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Preliminary Programme
Sunday 28th June 2015 19:00‐21:00 Pre‐registration and welcome reception in Sokos Hotel Palace Bridge Monday 29th June 2015 Morning 9:00‐10:15 10:15‐10:30 Registration Welcome coffee Welcome Opening Ceremony Ball Room 10:30‐11:15 Keynote lecture 1 System Methodology of Aeroelastic Research and its Role in the Design Process for Contemporary Aircraft. Prof. Sergey Chernyshev, TsAGI, Russia 11:15‐12:00 Keynote lecture 2 Recent Progress in Prediction of Buffet and Aeroacoustic Environments at NASA. Prof. David M. Schuster, NASA Langley Research Center, USA 12:00‐13:30 Lunch ifasd_2015_preliminary_programme_2015_05_07 Page 1 Monday 29th June 2015 Afternoon 13:30‐14:00 14:00‐14:30 14:30‐15:00 15:00‐15:30 Session 1 Session 2 Computational Aeroelasticity 1 Aerodynamics/CFD 1 Lorenz Tichy Kumar Bhatia Session 3 Experimental Methods 1 Mikhail Zichenkov IFASD‐2015‐088 Investigation of Shock Buffet Onset on Swept Wings S. Timme and F. Sartory University of Liverpool, UK IFASD‐2015‐145 Test and Analysis of a Gust Generator Kenichi Saitoh, Shunsuke Koike (JAXA) and Koichi Suzuki (ISE), Japan IFASD‐2015‐097 Linearized FUN3D for rapid aeroelastic design and analysis Chen Ping‐Chih, Zhicun Wang, ZONA Technology, Inc, USA IFASD‐2015‐209 An Eulerian‐Arbitrary Lagrangian Eulerian Computational Framework for Highly Nonlinear Turbulent Fluid‐Structure Interaction Problems and Validation for Buffeting and Flapping Wing Applications Charbel Farhat, Vinod Lakshminarayan Stanford University, USA IFASD‐2015‐012 Theoretical and experimental investigation of a structurally and aerodynamically nonlinear pitch and flap wing E.Verstraelen, J.Boutet, C.Grappasonni, G.Kerschen, G.Dimitriadis University of Liège, Belgium ifasd_2015_preliminary_programme_2015_05_07 Loads 1 Brian Caldwell Jos Meijer IFASD‐2015‐054 IFASD‐2015‐124 IFASD‐2015‐089 Nonlinear Actuator Modeling for Design and testing of a gust generator for a Application of numerical simulation for the Aeroservoelastic Dynamic Loads Simulations detection and analyzing rough landings of low subsonic wind tunnel Rami Veiberman, Martin Weiss and Moti Paul M.G.J. Lancelot, Jurij Sodja, Noud P.M. aircraft Werter, and Roeland De Breuker Karpel Rybin Andrey, JSC Tupolev, Russian Delft University of Technology, The Technion, Haifa, Israel Netherlands IFASD‐2015‐071 Industrial Frequency‐Domain Linearized Navier‐Stokes Calculations for Aeroelastic Problems in the Transonic Flow Regime G. Broux, F. Chalot, L. Daumas, N. Forestier, Z. Johan and M. Mallet DASSAULT AVIATION, France 15:30‐16:00 Session 5 IFASD‐2015‐117 IFASD‐2015‐066 Comparison of different approaches for Verification of the use of small‐disturbance modeling of atmospheric effects like gusts CFD aerodynamics in flutter and gust and wake‐vortices in the CFD Code TAU analyses for simple to highly complex Ralf Heinrich, Lars Reimer, configurations 1 2 DLR, Braunschweig, Germany Cyrille Vidy , Lukas Katzenmeier , Maximilian Winter2, Christian Breitsamter2 1 Airbus, Germany 2 TU München, Germany IFASD‐2015‐119 Accelerated convergence of high‐fidelity aeroelasticity using low‐fidelity aerodynamics Kristofer Jovanov, Roeland de Breuker Delft University, The Netherlands Session 4 Aeroservoelasticity 1 IFASD‐2015‐167 IFASD‐2015‐065 Aeroservoelasticity problems in transonic Effects of flight mechanics model flow simplification in a state space aeroelastic