the
American Institute of Aeronautics and Astronautics
(AIAA). The <strong>Forum</strong> Chair will be Professor Jonathan
Cooper, who holds the Royal Academy of Engineering
Airbus Sir George White Chair of Aerospace
Engineering at the University of Bristol.
IFASD2013 will consist of about 200 technical
presentations and posters providing a comprehensive
snapshot of the current status of industrial practice
and research activities in the fields of Aeroelasticity
and Structural Dynamics, covering all TRLs (Technology
Readiness Levels) from blue sky research through
to applications on full scale aerospace structures.
The technical sessions will include: the Aeroelastic
Prediction Workshop, Certification, Computational
Aeroelasticity, Control, Experimental Methods,
Flapping Wings, Flutter, Gusts, Highly Flexible Aircraft,
Loads, Morphing, Nonlinearity, Optimisation, Rotating
Systems, Smart Structures, Structural Dynamics,
Turbo-Machinery and Uncertainty.
ThE KEyNOTE SpEAKERS ARE:
Tom Wilson – Head of Technical Capability for Aircraft
Loads, Airbus.
Dewey hodges – Professor of Aerospace Engineering,
Georgia Institute of Technology.
FOR MORE INFORMATION AND TO REGISTER www.ifasd2013.com
Dr Wolf Kruger – Head of Loads Analysis and Aeroelastic
Design, DLR Institute of Aeroelasticity.
TEChNICAL VISITS – 27 JuNE 2013
Technical visits will be held to Airbus and other local
aerospace industries.
SOCIAL
Social events will include a reception on Brunel’s SS
Great Britain and a dinner to be held at the
@Bristol Science Centre.
WhO ShOuLD ATTEND
IFASD2013 will provide an excellent opportunity for
scientists and engineers from industry, government
and universities to exchange knowledge and findings
from current studies, and to discuss directions for
future research.
VENuE
Bristol Marriott Royal Hotel, Bristol, BS1 5TA, UK
CONTACT uS
Conference & Events
Royal Aeronautical Society
No.4 Hamilton Place
London, W1J 7BQ, UK
+44 (0)20 7670 4345
conference@aerosociety.com
www.aerosociety.com/events

pROGRAMME / DAY 3 – WEDNESDAY 26 JUNE
07:45
08:15
09:00
09:30
10:00
10:30
11:00
11:30
12:00
Exhibitors attending:
Supporters:
Main Lecture Theatre parallel 1 parallel 2 parallel 3
Registration
Keynote 3: Dr Wolf Krueger,
Head of Division Loads Analysis
and Design, German Aerospace
Center – DLR, Institute of
Aeroelasticity
Networking & Coffee Break
SESSION 28:
OpTIMISATION 3
28A) An Aeroelastic Multi
Fidelity Approach for
Aeroelastic Tailoring
Dr Roeland De Breuker, Assistant
Professor, Delft University of
Technology
28B) preliminary Design and
Optimisation for Flexible
Aircraft in a Distributed
Environment
Pier Davide Ciampa, German
Aerospace Center (DLR)
28C) parametric Studies for
Wing Mounted Fins
Ping-Chih Chen, President, ZONA
Technology, Inc.
28D) Automated Creation
of Aeroelastic Optimisation
Models from a parameterised
Geometry
Reinhold Maierl, PhD Student,
CASSIDIAN Air Systems
28E) Multi-Disciplinary
Wing Optimisation using a
Discipline-Specific Trust-
Region Method
Dr Simão Marques, Lecturer in
Aerospace Engineering, Queen’s
University Belfast
Networking Lunch
proceedings
Proceedings from this event are free to
delegates. If you are unable to attend and would
like to purchase a copy, then additional copies
can be purchased from the Royal Aeronautical
Society or by completing the registration form
below. Information on past conferences can be
found at www.aerosociety.com/proceedings.
Networking & Coffee Break
SESSION 29:
COMpuTATIONAL
AEROELASTICITy 4
29A) Grid Deformation for
Computational Aeroelastic
Analysis using RBF Interpolation
with Standard Greedy Method
Haris Hameed Mian, Postgraduate
Student, Northwestern
Polytechnical University
29B) A partitioned Method
for the Direct Aeroelastic
Simulation of Free-Flying
Aircraft
Georg Wellmer, Loads Engineer,
Cassidian
29C) Structural Response
prediction of Surface panels in
hypersonic Flow
Prof Jack McNamara, Associate
Professor, The Ohio State
University
29D) Time Domain Aeroelastic
Solution using Exact
Aerodynamic Influence
Coefficients and Nonlinear
Damping
Dr Vin Sharma, Flutter Engineer,
Air Force SEEK EAGLE Office
29E) Investigation of
Interaction of Shock Movement
with Structural Elastic
Deformations in Transonic Flow
Dr Svetlana Kuzmina, Leading
Scientific Researcher, TsAGI &
Dr Mikhail Zichenkov, Head of
A/C Structure Strength Complex,
TsAGI & Dr Fanil Ishmuratov,
Head of Static Aeroelesticity
Divison, TsAGI
Networking Lunch
Networking & Coffee Break
Sponsorship and exhibition space
Please contact the Conference & Events
Department for details on exhibiting,
sponsorship and insertion of information into
delegate packs on 020 7670 4345.
