IFASD Scientific Committee Conference

InternatIonal Forum on aeroelastIcIty & structural DynamIcs 201324 – 26 JuNE 2013 / BRISTOL, uK

Sponsored by:

BOOK YOUR PLACE AT WWW.AEROSOCIETY.COM/EVENTS

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pROGRAMME / DAY 1 – MONDAY 24 JUNE

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Registration

Welcome – Opening of IFASD 2013

Keynote 1: Future Research Challenges for the Loads and Aeroelastics Discipline in the Civil Aviation IndustryTom Wilson, Head of Technical Capability for Aircraft Loads, Airbus Operations LtdNetworking & Coffee Break SESSION 1: AEROELASTIC pREDICTION WORKShOp 11A) Lessons Learned from the Aeroelastic prediction WorkshopDr Jennifer Heeg, Research Engineer, NASA Langley Research Center 1B) Analysis of First AIAA Aeroelastic prediction Workshop Results of unforced and Oscillating hIRENASD WingBart 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 ResultsPawel Chwalowski, Senior Aerospace Engineer, NASA 1E) prediction of Aeroe-lastic Response of the hIRENASD Configura-tion based on TRANAIR Dr Gautam SenGupta, Technical Fellow, The Boe-ing Company. Jointly pre-sented 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 12A) Aircraft Aeroelastic Stability and Response during Wake penetrationDr Sudha U.P.V, Scientist, Aeronautical Development Agency 2B) Nonlinear Flutter Analysis for the Scaled F-35 with horizontal Tail Free-playPing-Chih Chen, President, ZONA Technology Inc.

2C) Identification of Aeroelastic parameters of helicopter Tail Rotor StructuresDr 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 ConfigurationsDr Louw van Zyl, Principal Researcher, Council for Scientific and Industrial Research of South Africa

2E) Wing Flutter Bench Investigation using Aerodynamic Force SimulationProf Vsevolod Smyslov, Chief Scientist, TsAGI& P. Karkle, G. Lysejkin & V. Pronin

Networking & Coffee Break SESSION 3: FLAppING WINGS3A) Flapping Wing Aeroelasticity using a Corotational FEM and a 3D panel MethodRiccardo Gori, PhD Student, University Roma Tre

3B) Kinematic and unsteady Aerodynamic Modelling, Numerical Simulation and parametric Study of Flapping Wing OrnithopterProf Dr Harijono Djojodihardjo, Professor of Aerospace Engineering, University Putra Malaysia3C) Simulation of Bird Wing Flapping using the unsteady Vortex Lattice MethodDr Norizham Abdul Razak, Post Doctoral Researcher, University of Liege

3D) A Calculus of Variations Approach for Manoeuvrability-Optimum Wing Kinematics of Flapping MAVs Near hoverProf Muhammad Hajj, Professor, Virginia Tech

3E) Aeroelastic Optimisation of Membrane prestress on a Flapping WingProf Mayuresh Patil, Associate Professor, Virginia Tech

Networking & Coffee Break SESSION 4: OpTIMISATION 14A) Aeroelastic Stochastic Optimisation, the Mass Grid Model CaseRémi Arnaud, PhD Student, ONERA

4B) The Role of Optimisation Tools in a Real-Life Wing Redesign to Avoid FlutterTorsten Bråmå, Technical Fellow, Saab AB

4C) Confident Aircraft Design and Development using Robust Aeroelastic AnalysisDr 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 VibrationsEdoardo Menga, Component Loads & Aerolelasticity R&T – EGLCRG Coordinator, Airbus Operations SL & Abarca-Lopez Ramon4E) Aeroelastic Sensitivities in Wing Structural Optimisation – An Industrial ApproachPaul Kealy, Loads and Aeroelastics Engineer, Airbus Operations Ltd

