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3rd Aircraft Structural Design Conference Programme

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Structures & Materials Group <strong>Conference</strong><br />

3RD AIRCRAFT STRUCTURAL<br />

DESIGN CONFERENCE<br />

9 - 11 OCTOBER 2012 / DELFT UNIVERSITY, THE NETHERLANDS<br />

Sponsored by: Supported by:<br />

BOOK YOUR PLACE AT WWW.AEROSOCIETY.COM/EVENTS


MONDAY 8 OCTOBER 2012<br />

18:00 - 20:00 - Welcome Reception and Registration<br />

PROGRAMME / DAY ONE - 9 OCTOBER 2012<br />

08.00<br />

08.30<br />

08.45<br />

09.30<br />

09.55<br />

10.20<br />

10.50<br />

11.15<br />

11.40<br />

12.05<br />

12.30<br />

13.30<br />

13.55<br />

14.20<br />

14.45<br />

16.00<br />

16.25<br />

16.50<br />

17.15<br />

Registration and Coffee<br />

<strong>Conference</strong> Welcome and Announcements<br />

Keynote<br />

Zafer Gurdal, Aerospace Structures Chair, Faculty of Aerospace<br />

Engineering, Delft University of Technology<br />

SESSION 1: COMPOSITES<br />

1A) Damage Analysis of Bonded Repairs in Composites using<br />

Digital Image Correlation Methods<br />

Dr Miguel Caminero, Lecturer, University of Castilla-La Mancha<br />

1B) Post-Buckling of Variable Angle Tow Composites using<br />

Variational Approach<br />

Dr Zhangming Wu, Research Assistant, ACCIS Centre<br />

Networking Break<br />

1C) Failure Mode Transition During Delamination of Thick<br />

Unidirectional L-Shaped Composite Laminates<br />

Demirkan Coker, Middle East Technical University<br />

1D) A Tool for the Automated <strong>Design</strong> of Multistable Composite<br />

Parts<br />

Luis Falcao, PhD Student, Instituto Superior Tecnico<br />

1E) Theoretical, A-Basis and B-Basis <strong>Design</strong> Allowables Failure<br />

Envelopes for Open Hole Composite Laminates using Smooth<br />

Specimens Material Property Database with Uncertainty<br />

Estimation<br />

Prof Carlos Cimini, Professor, UNICAMP – University of Campinas,<br />

Brazil<br />

1F) <strong>Design</strong> Exploration Methodology for Ultra Thick Laminated<br />

Composites<br />

Jacinto Carrasco, PhD Student, Cranfield University<br />

Networking Lunch<br />

SESSION 3: COMPOSITES<br />

3A) The Impact of <strong>Structural</strong> Component Complexity and Scale<br />

on the Cost of Automated Prepreg Ply Layup<br />

Matthew Mullan, PhD Student, Queens University<br />

3B) Unitised Damage-Tolerant Hybrid GLARE-CFRP Composite<br />

Structures for Unmanned Air Vehicles<br />

David Kordonowy, Aerostructures Research Group Manager, Aurora<br />

Flight Sciences<br />

3C) CFRP Wing Skin <strong>Design</strong> Under Consideration of Impact<br />

Damage and Aero Elastic Stiffness Requirements<br />

Ir Cyril Wentzel, Researcher, Delft University of Technology<br />

Break and travel to Koiter and Wall of Fame<br />

SESSION 4: TOPOLOGY / SHAPE<br />

4A) Effect of Wing-Box Structure on the Optimum Wing Outer<br />

Shape<br />

Ali Elham, PhD Researcher, Delft University of Technology<br />

4B) Using Topology Optimisation in Conceptual Wing <strong>Design</strong>,<br />

Luis Félix, Academia da Força Aérea Portuguesa<br />

4C) The Use of Topology Optimisation in the Conceptual <strong>Design</strong> of<br />

a Next Generation Lattice Composite Fuselage Structure<br />

Steffen Niemann, Scientist, DLR / German Aerospace Centre<br />

Prof Vassili Toropov, University of Leeds<br />

4D) Challenges in Shape Optimisation of Curved Surfaces with<br />

Openings<br />

Dan Wang, Northwestern Polytechnical University<br />

RECEPTION AT AEROSPACE ENGINEERING FACILITY<br />

SESSION 2: IMPACT / DYNAMICS<br />

2A) <strong>Aircraft</strong> Seat Compliance (CS25.562) Against Seat Track<br />

