IFASD 2013

PROGRAMME

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13/06/2013 19:21:15

SUNDAY 23 JUNE 2013

18.00 – 20.00 – Pre-Registration – Bristol Marriott Royal Hotel

PROGRAMME / DAY 1 – MONDAY 24 JUNE

Kings Room - 1st Floor

08:00

Registration

08:30

Welcome – Opening of IFASD 2013

08:45

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

09:30

Networking & Coffee Break SESSION 1: AEROELASTIC PREDICTION WORKSHOP 1 1A) Overview and Lessons Learned from the Aeroelastic Prediction Workshop Paul Taylor, Principal Engineer, Gulfstream Aerospace Corporation

10:00

10:30

1B) Analysis of First AIAA Aeroelastic Prediction Workshop Results of Oscillating HIRENASD Wing Bart Eussen, Senior R&D Engineer, NLR

Parallel 1 - 2nd Floor

Parallel 2 - 2nd Floor

Parallel 3 - 3rd Floor

Parallel 4 - 3rd Floor

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

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

Networking & Coffee Break SESSION 4: OPTIMISATION 1 4A) Aeroelastic Stochastic Optimisation, the Mass Grid Model Case Rémi Arnaud, PhD Student, ONERA

Networking & Coffee Break SESSION 5: ROTATING SYSTEMS / TURBOMACHINERY 1 5A) An Adaption of the P-Method to Analyse the Aerodynamic Damping in Turbomachinery Considering Modal Coupling Detlef Korte, Representative Aeroelasticity, MTU Aero Engines GmbH

2B) Nonlinear Flutter Analysis for the Scaled F-35 with Horizontal Tail Free Play Ping-Chih Chen, President, ZONA Technology Inc.

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

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

5B) Dynamic Loads on Aircraft due to Engine Imbalance at Blade Off Prof Oleg Kuznetsov, Principal Scientist, TsAGI & Regina Leontieva, Engineer, TsAGI

11:00

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-StokesMethods Mark Foerster, Research Engineer / Scientific Employee, Institute of Aerodynamics and Fluid Mechanics, TU München

2C) Identification of Aeroelastic Parameters of Helicopter Tail Rotor Structures Dr David Zimcik, Group Leader Aeroacoustics and Structural Dynamics, National Research Council Canada

3C) Simulation of Bird Wing Flapping using the Unsteady Vortex Lattice Method Prof Grigorios Dimitriadis, Associate Professor, University of Liege

4C) Confident Aircraft Design and Development using Robust Aeroelastic Analysis Dr Martin Leijonhufvud, Senior Aeronautical Engineer, Saab Aeronautics

5C) Dealing with Harmonics and Noise for Advanced Dynamic Identification of In-Flight Helicopter Data Ir Simone Manzato, Test RTD Research Engineer, LMS International

11:30

1D) Collaborative HIRENASD Analyses to Eliminate Variations in Computational Results Dr Adam Jirasek, Senior Research Engineer, Swedish Defence Research Agency, FOI

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

3D) A Calculus of Variations Approach for ManoeuvrabilityOptimum Wing Kinematics of Flapping MAVs Near Hover Prof Muhammad Hajj, Professor, Virginia Tech

4D) The Needs to Incorporate Aeroelastic Aspects into the Conceptual Design Process Dipl.-Ing Johannes Schweiger, Conceptual Design Analysis, Cassidian

5D) Probabilistic Investigations of Mode Localisation and Power Flow in a Mistuned, Generic Rotor Dipl.-Ing Gerrit Sinapius, Research Assistant, DLR

12:00

1E) Prediction of Aeroelastic Response of the HIRENASD Configuration based on TRANAIR Dr Gautam SenGupta, Technical Fellow, The Boeing Company

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

3E) Aeroelastic Shape Optimisation of a Flapping Wing Prof Mayuresh Patil, Associate Professor, Virginia Tech

4E) Aeroelastic Sensitivities in Wing Structural Optimisation – An Industrial Approach Paul Kealy, Loads and Aeroelastics Engineer, Airbus Operations Ltd