SESSION 30:
LOADS 4
30A) Fast prediction of Worst
Case Gusts Loads
Hamed Haddad Khodaparast,
Lecturer, College of Engineering,
Swansea University
30B) Wake Vortex Encounter
Loads Numerical Simulation
Sebastián Claverías-Ceacero,
Structural Dynamics and
Aeroelasticity Engineer, Airbus
Military
30C) An Integrated Loads
Analysis Model for Wake Vortex
Encounters
Dipl.-Ing Thiemo Kier, Research
Engineer, German Aerospace
Center (DLR)
30D) Efficient, Laplace-
Domain Aerodynamics for Load
Analyses
Natascha Jansson, Doctoral
Student, Royal Institute of
Technology (KTH)
30E) Numerical Study on the
Fluid-Structure Coupling
Behaviour of Cascade-Type
Thrust Reverser units for
Weight Optimisation
Dr Luis Teia Gomes, Installation
Aerodynamics Development
Engineer, Rolls-Royce
Deutschland Ltd & Co KG
Networking Lunch
Cancellations
In the event of cancellation, terms and
conditions will apply. Please go to
www.aerosociety.com/events for more details.
FOR MORE INFORMATION AND TO REGISTER www.ifasd2013.com
Networking & Coffee Break
SESSION 31:
NONLINEARITy 3
31A) Combined Frequency
and Time Domain Solutions for
Aeroservoelastic Response
with Nonlinearities
Prof Moti Karpel, Professor,
Technion – Israel Institute of
Technology
31B) Nonlinear Reduced
Order Models of unsteady
Aerodynamics for Non-classical
Aileron Buzz Analysis
Francesca Fusi, PhD Candidate,
University of Milan
31C) Investigations of Transonic
Aircraft in the Joint DLR /
ONERA project Non-Linear
Aeroelastic Simulation, NLAS II
Prof Wolf Krueger, Head of Loads
Analysis and Aeroelastic Design
Department, German Aerospace
Center – DLR & Philippe Girodroux-
Lavigne, Head of Modelling
and Numerical Simulation of
Aeroelasticity Research Unit,
ONERA – The French Aerospace Lab
31D) Aeroelastic Design
Exploiting Structural
Geometric Nonlinearities
Prof Jonathan Cooper, Airbus Sir
George White Chair of Aerospace
Engineering, University of Bristol
31E) Geometrically Non-linear
Structural Modal Analysis for
Local and Impulsive Excitation
Lars Oliver Bernhammer, PhD
Student, Delft University of
Technology
Networking Lunch
hotel Accommodation
To book a room at the Marriott Royal, please
visit www.ifasd2013.com for more details.
Rooms have been reserved on behalf of the
delegates, please mention the conference
and the RAeS if calling directly to receive
the discount.

pROGRAMME / DAY 3 – WEDNESDAY 26 JUNE (cont)
13:30
14:00
14:30
15:00
15:30
16:00
16:30
17:00
17:30
Main Lecture Theatre parallel 1 parallel 2 parallel 3
SESSION 32:
ExpERIMENTAL METhODS 2
32A) Flutter Wind Tunnel
Test at high Transonic Mach
of a Flexible Empennage with
Variable Control Surface Free–
play and Stiffness
Paul Taylor, Principal Engineer,
Gulfstream Aerospace
Corporation
32B) A400M Flight Vibration
Survey for Equipment
Environmental Qualification
Marc Montagne, Vibration Team
Leader, Airbus Military
32C) Experimental
Investigation of the Aeroelastic
Behaviour of a Laminar Wing in
Transonic Flow
Anne Hebler, Research Engineer,
German Aerospace Center (DLR)
32D) Stability Assessment of
a propeller-Wing Wind Tunnel
Model Based on Analysis using
Measured Structural Data and
Online-Monitoring
Dipl. Ing Alireza Rezaeian,
Aerospace Engineer, Research
Associate, German Aerospace
Centre (DLR), Institute of
Aeroelasticity
Networking & Tea Break
SESSION 36:
GuSTS 2
36A) Linear Reduced Order
Modelling for Gust Response
Analysis using the DLR-TAu
Code
Dr Sebastian Timme, Lecturer,
University of Liverpool
36B) Comparison of Different
Approaches for Gust Modelling
in the CFD Code TAu
Dr Ralf Heinrich, Team Leader
of Group “Multidisciplinary
Modeling”, German Aerospace
Center (DLR)
36C) high-Fidelity Simulation
of Aeroelastic Wind Gust Effect
in Aerodynamic Shapes
Dr Ruben Sevilla, Lecturer,
Swansea University
ThuRSDAy 27 JuNE 2013