Predistortion Load Case: Use of Numerical Simulation Tools for<br />

Concept Development<br />

Omkar Gulavani, PhD Researcher, Cranfield University<br />

2B) Simulation of Composite Crush Structures<br />

Dr Alan Prior, Director SIMULIA North-Nordics CSE, Dassault Systemes<br />

Networking Break<br />

2C) Random Vibration of A Rectangular FGM Strip<br />

Dr Vedat Dogan, Faculty Member, Istanbul Technical University<br />

2D) Behavioural Study of a Landing Gear (under Abnormal Landing<br />

Conditions)<br />

Amanda Sibanda, Student, University of the West of England<br />

2E) Dynamics Analysis of <strong>Aircraft</strong> Wing Electro-Impulse De-Icing<br />

Process<br />

Dr Yongjie Zhang, Senior Lecturer, School of Aeronautics, Northwestern<br />

Polytechnical University<br />

Networking Lunch<br />

KOITER SESSION I<br />

K1A) An Isogeometric Layerwise Model for Composite Laminates<br />

Yujie Guo, PhD Candidates, ASCM, Delft University of Technology<br />

K1B) A Fast Procedure for the <strong>Design</strong> of Composite Stiffened Panels<br />

Dr Riccardo Vescovini, Post-Doctoral Fellow, Politecnico di Milano<br />

(POLIMI)<br />

K1C) Post-Buckling Analysis of Composite Stiffened Panels under<br />

Dynamic In-Plane Loading<br />

Dr Eelco Jansen, Senior Faculty Member, Leibniz Universität Hannover,<br />

Institute of <strong>Structural</strong> Analysis<br />

Break and travel to Koiter and Wall of Fame<br />

KOITER SESSION II<br />

K2A) A Koiter-Newton Approach for Nonlinear <strong>Structural</strong> Analysis<br />

Ke Liang, PhD Researcher, Delft University of Technology<br />

K2B) Cross-Sectional Modelling of Thin-Walled Composite Beams<br />

with Initial Twist and Taper<br />

Etana Ferede, PhD Student, Delft University of Technology<br />

K2C) A Component-Wise Approach for the Analysis of Metallic and<br />

Composite <strong>Aircraft</strong> Structures<br />

Prof Erasmo Carrera, Full Professor, Politecnico di Torino<br />

FOR MORE INFORMATION AND TO REGISTER www.aerosociety.com/events


PROGRAMME / DAY TWO - 10 OCTOBER 2012<br />

08.00<br />

08.45<br />

09.30<br />

09.55<br />

10.20<br />

10.50<br />

11.15<br />

11.40<br />

12.05<br />

12.30<br />

13.30<br />

13.55<br />

14.20<br />

14.45<br />

15.10<br />

15.40<br />

16.05<br />

16.30<br />

16.55<br />

17.20<br />

17.45<br />

18.15<br />

Registration and Coffee<br />

Keynote: Multifidelity Modeling for <strong>Aircraft</strong> <strong>Design</strong> and<br />

Optimisation<br />

Prof Karen Willcox, Professor of Aeronautics and Astronautics,<br />

Massachusetts Institute of Technology<br />

SESSION 5: MDO<br />

5A) A Bi-Level High Fidelity Aero-<strong>Structural</strong> Integrated <strong>Design</strong><br />

Methodology<br />

Christophe Blondeau, Research Engineer, ONERA<br />

5B) A Robust Multidisciplinary Approach to Aerostructural <strong>Design</strong><br />

Dr Andrew March, Research Assistant, Massachusetts Institute of<br />

Technology<br />

Networking Break<br />

5C) Multi-Objective Optimisation Strategies for <strong>Aircraft</strong> Multi-<br />

Disciplinary <strong>Design</strong><br />

Stefania Gemma, PhD Student, University of Rome “La Sapienza”<br />

5D) Multi-Modeling Approach in Pre-<strong>Design</strong>ing of Fuselage / Wing<br />