Networking & Coffee Break SESSION 5: ROTATING SySTEMS / TuRBOMAChINERy 15A) An Adaption of the p-Method to Analyse the Aerodynamic Damping in Tubomachinery Considering Modal CouplingDetlef Korte, Representative Aeroelasticity, MTU Aero Engines GmbH5B) Dynamic Loads on the Aircraft due to Engine Imbalance at Blade OffProf Oleg Kuznetsov, Principal Scientist, TsAGI & Regina Leontieva, Engineer, TsAGI

5C) Dealing with harmonics and Noise for Advanced Dynamic Identification of In-Flight helicopter DataIr Simone Manzato, Test RTD Research Engineer, LMS International

5D) probabilistic Investigations of Mode Localisation and power Flow in a Mistuned, Generic RotorDipl.-Ing Gerrit Sinapius, Research Assistant, DLR 5E) Aerodynamic Loading on Bird-Damaged Fan Blades and its Effect on Aeroelastic ResponseEric Muir, PhD Candidate, The University of Michigan

18.00 – 20.00 – pre-Registration – Bristol Marriott RoyalSuNDAy 23 JuNE 2013

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CLOSE OF DAy ONE – WELCOME DRINKS RECEpTION – SS GREAT BRITAIN

pROGRAMME / DAY 1 – MONDAY 24 JUNE (cont)

12:30

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Networking Lunch

SESSION 6: AEROELASTIC pREDICTION WORKShOp 26A) Reduced Order Modelling of Nonlinear, Transient Aerodynamics of the hIRENASD WingDipl.-Ing Klemens Lindhorst, Research Assistant, TU Braunschweig6B) Investigation of Experimental uncertainty & Computational Variation for the hIRENASD data sets of the Aeroelastic prediction WorkshopProf Melike Nikbay, Associate Professor, Istanbul Technical University6C) Computation of the unsteady Aerodynamics of the Rectangular Supercritical Wing for the Aeroelastic prediction WorkshopDr David Schuster, NASA Technical Fellow for Aerosciences, NASA Engineering and Safety Center6D) The Validation of Aeroelastic Simulations using STAR-CCM+ Coupled to AbaqusAlan Mueller, CD-Adapco Refreshments and poster Sessions SESSION 11: AEROELASTIC pREDICTION WORKShOp 311A) Comparison of Aeroelastic Solutions on the hIRENASD ModelAnne-Sophie Sens, Research Scientist, ONERA

11B) Numerical prediction and post-Test Numerical Analysis of the ASDMAD Wind Tunnel Tests in ETWProf 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 ConditionsDr.-Ing. Athanasios Dafnis, Aachen University, Chair and Institute of Aerospace and Lightweight Structures

Networking Lunch

SESSION 7: ExpERIMENTAL METhODS 17A) An Actively Controlled Air Support System for Ground Vibration TestingDr 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 TestingProf Tim De Troyer, Lecturer, Vrije Universiteit Brussel

7C) A New and Time Efficient procedure for the Identification of Modal parameters on AircraftsDr.-Ing Yves Govers, Team Leader Modal Testing and Model Validation, German Aerospace Center (DLR)

7D) Design and Construction of Aeroelastic Wind Tunnel ModelsProf 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 ShapeDr Ranjan Vepa, Lecturer, Queen Mary, University of London

12B) Chiral-Rib Structures For Morphing WingsDr 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 DevicesShijun Guo, Reader Aeroelasticity and Composite Structures, Cranfield University

Networking Lunch

SESSION 8: CONTROL8A) Control of Resonating FWMAV Structures using Repeated EigenvaluesHugo Peters, PhD Researcher, Delft University of Technology

8B) Nonlinear Control of a Flexible Aeroelastic SystemDr Shakir Jiffri, Research Associate, University of Liverpool

8C) Design of a Winglet Control Device for Active Load AlleviationDr Andreas Wildschek, Research Engineer, EADS Innovation Works & Martin Herring, Research Engineer, EADS Innovation Works