5E) Aerodynamic Loading on Bird-Damaged Fan Blades and its Effect on Aeroelastic Response Eric Muir, PhD Candidate, The University of Michigan

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PROGRAMME / DAY 1 – MONDAY 24 JUNE (cont)

Kings Room - 1st Floor

Parallel 1 - 2nd Floor

12:30

Networking Lunch

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

Parallel 3 - 3rd Floor

Parallel 4 - 3rd Floor

Networking Lunch

Networking Lunch

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

SESSION 8: CONTROL 8A) Control of Resonating FWMAV Structures using Repeated Eigenvalues Hugo Peters, PhD Researcher, Delft University of Technology

SESSION 9: LOADS 1 9A) Ground Dynamic Loads Calculations Strategies for Civilian and Military Aircrafts Vincent Jacques, Structural Dynamics Engineer, Dassault Aviation

SESSION 10: STRUCTURAL DYNAMICS 10A) Analytical Model of Structural Damping Properties at Riveted Lap Joint Shigeru Machida, Senior Researcher, Japan Aerospace Exploration Agency

14:30

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

7B) New Excitation and Measurement Techniques to Integrate GVT and Flight Flutter Testing Prof Tim De Troyer, Lecturer, Vrije Universiteit Brussel

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

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)

10B) Modelling of Damage in Laminated Composite Plates and Nonlinear Flutter Analysis Dr Ranjan Vepa, Lecturer, Queen Mary, University of London

15:00

6C) The Validation of Aeroelastic Simulations using STAR-CCM+ Coupled to Abaqus Rafael Ritterbusch, Technical Specialist Fluid Structure Interaction, CDAdapco

7C) Generating of Beam Computational Model of High Aspect Ratio Wing on the Basis of Full-Scale Structure Stiffness Tests Yury Nayko, Principal Expert, Central Aerohydrodynamic Institute

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

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 Dynamics and Control

10C) Structural Dynamic Response of a Wing Box Aeroelastic Model Dr Emanuela Bocchio, Aeroelasticity Specialist, Alenia Aermacchi

15:30

6D) Comparison of Aeroelastic Solutions on the HIRENASD Model Anne-Sophie Sens, Research Scientist,

7D) Design and Construction of Aeroelastic Wind Tunnel Models Prof Ulf Ringertz, Professor, Kungliga Tekniska Högskolan

8D) Active Control for Flutter Suppression: An Experimental Investigation Prof Jonathan Cooper, Airbus Sir George White Chair of Aerospace Engineering, University of Bristol

9D) Modelling Of Aerodynamic Loads On Flexible Bodies For Ground Loads Analysis Dr Yves Lemmens, Senior Research Engineer, LMS International

10D) Implementation of Geometrically Exact Beam Element for Nonlinear Dynamics Modelling Jielong Wang, Senior Engineer, Commerical Aircraft Corporation of China Ltd (COMAC)

Networking and Tea Break 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

Networking and Tea Break SESSION 13: UNCERTAINTY 1 13A) Uncertainty Quantification for LCO Using an Harmonic Balance Method Richard Hayes, PhD Research Student, Queen’s University Belfast

Networking and Tea Break

Networking and Tea Break SESSION 15: LOADS 2 15A) High Fidelity Simulation Wing Loads with an Active Winglet Control Surface Dr John Pattinson, Research Engineer, EADS Innovation Works & Martin Herring, Research Engineer, EADS Innovation Works

12B) Chiral-Rib Structures For Morphing Wings Dr Giuseppe Quaranta, Assistant Professor, Dept. of Aerospace Science and Technology, University of Milan

13B) Uncertainty Quantification for Aeroelastic Analyses of Semi-Span Supersonic Transport (S4T) Wing via Model Reduction Techniques Pinar Acar, Research Assistant, Istanbul Technical University

14B) Application of a Modern On-Board Excitation System During the Ground Vibration Testing of a Business Jet Demian Gomes Da Silva, Product Development Engineer, Embraer S.A