Section Consisted of Stiffened Composite Panels<br />

Dr Victor Fomin, Leading Scientific Resercher, TsAGI<br />

5E) <strong>Design</strong> of a Composite Forward Swept Wing using Advanced<br />

Aeroelastic Tailoring Optimisation Methods<br />

Noud Werter, PhD Student, Delft University of Technology<br />

5F) Multidisciplinary <strong>Design</strong> and Optimisation of <strong>Aircraft</strong> Box<br />

Structures<br />

Reinier van Dijk, PhD Candidate, Delft University of Technology<br />

Networking Lunch<br />

SESSION 7: OPTIMISATION<br />

7A) <strong>Structural</strong> Optimisation of <strong>Aircraft</strong> Concepts through a Hyper-<br />

Heuristic Approach<br />

Jonathan Allen, Research Postgraduate, Durham University<br />

7B) The AIRBUS <strong>Structural</strong> Rapid Sizing Tool based on LMS<br />

Samtech CÆSAM Framework<br />

Dr Malherbe Ghislaine, Business Developer Manager, LMS SAMTECH<br />

7C) Simultaneous <strong>Design</strong> of <strong>Structural</strong> Layout and Discrete Fibre<br />

Orientation of Composite <strong>Aircraft</strong> Structures using a Bi-Value<br />

Coding Parameterization<br />

Prof Pierre Duysinx, Professor, University of Liege<br />

7D) Efficient Optimisation of Large <strong>Aircraft</strong> Fuselage Structures<br />

Jos Vankan, Senior Scientist, National Aerospace Laboratory – NLR<br />

Networking Break<br />

7E) Enhance Derivative <strong>Design</strong> Considering Global Sensitivity of<br />

<strong>Design</strong> Parameters<br />

Dr Kamran Behdinan, Professor, University of Toronto<br />

7F) Parameter Free Optimisation for the <strong>Design</strong> of Large and<br />

Lightweight Composite Structures<br />

Mr Michael Fischer, Research Associate and Chair of <strong>Structural</strong><br />

Analysis, Technische Universität München<br />

7G) Optimised <strong>Design</strong> of Stiffened Panels Using Variable Angle<br />

Tows<br />

Dr Wenli Liu, Research Officer, University of Bath<br />

7H) <strong>Design</strong>, Analysis and Optimisation of Thin Walled Semi-<br />

Monocoque Wing Structures using Different <strong>Structural</strong><br />

Idealisations in the Preliminary <strong>Design</strong> Phase<br />

Prof Altan Kayran, Faculty Member, Middle East Technical University<br />

7J) Detail <strong>Design</strong> of the Tail Unit of a Newly <strong>Design</strong>ed Agricultural<br />

<strong>Aircraft</strong><br />

Ahmed Gubaratalla, Teaching Assistant, Sudan University of Science<br />

and Technology<br />

CLOSE OF DAY AND DEPARTURE FOR CONFERENCE DINNER.<br />

SESSION 6: DESIGN PHILOSOPHY<br />

6A) An Improved Stress-Strain Curve Model for Advanced Materials<br />

Dr Frédéric Bron, R&D Engineer, Aerospace Products, Constellium CRV<br />

6B) Efficient Finite Element Simulation of <strong>Aircraft</strong> Fasteners and<br />

Joints<br />

Dr Alan Prior, Director SIMULIA North-Nordics CSE, Dassault<br />

Systemes<br />

Networking Break<br />

6C) Damage Tolerance <strong>Design</strong><br />

Prof Luis Reis, Associate Professor, Instituto Superior Técnico<br />

6D) Evaluation of <strong>Structural</strong> Loads<br />

Pedro Albuquerque, TAP Portugal Group<br />

6E) FAA Certification of Pressurised <strong>Aircraft</strong> Crack Initiation &<br />

Propagation Analysis Supported by Test<br />

Dr Frank Abdi, Chief Technical Officer, AlphaStar Corporation<br />

6F) Adaptive Camber-Morphing Wing with Optimised Composite<br />

Laminate Lay-Up<br />

Ashley Dale, Postgraduate Research Student, University of Liverpool<br />

Networking Lunch<br />

SESSION 8: MORPHING<br />

8A) Span Morphing: <strong>Design</strong>, Modelling, and Optimisation<br />

Rajic Ajaj, Research Assistant, Swansea University<br />

8B) Aeroelastic Characterisation of Corrugated Skins for Wing<br />

Morphing<br />

Dr Narcis Ursache, School of Engineering, Brunel University<br />

8C) Combining Active and Passive Load Alleviation Techniques in<br />

Transport <strong>Aircraft</strong> <strong>Structural</strong> <strong>Design</strong><br />