8D) Active Control for Flutter Suppression: An Experimental InvestigationProf John Mottershead, Alexander Elder Professor of Applied Mechanics, University of LiverpoolRefreshments and poster Sessions SESSION 13: uNCERTAINTy 113A) uncertainties in Control Surface Free-play and Structural properties and their Effect on Flutter and LCODr Dale Pitt, Boeing Technical Fellow, The Boeing Company13B) uncertainty Quantification for Aeroelastic Analyses of Semi-Span Supersonic Transport (S4T) Wing via Model Reduction TechniquesPinar Acar, Research Assistant, Istanbul Technical University13C) uncertainty Management Application to Target Design Load Setting, An Airbus Industrial use Case ExampleSimon Coggon, Ground Loads Modelling Expert, Airbus

Networking Lunch

SESSION 9:LOADS 19A) Ground Dynamic Loads Calculations Strategies for Civilian and Military AircraftsVincent Jacques, Structural Dynamics Engineer, Dassault Aviation

9B) A Method for Application of Frequency Domain-based Load Sources to Full-scale Aircraft Fatigue TestsDr Chance McColl, Director of Engineering – Marietta, Technical Data Analysis, Inc. (TDA)9C) Robust performance Analysis Applied to Loads Computation of a Flexible AircraftDipl.-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 AnalysisDr Yves Lemmens, Senior Research Engineer, LMS International

Refreshments and poster Sessions SESSION 14: CERTIFICATION 114A) Aeroelastic Certification of Light Sport Aircraft According “LTF” RegulationDr Jiri Cecrdle, Senior Scientist, Aeronautical Research and Test Institute (VZLU)

14B) Transonic Flutter Wind Tunnel Tests of high Aspect Ratio WingDr 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 InnovationPing-Chih Chen, President, ZONA Technology, Inc. & Dr Ned Lindsley, Research Engineer, Air Force Research Laboratory (AFRL/VASD)

Networking Lunch

SESSION 10:STRuCTuRAL DyNAMICS10A) Analytical Model of Structural Damping properties at Riveted Lap JointShigeru Machida, Senior Researcher, Japan Aerospace Exploration Agency

10B) Development of a Structural Model of the CRM Configuration for Aeroelastic and Loads AnalysisThomas Klimmek, Research Scientist, German Aerospace Centre (DLR), Institute of Aeroelasticity10C) Structural Dynamic Response of a Wing Box Aeroelastic ModelDr Emanuela Bocchio, Aeroelasticity Specialist, Alenia Aermacchi

10D) Modal Analysis in a Three Dimensional Continuous-Time State-Space unsteady Aerodynamic ModelNoud Werter, PhD Candidate, Delft University of TechnologyRefreshments and poster Sessions SESSION 15: LOADS 215A) high Fidelity Simulation of Novel Loads Control DevicesDr John Pattinson, Research Engineer, EADS Innovation Works & Martin Herring, Research Engineer, EADS Innovation Works15B) Validation Environment for Structural Loads Monitoring AlgorithmDipl.-Ing Thorben Herfeld, Development Engineer, DMecS Development of Mechatronic Systems GmbH & Co. KG

15C) Load Analysis Method of Very Flexible Wing/propeller SystemXie Changchuan, Master Graduate Student, Beihang University & Zhang Lijuan, Master Graduate Student, Beihang University

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pROGRAMME / DAY 2 – TUESDAY 25 JUNE

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Registration

Keynote 2: Dewey Hodges, Professor of Aerospace Engineering, Georgia Institute of Technology

Networking & Coffee Break

SESSION 16: hIGhLy FLExIBLE AIRCRAFT16A) Critical Flight Loads on the Geometrically Nonlinear Dynamics of Very Flexible AircraftDr Joseba Murua, Lecturer in Aerospace Engineering, University of Surrey16B) Reduced-Order Aeroelastic Models for the Dynamics of Manoeuvring Flexible AircraftHenrik Hesse, PhD Research Student, Imperial College London

16C) In-Flight Aeroelastic System Identification of high-Aspect-Ration Motor GliderAlexander Köthe, Research Co-worker, Berlin Institute of Technology