15B) Validation Environment for Structural Loads Monitoring Algorithm Dipl.-Ing Thorben Herfeld, Development Engineer, DMecS Development of Mechatronic Systems GmbH & Co. KG

13C) Uncertainty Management Application to Target Design Load Setting, An Airbus Industrial use Case Example Simon Coggon, Ground Loads Modelling Expert, Airbus

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)

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

14:00

ONERA

16:00

16:30

17:00

17:30

Networking and Tea Break SESSION 11: AEROELASTIC PREDICTION WORKSHOP 3 11A) Numerical Prediction and PostTest Numerical Analysis of the ASDMAD Wind Tunnel Tests in ETW Prof Dr.-Ing Josef Ballmann, RET Professor & ITAM Consultant, ITAM GmbH 11B) 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 11C) Aeroelastic Calculation of Innovative NonConventional Aircraft with Swinging Canard Surface Wojciech Chajec, Lecturer, Institute of Aviation

Parallel 2 - 2nd Floor

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)

18:15

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CLOSE OF DAY ONE – WELCOME DRINKS RECEPTION – SS GREAT BRITAIN

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PROGRAMME / DAY 2 – TUESDAY 25 JUNE

07:45 08:15

09:00

09:30

10:00

10:30

11:00

11:30

Kings Room - 1st Floor

Parallel 1 - 2nd Floor

Parallel 2 - 2nd Floor

Parallel 3 - 3rd Floor

Keynote 2: A Unified Approach for Reduced-Order Modeling of Lifting Surfaces Dewey Hodges, Professor of Aerospace Engineering, Georgia Institute of Technology Networking & Coffee Break

Networking & Coffee Break

Networking & Coffee Break

Networking & Coffee Break

SESSION 16: HIGHLY FLEXIBLE AIRCRAFT 16A) Preliminary Flight Test Correlations of the X-HALE Aeroelastic Experiment Prof Carlos Cesnik, Professor of Aerospace Engineering, University of Michigan

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

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

SESSION 19: NONLINEARITY 1 19A) Aeroelastiic Analysis for a Three-Dimensional Structurally Nonlinear Wing with a Control Surface Prof SangJoon Shin, Associate Professor, Seoul National University

16B) Reduced-Order Aeroelastic Models for the Dynamics of Manoeuvring Flexible Aircraft Henrik Hesse, PhD Research Student, Imperial College London

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

18B) A New Methodology for the Estimation of Structural Load Level due to Complex Unsteady Aerodynamic Excitation Hadrien Mamelle, Structural Dynamics Engineer, Dassault Aviation

19B) Nonlinear Analysis of the Influence of Aircraft Dynamics on Nose Landing Gear Shimmy Nandor Terkovics, PhD Student, University of Bristol

16C) In-Flight Aeroelastic System Identification of HighAspect-Ration Motor Glider Alexander Köthe, Research Coworker, Berlin Institute of Technology

17C) A Reduced-Order Model for Aeroelastic Studies on Airfoils with Active High-Lift Devices Dipl.-Ing Ian Krukow, Research Assistant, TU Braunschweig

18C) Use of Linearized CFD for Unsteady Aerodynamics for Gust Loads Jörg Hasselbring , Dynamic Loads Engineer, Airbus Operations GmbH

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

16D) Condensation of Large Finite-element Models for Wing Load Analysis with Geometrically-nonlinear Effects

17D) A Study on The Effect of Weapon Installation to Aeroelastic Characteristic of Fighter Aircraft Wing Rianto Adhy Sasongko, Lecturer and Researcher, Institut Teknologi Bandung, Indonesia

18D) Continuous Turbulence Design Loads Calculation in Presence of Non-linear Controls Prof Sergio Ricci, Associate Professor, University of Milan

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

17E) Efficient Identification of Aerodynamic and Aeroelastic Models Using Coupled CSDCFD Simulations Taehyoun Kim, Associate Professor, National University of Singapore