Felix Stroscher, Research Assistant, Technische Universitat Munchen<br />

8D) Stiffness and Layout Tailoring of a Morphing High-lift System<br />

with Aeroelastic Loads<br />

Dr Glenn Thuwis, PhD Researcher, Delft University of Technology<br />

Networking Break<br />

8E) Static and Dynamic Analysis and Comparison of Fixed and<br />

Morphing Wing Equipped UAV <strong>Aircraft</strong>: Optimal Control Calculation<br />

and Energy Estimates Evaluation<br />

José Lobo do Vale, Researcher, IST Lisbon - Aerospace Group<br />

8F) <strong>Design</strong> of Morphing Wing Structures by using <strong>Structural</strong><br />

Topology Optimisation<br />

Prof Liyong Tong, Professor, The University of Sydney<br />

8G) Onboard Damage Control Technique (ODCT)<br />

Abdul Sayeed Khan, Student, SRM University<br />

Mohamed Sharieffudeens, Student, SRM University<br />

8H) Smart Vortex Generators/Dimples Matrix based on MEMS<br />

Pressure Sensors for Modern <strong>Aircraft</strong>s<br />

Deepanshu Srivastav, Student, BITS Pilani K K Birla Goa Campus<br />

SESSION 9: PANEL MODELLING<br />

9A) Strength-Stability Optimisation of Hybrid-Stiffness Laminated<br />

Plates with Cutouts Subjected to Multiple Loads<br />

Tanut Ungwattanapanit, Research Associate, Institute of Lightweight<br />

Structures, Technische Universität München<br />

9B) Parametric Modelling of Fuselage Panels for <strong>Structural</strong> Analysis<br />

and Cost Estimation<br />

Haiqiang Wang, PhD Candidate, Delft University of Technology<br />

THE CONFERENCE AFTER DINNER SPEAKER WILL BE<br />

MARC. L.J.DIERIKX.


PROGRAMME / DAY THREE - 11 OCTOBER 2012<br />

08.00<br />

08.45<br />

09.30<br />

09.55<br />

10.20<br />

10.50<br />

11.15<br />

11.40<br />

12.05<br />

12.30<br />

13.30<br />

REGISTRATION FORM:<br />

Registration and secure payment can be made on-line at www.aerosociety.com/events.<br />

Alternatively, complete one registration form per person (photocopies may be used) and return with payment to:<br />

<strong>Conference</strong> & Events Department, Royal Aeronautical Society, No.4 Hamilton Place, London, W1J 7BQ, UK<br />

TITLE:<br />

POSITION:<br />

ORGANISATION:<br />

ADDRESS:<br />

TEL NO:<br />

EMAIL:<br />

Registration and coffee<br />

Keynote<br />

Luiz E Rimoldi, Technology Development Senior Manager, Embraer<br />

SESSION 10: MANUFACTURING<br />

10A) Geometric Parameterisation of Firtree Joints in Gas<br />

Turbine Discs Considering Manufacturing Variability<br />

Mr Aditya Deshpande, PhD Student, University of Southampton<br />

10B) Innovating the Overbraiding <strong>Design</strong> Process to Optimise<br />

the Development of Composite <strong>Aircraft</strong> <strong>Structural</strong> Components<br />

Dr Erik Baalbergen, Scientist, National Aerospace Laboratory<br />

Networking Break<br />

10C) Automated Production of Large and Complex Single Parts<br />

and Assembly of Helicopter Airframe Structures– Combined<br />

Materials, Cost and Time Saving Approach<br />

Mr Christoph Steindl, Project Manager, Airframe <strong>Design</strong>,<br />

Eurocopter Deutschland GmbH<br />

10D) Industrialisation of a Thermoplastic Horizontal Tail Plane<br />

for a New Helicopter<br />

Mr Marc Koetsier, Senior Manufacturing Engineer New Concept<br />

Development, Fokker Aerostructures B.V.<br />

10E) <strong>Structural</strong> <strong>Design</strong> of the Laminar Products Family for it’s<br />