16D) Condensation of Large Finite-element Models for Wing Load Analysis with Geometrically-nonlinear EffectsDr Rafael Palacios, Senior Lecturer, Imperial College London16E) preliminary Flight Test Correlations of the x-hALE Aeroelastic ExperimentProf Carlos Cesnik, Professor of Aerospace Engineering, University of Michigan Networking Lunch

SESSION 20: OpTIMISATION 220A) Design and Aeroelastic Assessment of a Forward Swept Wing AircraftDr Wolf Krueger, Head of Division Loads Analysis and Design, German Aerospace Center (DLR), Institute of Aeroelasticity20B) On the use of Tow-Steered Composites for Aeroelastic TailoringOlivia Stodieck, PhD Researcher in Aerospace Engineering, University of Bristol20C) The Needs to Incorporate Aeroelastic Aspects into the Conceptual Design processDipl.-Ing Johannes Schweiger, Conceptual Design Analysis, Cassidian

20D) Multidisciplinary Optimisation of Flexible Aircraft in Flight with Superimposed Static and Dynamic Aeroelastic LoadsOgmundur Petersson, Specialist, Cassidian Air Systems

Networking & Tea Break

Networking & Coffee Break

SESSION 18:LOADS 318A) New Method for horizontal Tail plane Buffeting Loads predictionRaul 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 ExcitationHadrien Mamelle, Structural Dynamics Engineer, Dassault Aviation18C) use of Linearized CFD for unsteady Aerodynamics for Gust LoadsGuillermo Jenaro, HO Dynamic Loads, Airbus Operations GmbH & Jörg Hasselbring , Dynamic Loads Engineer, Airbus Operations GmbH18D) Continuous Turbulence Design Loads Calculation in presence of Non-linear ControlsProf Sergio Ricci, Associate Professor, University of Milan

18E) Identification of unsteady Aerodynamic Loads using Aeroelastic Response and Kalman FilterProf Luiz Góes, Professor, ITA - Aeronautical Institute of Technology & Roberto Gil A da Silva, Professor, ITA – Aeronautical Institute of Technology Networking Lunch

SESSION 22: FLuTTER22A) A Consistent Strip Theory for T-tail Flutter ComputationsProf Pablo Garcia-Fogeda, Professor of Aeroelasticity, EIAE-UPM

22B) T-Tail Flutter: potential-flow Modelling and Experimental ValidationDr Joseba Murua, Lecturer in Aerospace Engineering, University of Surrey22C) Experimental and Computational Investigation of a Full Aircraft Flutter at Transonic SpeedsProf Qian Wei, Senior Engineer, Shenyang Aircraft Design & Research Institute

Networking & Tea Break

Networking & Coffee Break

SESSION 17: COMpuTATIONAL AEROELASTICITy 117A) Forced Motion Simulations using a Linear Frequency Domain Solver For a Generic Transport AircraftReik Thormann, Scientist, DLR, Institute of Aeroelasticity

17B) Forced Response Calculation using TWIN ApproachDr Majid Mesbah, Researcher, Cenaero

17C) A Reduced-Order Model for Aeroelastic Studies on Circulation Controlled WingsDipl.-Ing Ian Krukow, Research Assistant, TU Braunschweig

17D) Roll Damping Derivative from Wind Tunnel Forced-Oscillation Tests and Generalised Lifting – Surface Aerodynamic TheoryAnthony Pototzy, Aeroelasticity Branch, NASA Langley Research Center17E) Efficient Identification of Aerodynamic and Aeroelastic Models using Coupled CSD-CFD SimulationsTaehyoun Kim, Associate Professor, National University of Singapore Networking Lunch

SESSION 21: COMpuTATIONAL AEROELASTICITy 221A) Role of Mach Number Freeze in Transonic FlutterProf Oddvar Bendiksen, Professor, University of California 21B) Influence of Transitional Flows at Transonic Mach Numbers on the Flutter Speed of a Laminar AirfoilMichael Fehrs, Research Assistant, (DLR) – Institute of Aeroelasticity 21C) Time Integration Schemes’ Influence on partitioned Method for the Fluid–Structure Coupling procedureGuillaume Bénéfice, PhD Student, Ecole Centrale Lyon