18E) Aeroelastic Response of a 2D Wing with Aerodynamic and Structural Nonlinearity Dr Norizham Abdul Razak, Post Doctoral Researcher, University of Liege

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

Networking Lunch

Networking Lunch

Networking Lunch

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

SESSION 21: COMPUTATIONAL AEROELASTICITY 2 21A) Role of Mach Number Freeze in Transonic Flutter Prof Oddvar Bendiksen, Professor, University of California

SESSION 22: FLUTTER 22A) T-Tail Flutter: Potential-flow Modelling and Experimental Validation Dr Joseba Murua, Lecturer in Aerospace Engineering, University of Surrey

SESSION 23: NONLINEARITY 2 23A) Instability of Aeroelastic Systems with Softening Nonlinearity Xiaojun Wei, PhD Student, University of Liverpool

22B) Experimental and Computational Investigation of a Full Aircraft Flutter at Transonic Speeds Prof Qian Wei, Senior Engineer, Shenyang Aircraft Design & Research Institute

23B) Limit-Cycle Oscillations of Supercritical Airfoils Anna Van Rooij, PhD Candidate, German Aerospace Center (DLR)

22C) Flutter Margin Prediction by Combination of Random Decrement Method and Eigensystem Realisation Algorithm

23C) Limit-Cycle-Oscillation Simulations of Aerostability Windtunnel Experiments Bernd Stickan, Development Engineer, Airbus

Registration

Dr Rafael Palacios, Senior Lecturer, Imperial College London & Yinan Wang, Research Assistant, Imperial College London 16E) A Precise Manufacturing Method of the Cpomposite Structure-Similar Dr Rui Yang, Dalian University of Technology

12:00 13:30

14:00

14:30

20B) On the Use of TowSteered Composites for Aeroelastic Tailoring Olivia Stodieck, PhD Researcher in Aerospace Engineering, University of Bristol 20C) 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 & Ramon AbarcaLopez

15:00

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

15:30

Networking & Tea Break

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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 NonLinear Harmonic Method to Flow Computation Around Moving and Deforming Structures Francois Debrabandere, Development Engineer, Numeca International Networking & Tea Break

Masato Tamayama, Associate Senior Researcher, Japan Aerospace Exploration Agency

Networking & Tea Break

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PROGRAMME / DAY 2 – TUESDAY 25 JUNE (cont)

16:00

16:30

17:00

17:30

Kings Room - 1st Floor

Parallel 1 - 2nd Floor

Parallel 2 - 2nd Floor

Parallel 3 - 3rd Floor

SESSION 24: GUSTS 1 24A) Gust Load Alleviation Based on Model Predictive Control Hans-Gerd Giesseler, Expert, Airbus Operations GmbH

SESSION 25: COMPUTATIONAL AEROELASTICITY 3 25A) An Unsteady Hybrid ROM Approach for Efficient NonLinear Aeroelastic Modelling Dr Arnaud Malan, Associate Professor, University of Cape Town

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

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

24B) High Fidelity Numerical Simulations for Gust Response Analysis Dr Fabien Huvelin, Research Engineer, ONERA

25B) Dynamic Stability and Response Analyses Using a Small-Disturbance CFD Method Cyrille Vidy, Development Engineer, Cassidian (EADS Germany)

26B) Structural Dynamic Analysis of a Troposkien Shape Vertical Axis Wind Turbine Using Mixed Finite Element Formulation Amin Fereidooni, M.A.Sc Student, Carleton University

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

24C) DLM-Correction Methods for Aerodynamic Gust Response Prediction Diliana Dimitrov, Research Assistant, Institute of Aeroelasticity, German Aerospace Center (DLR)

25C) Small Disturbance Navier-Stokes Investigations of Fighter-Type-Delta-Wing Pitching Oscillations Dipl.-Ing Alexander Pechloff, Research Engineer, TU Munich

26C) Nodal Energy Weighted Transformation: A New Mistuning Projection for FladeTM Systems Colin Fitzner, Graduate Student Research Assistant, University of Michigan