SESSION 33:
COMpuTATIONAL
AEROELASTICITy 5
33A) Sensitivity Evaluation
in Transonic Fluid-Structure
Interactions
Prof Marilyn Smith, Associate
Professor, Georgia Institute of
Technology
33B) Computational Aeroelastic
Analysis of the Semi-Span
Super-Sonic Transport (S4T)
Wind-Tunnel Model
Mark Sanetrik, Research
Engineer, NASA Langley
Research Center
33C) A Novel Computational
Approach to unsteady
Aerodynamic and Aeroelastic
Flow Simulation
Eliot Quon, Graduate Research
Assistant, Georgia Institute of
Technology
33D) Aerodynamic
Optimisation of a Flexible
high-Lift Wing
Giuseppe Trapani, EngD
Researcher, Cranfield University
Networking & Tea Break
SESSION 37:
COMpuTATIONAL
AEROELASTICITy 6
37A) The NASA high Speed
ASE project: Computational
Analyses of a Low-Boom
Supersonic Configuration
Dr Walter Silva, Senior Research
Scientist, NASA Langley
Research Center
37B) A Time-Spectral
Aeroelastic Method for
Transonic Flutter prediction
Dr Gaetan Kenway, Post Doctoral
Researcher, University of
Michigan
37C) using proper Orthogonal
Decomposition and Dynamic
Mode Decomposition Methods
for Comparing CFD Results
Experimental Measurements
Amandine Guissart, PhD
Student, University of Liège
SESSION 34:
AEROELASTIC ANALySIS 2
34A) Modelling and Analysis
of the Flight Dynamics of a
Deformable Aircraft with
Structurally-Linearized Full
Inertial Coupling
Antônio Bernardo Guimarães
Neto, Master’s Student,
Technological Institute of
Aeronautics (ITA)
34B) Modelling of Damage in
Laminated Composite plates
and Nonlinear Flutter Analysis
Dr Ranjan Vepa, Lecturer, Queen
Mary, University of London
34C) Stability Enhancement of
a Transonic Wing using a Simple
passive Attachment
D. Michael McFarland, Research
Associate Professor, University
of Illinois at Urbana-Champaign
34D) Spectral Finite Element
Modelling and updating in
Aeroelastic Analysis of Light
Sport Aircraft
Joseph Gross, Research
Associate, Hamburg University
of Technology
Networking & Tea Break
SESSION 38:
uNCERTAINTy 2
38A) uncertainty
Quantification in Aeroelastic
Composite Structures using
Lamination parameters
Prof Carl Scarth, PhD student,
ACCIS Centre, University of
Bristol
38B) Application of uncertainty
Management to Improve
Reliability of hard Landing
Criticality Assessment Criteria
Thomas Wilson, Head of Ground
Loads, Airbus UK
38C) uncertainties in
Measurements and Data
Evaluation Concerning
Transonic high Reynolds
Number Wind Tunnel Tests
Dr Alexander Boucke, Scientist,
ITAM GmbH
CLOSING CEREMONy AND IFASD2015 ANNOuCEMENT
Technical Tours to Airbus and other local aerospace industries
FOR MORE INFORMATION AND TO REGISTER www.ifasd2013.com
SESSION 35:
ROTATING SySTEMS /
TuRBOMAChINERy 3
35A) Counter-Rotating
Open Rotor Whirl Flutter
phenomenon. Investigations
using elsA solver
Dr Simon Verley, Research
Scientist, ONERA
35B) propeller – Flexible
Wing Interaction using Rapid
Computational Methods
Chenhui Liu, Flight Physics
Engineering Intern, Airbus
35C) Aeroelastic Design Study
of Subsonic high pressure
Turbine Blades for Space
Applications
Dr Pieter Groth, Senior
Aerodynamic Design Engineer,
GKN Aerospace Sweden
35D) Numerical Investigation of
an L-Shaped Deployable Gurney
Tab for Rotorcraft Vibration
Control
Valentina Motta, PhD Candidate,
University of Milan
Networking & Tea Break
SESSION 39:
SMART STRuCTuRES
39A) Aeroelastic Simulations of
the SADE FNG Smart Leading
Edge – Smart Single Slotted
Flap high-Lift Configuration
Dr Mats Dalenbring, Senior
Researcher, Swedish Defence
Research Agency (FOI)
39B) Adaptive Camber and
Chord Morphing Wing with
0-ʋ honeycomb Compared to
Conventional Wing
Ashley Dale, PhD Research
Student, University of Bristol
39C) Loads, Vibration and
Manoeuvre Control using
Active Floating Flaps
Mark Pustilnik, Master Student –
the Aerospace Faculty, Technion