21D) Extension of the Non-Linear harmonic Method to Flow Computation Around Moving and Deforming StructuresFrancois Debrabandere, Development Engineer, Numeca International

Networking & Tea Break

Networking & Coffee Break

SESSION 19:NONLINEARITy 119A) Analysis for a Three-dimensional Structurally Nonlinear Wing with a Control SurfaceProf SangJoon Shin, Associate Professor, Seoul National University19B) Nonlinear Analysis of the Influence of Aircraft Dynamics on Nose Landing Gear ShimmyNandor Terkovics, PhD Student, University of Bristol

19C) Nonlinear Aeroelastic Response of a flat panel. A Normal Form ApproachMarco Eugeni, PhD Student, University of Rome “La Sapienza”

19D) Nonlinear Dynamic Analysis of an F-16 Aircraft using GVT DataSimone Manzato, RTD Test Research Engineer, LMS International

19E) Application of Nonlinear Geometrical Effects to the Analysis of Structural Loads using Fast Evaluation MethodsDr.-Ing Moriz Dirk Scharpenberg, Flight Physics Engineer, Airbus

Networking Lunch

SESSION 23: NONLINEARITy 223A) Instability of Aeroelastic Systems with Softening NonlinearityXiaojun Wei, PhD Student, University of Liverpool 23B) Limit-Cycle Oscillations of Supercritical AirfoilsAnna Van Rooij, PhD Candidate, German Aerospace Center (DLR) 23C) Identification of Structural Non-linear Stiffness and Damping parameters using the Restoring Force Surface MethodDr Marc Boeswald, Head of Department of Structural Dynamics, German Aerospace Center (DLR)23D) Limit-Cycle-Oscillation Simulations of Aerostability Windtunnel ExperimentsBernd Stickan, Development Engineer, Airbus

Networking & Tea Break

Dinner sponsored by:

pROGRAMME / DAY 2 – TUESDAY 25 JUNE (cont)

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SESSION 24: GuSTS 124A) Gust Loads Alleviation Based on Model predictive ControlHans-Gerd Giesseler, Expert, Airbus Operations GmbH

24B) high Fidelity Numerical Simulations for Gust Response AnalysisDr Fabien Huvelin, Research Engineer, ONERA

24C) DLM-Correction Methods for Aerodynamic Gust Response predictionDiliana Dimitrov, Research Assistant, Institute of Aeroelasticity, German Aerospace Center (DLR)24D) Reduced Order Modelling for the Gust Response of the FFAST WingDr Christopher Wales, Research Associate, University of Bristol

SESSION 26: ROTATING SySTEMS / TuRBOMAChINERy 226A) On the use of Radial Basis Functions to Numerically predict Flutter in TurbomachineryYannick Rozenberg, Associate Professor, University Lyon 1 – LMFA

26B) Structural Dynamic Analysis of a Vertical Axis Wind Turbine with Troposkien GeometryAmin Fereidooni, M.A.Sc Student, Carleton University26C) Nodal Energy Weighted Transformation: A New Mistuning projection for FladeTM SystemsColin Fitzner, Graduate Student Research Assistant, University of Michigan26D) Numerical Investigation of a Contrafan Aeroelastic Response with Multichorochronic Boundary ConditionsDr Antoine Placzek, Research Engineer, ONERA

SESSION 25: COMpuTATIONAL AEROELASTICITy 325A) Evaluation of Linear, Inviscid, and Viscous Aeroelastic Solutions of the AGARD 445.6 Wing using Reduced–Order Modeling and Root Locus SolutionsDr Walter Silva, Senior Research Scientist, NASA Langley Research Center25B) Dynamic Stability and Response Analyses using a Small-Disturbance CFD MethodCyrille Vidy, Development Engineer, Cassidian (EADS Germany)25C) Small Disturbance Navier-Stokes Investigations of Fighter-Type-Delta-Wing pitching OscillationsDipl.-Ing Alexander Pechloff, Research Engineer, TU Munich 25D) A 3-D Zero-Lift Drag prediction including Aeroelastic EffectsDr Raymond Kolonay, Aerospace Engineer, United States Air Force Research Lab