27C) Flutter Wind Tunnel Tests for a Regional Aircraft Satoshi Yonemoto, Mitsubishi Heavy Industries, Ltd

26D) Numerical Investigation of a Contrafan Aeroelastic Response with Multichorochronic Boundary Conditions Dr Antoine Placzek, Research Engineer, ONERA

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

24D) Reduced Order Modelling for the Gust Response of the FFAST Wing Dr Christopher Wales, Research Associate, University of Bristol

25D) A 3-D Zero-Lift Drag Prediction including Aeroelastic Effects Dr Darrel Roberton, Senior Research Engineer, University of Dayton Research Institute

18:30

CONFERENCE DINNER – AT-BRISTOL SCIENCE CENTRE

Dinner sponsored by:

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PROGRAMME / DAY 3 – WEDNESDAY 26 JUNE

Kings Room - 1st Floor

Parallel 1 - 2nd Floor

Parallel 2 - 2nd Floor

Parallel 3 - 3rd Floor

07:45

Registration

08:15

Keynote 3: Aeroelastic Design and Optimisation of Green Aircraft Dr Wolf Krueger, Head of Division Loads Analysis and Design, German Aerospace Center – DLR Networking & Coffee Break

Networking & Coffee Break

Networking & Coffee Break

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

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

SESSION 30: LOADS 4 30A) Fast Prediction of Worst Case Gusts Loads Hamed Haddad Khodaparast, Lecturer, College of Engineering, Swansea University

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

10:00

28B) Parametric Studies for Wing Mounted Fins Ping-Chih Chen, President, ZONA Technology, Inc.

29B) A Partitioned Method for the Direct Aeroelastic Simulation of Free-Flying Aircraft Georg Wellmer, Loads Engineer, Cassidian

30B) Wake Vortex Encounter Loads Numerical Simulation Sebastián Claverías-Ceacero, Structural Dynamics and Aeroelasticity Engineer, Airbus Military

31B) Nonlinear Reduced Order Models of Unsteady Aerodynamics for Non-classical Aileron Buzz Analysis Francesca Fusi, PhD Candidate, University of Milan

10:30

28C) Automated Creation of Aeroelastic Optimisation Models from a Parameterised Geometry Reinhold Maierl, PhD Student, CASSIDIAN Military Air Systems Centre

29C) Structural Response Prediction of Surface Panels in Hypersonic Flow Prof Jack McNamara, Associate Professor, The Ohio State University

30C) An Integrated Loads Analysis Model for Wake Vortex Encounters Dipl.-Ing Thiemo Kier, Research Engineer, German Aerospace Center (DLR)

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 GirodrouxLavigne, Head of Modelling and Numerical Simulation of Aeroelasticity Research Unit, ONERA – The French Aerospace Lab

28D) Multi-Disciplinary Wing Optimisation using a Discipline-Specific TrustRegion Method

29D) Time Domain Aeroelastic Solution Using Exact Aerodynamic Influence Coefficients and Nonlinear Damping Dr Vin Sharma, Flutter Engineer, Air Force SEEK EAGLE Office

30D) Efficient, LaplaceDomain Aerodynamics for Load Analyses Dr David Eller, Flight Dynamics Group, Royal Institute of Technology (KTH)

31D) Aeroelastic Design Exploiting Structural Geometric Nonlinearities Prof Jonathan Cooper, Airbus Sir George White Chair of Aerospace Engineering, University of Bristol

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

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

31E) Geometrically Non-linear Structural Modal Analysis for Local and Impulsive Excitation Lars Oliver Bernhammer, PhD Student, Delft University of Technology

Networking Lunch

Networking Lunch

Networking Lunch

09:00

09:30

11:00

Dr Simão Marques, Lecturer in Aerospace Engineering, Queen’s University Belfast 11:30

12:00

Networking Lunch

Exhibitors attending in the Lancaster Room:

Supporters:

FOR MORE INFORMATION

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13/06/2013 19:39:08

PROGRAMME / DAY 3 – WEDNESDAY 26 JUNE (cont)