Comapct Production Technology Planning<br />

Dr Dmitry Svirsky, Senior Scientific Employee, United Institute of<br />

Informatics Problems of NAS, Belarus<br />

10F) On the Effect of Draping Strategy on FE-Based Draping<br />

Simulation of Basic and Complex 3D Geometries for Automated<br />

Preforming<br />

Mr Daniel Liebau, PhD Student, Daimler AG<br />

CLOSE OF CONFERENCE AND LUNCH<br />

TECHNICAL TOUR TO FOKKER WITH RETURN TO DELFT<br />

SIGNATURE:<br />

FIRST NAME: SURNAME:<br />

FAX NO:<br />

RAES MEMBERSHIP NO:<br />

REGISTRATION FEES: (include refreshments, lunch, conference dinner, technical tour &<br />

proceedings)<br />

Fee £ VAT 20% £ Total £<br />

Non-Member 630.00 126.00 756.00<br />

RAeS Corporate Partner * (inc. Armed Forces) 510.00 102.00 612.00<br />

RAeS/ CEAS / AIAA Members 430.00 86.00 516.00<br />

Speaker / Chairman 430.00 86.00 516.00<br />

RAeS Baseline Member 250.00 50.00 300.00<br />

<strong>Conference</strong> Dinner (No Charge) - (Additional guest tickets available from RAeS C&E Department)<br />

Attendance for Technical Tour (No Charge) - Thursday 11 October<br />

RAeS Student Affiliate Members may attend free of charge subject to availability.<br />

* RAeS Corporate Partners are entitled to the special offer of five places for £ 2,000 + VAT<br />

SESSION 11: STRUCTURAL DESIGN<br />

11A) Panoramic Passenger Windows Applied to Transport<br />

<strong>Aircraft</strong><br />

Dr Doris Empl, Research Associate, Bauhaus Luftfahrt e. V.<br />

11B) Refine, Redefine, or Radical Rethink? What are the Real<br />

Challenges of the 21st Century?<br />

Dr Donough Wilson, Research partner, VIVID/futureVision<br />

Networking Break<br />

11C) The Overall <strong>Structural</strong> <strong>Design</strong> of Jet Engine Based on<br />

Master Model<br />

Zhang Rui, School of Jet Propulsion, Beihang Univeristy<br />

11D) Mechanism Analyses: Finding the Missing Link in<br />

<strong>Structural</strong> <strong>Design</strong><br />

Dr Alan Prior, Director SIMULIA North-Nordics CSE, Dassault<br />

Systemes<br />

11E) Supersonic Transport: Challenges and Solutions<br />

Quaid Vohra<br />

11F) The Oval Fuselage: A New Centerbody Concept for<br />

Blended-Wing-Body <strong>Aircraft</strong><br />

Dr Roelof Vos, Assistant Professor, Aerospace Engineering, Delft<br />

University of Technology<br />

CREDIT CARDS:<br />

The RAeS can accept payment on the following<br />

payment cards<br />

Visa Mastercard Amex Maestro<br />

Switch Issue Number:<br />

Expiry Date: Month Year<br />

Card Number:<br />

Please include your CVC security code:<br />

These are the last 3 digits on the signature panel<br />

on the back of the card or 4 digits printed on the<br />

front of the Amex card<br />

METHODS OF PAYMENT:<br />

All payments should be made in Sterling (UK£).<br />

Online: Registration and secure payment can be made online<br />

at www.aerosociety.com/events<br />

Cheque: Should be made payable to the RAeS and enclosed<br />

with this registration form. Please add £15 if your cheque<br />

is not drawn on a UK bank to cover bank charges/currency<br />

exchange rates.<br />

Bank Transfer: Payments can be made by bank transfer into<br />

Account No. 01564641, Sort Code 40 05 22, HSBC Bank<br />

plc, Mayfair Branch, 18a Curzon Street, London W1J 7LA,<br />

UK. Please indicate on the registration form if you have paid<br />

your fees direct.<br />

Reference: #684

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