SESSION 27: CERTIFICATION 227A) Development of a New Tool for Static Aeroelastic Analysis Applied on the SAAB Gripen Fighter AircraftHans Soderberg, Senior Engineer, SAAB Aeronautics

27B) Flight Test Validation of Wake Vortex Encounter LoadsDr Héctor Climent, Head of Structural Dynamics and Aeroelasticity, Airbus Military

27C) Flutter Wind Tunnel Tests for a Regional AircraftHiroyuki Morino, Manager, Mitsubishi Aircraft Corporation & Satoshi Yonemoto, Mitsubishi Heavy Industries, Ltd

27D) Store Ejection Simulations on a Rafale AircraftGuillaume Reinhardt, Engineer, Dassault Aviation

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Non-Member 600.00 120.00 720.00

RAeS Corporate Partner (inc. Armed Forces)* 550.00 110.00 660.00

CEAS / AIAA Member Rate 550.00 110.00 660.00 RAeS Member 500.00 100.00 600.00 Speaker & Chairmen 500.00 100.00 600.00 Welcome Reception Ticket (Monday 24 June – Included in price of conference) Conference Dinner Ticket (Tuesday 25 June – Included in price of conference) Guest Conference Dinner Ticket 50.00 10.00 60.00 Technical Tour Attendance (Thursday 27 June)

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CONFERENCE DINNER – @BRISTOL SCIENCE CENTRE

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SyNOpSIS

The International Forum 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 Forum 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 Forum 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.

Dr Wolf Kruger – Head of Loads Analysis and Aeroelastic Design, DLR Institute of Aeroelasticity.

TEChNICAL VISITS – 27 JuNE 2013Technical visits will be held to Airbus and other local aerospace industries.

SOCIALSocial events will include a reception on Brunel’s SS Great Britain and a dinner to be held at the @Bristol Science Centre.

WhO ShOuLD ATTENDIFASD2013 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.

VENuEBristol Marriott Royal Hotel, Bristol, BS1 5TA, UK

CONTACT uSConference & EventsRoyal Aeronautical SocietyNo.4 Hamilton PlaceLondon, W1J 7BQ, UK+44 (0)20 7670 4345

conference@aerosociety.com www.aerosociety.com/events

proceedingsProceedings 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.

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pROGRAMME / DAY 3 – WEDNESDAY 26 JUNE

07:45

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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 328A) An Aeroelastic Multi Fidelity Approach for Aeroelastic TailoringDr Roeland De Breuker, Assistant Professor, Delft University of Technology

28B) preliminary Design and Optimisation for Flexible Aircraft in a Distributed EnvironmentPier Davide Ciampa, German Aerospace Center (DLR)28C) parametric Studies for Wing Mounted FinsPing-Chih Chen, President, ZONA Technology, Inc.

28D) Automated Creation of Aeroelastic Optimisation Models from a parameterised GeometryReinhold Maierl, PhD Student, CASSIDIAN Air Systems 28E) Multi-Disciplinary Wing Optimisation using a Discipline-Specific Trust-Region MethodDr Simão Marques, Lecturer in Aerospace Engineering, Queen’s University Belfast Networking Lunch

Networking & Coffee Break

SESSION 30: LOADS 430A) Fast prediction of Worst Case Gusts LoadsHamed Haddad Khodaparast, Lecturer, College of Engineering, Swansea University

30B) Wake Vortex Encounter Loads Numerical SimulationSebastián Claverías-Ceacero, Structural Dynamics and Aeroelasticity Engineer, Airbus Military30C) An Integrated Loads Analysis Model for Wake Vortex EncountersDipl.-Ing Thiemo Kier, Research Engineer, German Aerospace Center (DLR) 30D) Efficient, Laplace-Domain Aerodynamics for Load AnalysesNatascha 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 OptimisationDr Luis Teia Gomes, Installation Aerodynamics Development Engineer, Rolls-Royce Deutschland Ltd & Co KG