Kings Room - 1st Floor

Parallel 1 - 2nd Floor

Parallel 2 - 2nd Floor

Parallel 3 - 3rd Floor

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

SESSION 33: COMPUTATIONAL AEROELASTICITY 5 33A) Flutter Optimisation of a Biaxial Composite Plate in Terms of Fiber Orientation via Genetic Algorithm Levent Unlusoy, Lecturer, University of Turkish Aeronautical Association

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)

SESSION 35: ROTATING SYSTEMS / TURBOMACHINERY 3 35A) Counter-Rotating Open Rotor Whirl Flutter Phenomenon. Investigations using elsA solver Dr Simon Verley, Research Scientist, ONERA

14:00

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

33B) Stochastic LCO Analysis for an Airfoil by Intrusive PCE Method Dr Yuting Dai, Lecturer, Beihang University

34B) Development of a Structural Model of the CRM Configuration for Aeroelastic and Loads Analysis Thomas Klimmek, Research Scientist, DLR, German Aerospace Centre, Institute of Aeroelasticity

35B) Propeller – Flexible Wing Interaction using Rapid Computational Methods Chenhui Liu, Flight Physics Engineering Intern, Airbus

14:30

32C) Experimental Investigation of the Aeroelastic Behaviour of a Laminar Airfoil in Transonic Flow Anne Hebler, Research Engineer, German Aerospace Center (DLR)

34C) Spectral Finite Element Modelling and Updating in Aeroelastic Analysis of Light Sport Aircraft Joseph Gross, Research Associate, Hamburg University of Technology

35C) Rotorcraft Aeroelastic Analysis using Dynamic Wake/ Dynamic Stall Models and its Validation Rohin Kumar, PhD Student, Indian Institute of Technology Kanpur

15:00

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

33C) A Novel Computational Approach to Unsteady Aerodynamic and Aeroelastic Flow Simulation Eliot Quon, Graduate Research Assistant, Georgia Institute of Technology

15:30

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

13:30

16:00

16:30

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)

17:00

36C) High-Fidelity Simulation of Aeroelastic Wind Gust Effect in Aerodynamic Shapes Dr Ruben Sevilla, Lecturer, Swansea University

17:30

35D) Numerical Investigation of an L-Shaped Deployable Gurney Tab for Rotorcraft Vibration Control Valentina Motta, PhD Candidate, University of Milan

33D) Aerodynamic Optimisation of a Flexible High-Lift Wing Giuseppe Trapani, EngD Researcher, Cranfield University

Networking & Tea Break SESSION 37: COMPUTATIONAL AEROELASTICITY 6 37A) Optimisation of the WingStore Position For Maximum Flutter Speed Omer Bajwa, Post Graduate Student, NUST College of Electrical and Mechanical Engineering

Networking & Tea Break SESSION 38: UNCERTAINTY 2 38A) Uncertainty Quantification in Aeroelastic Composite Structures Using Lamination Parameters Carl Scarth, PhD student, ACCIS Centre, University of Bristol

37B) Optimal Control Surfaces Layout For An Active Aeroelastic Wing Ronan Goachet, PhD Student, Bristol University

38B) Application of Uncertainty Management to Improve Reliability of Hard Landing Criticality Assessment Criteria Thomas Wilson, Head of Technical Capability for Aircraft Loads, Airbus Operations Ltd

37C) Using Proper Orthogonal Decomposition and Dynamic Mode Decomposition Methods for Comparing CFD Results Experimental Measurements Amandine Guissart, PhD Student, University of Liège

38C) Uncertainties in Measurements and Data Evaluation Concerning Transonic High Reynolds Number Wind Tunnel Tests Dr Alexander Boucke, Scientist, ITAM GmbH

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-‫ ט‬Honeycomb 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

CLOSING CEREMONY AND IFASD2015 ANNOUCEMENT

THURSDAY 27 JUNE 2013 Technical Tours to Airbus, National Composite Centre and University Bristol. Please see tour information for more details.

FOR MORE INFORMATION

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