Networking Lunch

Networking & Coffee Break

SESSION 29: COMpuTATIONAL AEROELASTICITy 429A) Grid Deformation for Computational Aeroelastic Analysis using RBF Interpolation with Standard Greedy MethodHaris Hameed Mian, Postgraduate Student, Northwestern Polytechnical University29B) A partitioned Method for the Direct Aeroelastic Simulation of Free-Flying AircraftGeorg Wellmer, Loads Engineer, Cassidian29C) Structural Response prediction of Surface panels in hypersonic FlowProf Jack McNamara, Associate Professor, The Ohio State University 29D) Time Domain Aeroelastic Solution using Exact Aerodynamic Influence Coefficients and Nonlinear DampingDr Vin Sharma, Flutter Engineer, Air Force SEEK EAGLE Office29E) Investigation of Interaction of Shock Movement with Structural Elastic Deformations in Transonic FlowDr 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, TsAGINetworking Lunch

Networking & Coffee Break

SESSION 31: NONLINEARITy 331A) Combined Frequency and Time Domain Solutions for Aeroservoelastic Response with NonlinearitiesProf Moti Karpel, Professor, Technion – Israel Institute of Technology

31B) Nonlinear Reduced Order Models of unsteady Aerodynamics for Non-classical Aileron Buzz AnalysisFrancesca Fusi, PhD Candidate, University of Milan31C) Investigations of Transonic Aircraft in the Joint DLR / ONERA project Non-Linear Aeroelastic Simulation, NLAS IIProf 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 Lab31D) Aeroelastic Design Exploiting Structural Geometric NonlinearitiesProf Jonathan Cooper, Airbus Sir George White Chair of Aerospace Engineering, University of Bristol 31E) Geometrically Non-linear Structural Modal Analysis for Local and Impulsive ExcitationLars Oliver Bernhammer, PhD Student, Delft University of Technology Networking Lunch

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FOR MORE INFORMATION AND TO REGISTER www.ifasd2013.com

pROGRAMME / DAY 3 – WEDNESDAY 26 JUNE (cont)

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SESSION 32: ExpERIMENTAL METhODS 232A) Flutter Wind Tunnel Test at high Transonic Mach of a Flexible Empennage with Variable Control Surface Free–play and StiffnessPaul Taylor, Principal Engineer, Gulfstream Aerospace Corporation

32B) A400M Flight Vibration Survey for Equipment Environmental QualificationMarc Montagne, Vibration Team Leader, Airbus Military

32C) Experimental Investigation of the Aeroelastic Behaviour of a Laminar Wing in Transonic FlowAnne 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-MonitoringDipl. Ing Alireza Rezaeian, Aerospace Engineer, Research Associate, German Aerospace Centre (DLR), Institute of Aeroelasticity

Networking & Tea Break

SESSION 36: GuSTS 236A) Linear Reduced Order Modelling for Gust Response Analysis using the DLR-TAu CodeDr Sebastian Timme, Lecturer, University of Liverpool

36B) Comparison of Different Approaches for Gust Modelling in the CFD Code TAuDr Ralf Heinrich, Team Leader of Group “Multidisciplinary Modeling”, German Aerospace Center (DLR)36C) high-Fidelity Simulation of Aeroelastic Wind Gust Effect in Aerodynamic ShapesDr Ruben Sevilla, Lecturer, Swansea University

SESSION 34: AEROELASTIC ANALySIS 234A) Modelling and Analysis of the Flight Dynamics of a Deformable Aircraft with Structurally-Linearized Full Inertial CouplingAntônio Bernardo Guimarães Neto, Master’s Student, Technological Institute of Aeronautics (ITA)34B) Modelling of Damage in Laminated Composite plates and Nonlinear Flutter AnalysisDr Ranjan Vepa, Lecturer, Queen Mary, University of London

34C) Stability Enhancement of a Transonic Wing using a Simple passive AttachmentD. Michael McFarland, Research Associate Professor, University of Illinois at Urbana-Champaign

34D) Spectral Finite Element Modelling and updating in Aeroelastic Analysis of Light Sport AircraftJoseph Gross, Research Associate, Hamburg University of Technology Networking & Tea Break

SESSION 38: uNCERTAINTy 238A) uncertainty Quantification in Aeroelastic Composite Structures using Lamination parametersProf Carl Scarth, PhD student, ACCIS Centre, University of Bristol

38B) Application of uncertainty Management to Improve Reliability of hard Landing Criticality Assessment CriteriaThomas Wilson, Head of Ground Loads, Airbus UK 38C) uncertainties in Measurements and Data Evaluation Concerning Transonic high Reynolds Number Wind Tunnel TestsDr Alexander Boucke, Scientist, ITAM GmbH

SESSION 33: COMpuTATIONAL AEROELASTICITy 533A) Sensitivity Evaluation in Transonic Fluid-Structure InteractionsProf Marilyn Smith, Associate Professor, Georgia Institute of Technology

33B) Computational Aeroelastic Analysis of the Semi-Span Super-Sonic Transport (S4T) Wind-Tunnel ModelMark Sanetrik, Research Engineer, NASA Langley Research Center33C) A Novel Computational Approach to unsteady Aerodynamic and Aeroelastic Flow SimulationEliot Quon, Graduate Research Assistant, Georgia Institute of Technology33D) Aerodynamic Optimisation of a Flexible high-Lift WingGiuseppe Trapani, EngD Researcher, Cranfield University

Networking & Tea Break

SESSION 37: COMpuTATIONAL AEROELASTICITy 637A) The NASA high Speed ASE project: Computational Analyses of a Low-Boom Supersonic ConfigurationDr Walter Silva, Senior Research Scientist, NASA Langley Research Center37B) A Time-Spectral Aeroelastic Method for Transonic Flutter predictionDr Gaetan Kenway, Post Doctoral Researcher, University of Michigan 37C) using proper Orthogonal Decomposition and Dynamic Mode Decomposition Methods for Comparing CFD Results Experimental MeasurementsAmandine Guissart, PhD Student, University of Liège

SESSION 35: ROTATING SySTEMS / TuRBOMAChINERy 335A) Counter-Rotating Open Rotor Whirl Flutter phenomenon. Investigations using elsA solverDr Simon Verley, Research Scientist, ONERA

35B) propeller – Flexible Wing Interaction using Rapid Computational MethodsChenhui Liu, Flight Physics Engineering Intern, Airbus

35C) Aeroelastic Design Study of Subsonic high pressure Turbine Blades for Space ApplicationsDr Pieter Groth, Senior Aerodynamic Design Engineer, GKN Aerospace Sweden35D) Numerical Investigation of an L-Shaped Deployable Gurney Tab for Rotorcraft Vibration ControlValentina Motta, PhD Candidate, University of Milan Networking & Tea Break

SESSION 39: SMART STRuCTuRES39A) Aeroelastic Simulations of the SADE FNG Smart Leading Edge – Smart Single Slotted Flap high-Lift ConfigurationDr Mats Dalenbring, Senior Researcher, Swedish Defence Research Agency (FOI)

39B) Adaptive Camber and Chord Morphing Wing with 0-ʋ honeycomb Compared to Conventional WingAshley Dale, PhD Research Student, University of Bristol 39C) Loads, Vibration and Manoeuvre Control using Active Floating FlapsMark Pustilnik, Master Student – the Aerospace Faculty, Technion

Main Lecture Theatre parallel 1 parallel 2 parallel 3

Technical Tours to Airbus and other local aerospace industries

ThuRSDAy 27 JuNE 2013

CLOSING CEREMONy AND IFASD2015 ANNOuCEMENT