S. Kuzmina, F. Ishmuratov, V. Popovsky, model for loads analysis A.Chizhov Bimo Prananta, Rob Huls, Hans van Tongeren, Toni Kanakis TsAGI, Russia NLR, The Netherlands IFASD‐2015‐010 Optimisation of active systems for wing vibration control Salvatore Maraniello, Rafael Palacios Imperial College London, UK IFASD‐2015‐183 Aircraft Dynamic Loads with Varying Geometry and Flight Mechanics Effects Moti Karpel and Aviv Romm Technion, Haifa, Israel Manuel Reyes and Hector Climent Airbus Defence & Space, Getafe, Spain IFASD‐2015‐173 IFASD‐2015‐157 IFASD‐2015‐159 IFASD‐2015‐015 Analysis of flight loads and static Frequency‐domain approach for transonic An experimental demonstration of active Control of the GNBA Aircraft Based on a transonic buffet control using a closed‐loop Unified Dynamics Formulation with Inclusion aeroelasticity characteristics of the airplane unsteady aerodynamics modelling methodology with the use of three‐dimensional Adrien Poncet‐Montanges, Dorian Jones, of Airframe Flexibility Arnaud Lepage, Arnaud Geeraert, Julien aerodynamics Jonathan E Cooper, University of Bristol, UK. Rafael M. Bertolin M. Kwiatkowska, R. Leonteva, PSC Tupolev, Yves Lemmens, Siemens Industry Software Dandois, Pascal Molton, Frederic Ternoy, Jean Flavio J. Silvestre ITA, Brazil Bernard Dor, Eric Coustol Denis Nekhaev, MSC.Software, Russia NV, Belgium ONERA, France Coffee break Page 2 16:00‐16:30 16:30‐17:00 17:00‐17:30 IFASD‐2015‐180 Aeroelastic response simulations of exible aircraft with the commercial structural solver Abaqus M. C. Ruggeri and R. G. A. da Silva, ITA, Brazil C. E. de Souza, UFGRS, Brazil IFASD‐2015‐163 IFASD‐2015‐042 Formation of Chimneys in Flutter Boundaries Sensor Calibration for Calculation of Loads on a Flexible Aircraft at Transonic Mach Numbers Marcus Vinicius Preisighe Viana Oddvar O. Bendiksen, DLR, Germany University of California, USA IFASD‐2015‐074 Dynamic stability of a hose‐drogue‐wing system for aerial refueling P. García‐Fogeda* and F. Arévalo** *ETSIAE, SPAIN, ** AIRBUS, Getafe SPAIN IFASD‐2015‐008 Monitoring of Loads and Accumulated Fatigue Damages of Each Individual Aircraft in Service V.I. Kleptsov1, T.I. Orlova2, V.I. Tsimbalyuk2 1 Beriev Aircraft Company, Russia 2 TsAGI, Russia IFASD‐2015‐206 IFASD‐2015‐096 Numerical Study of the Transonic Limit Cycle Nonlinear aeroelastic modeling via Oscillation Phenomenon on the F‐16 Fighter conformal mappings for a typical section in Aircraft arbitrary motion Michael Iovnovich and Dan Michaels and C. Risoa, G. Riccardib, F. Mastroddia a Motti Adar, Israeli Air Force, Sapienza University of Rome Daniella E. Raveh, Technion, Israel b Second University of Naples, Italy IFASD‐2015‐051 Identification of aeroelastic MIMO models from time‐varying data Julien Ertveldt, John Lataire, Rik Pintelon, Steve Vanlanduit Vrije Universiteit Brussel, Belgium IFASD‐2015‐072 Coupled electro‐mechanical modelling of integrally actuated membrane wings Stefano Buoso and Rafael Palacios Imperial College, London, UK IFASD‐2015‐086 Gust Response analysis of High Altitude, Long Endurance aircraft Chen Zhanjun, Fu Zhichao, Lv Jinan, Liu Ziqiang China Academy of Aerospace Aerodynamics, Beijing, China IFASD‐2015‐041 IFASD‐2015‐070 Combined unsteady aerodynamics and Unsteady and Post‐Stall Aerodynamic structural response on auxiliary power unit Modeling for Aircraft Dynamics Simulation flap door: theoretical method and flight test Ryan Paul1 , Joseba Murua2 , and Ashok comparison Gopalarathnam1 Ángel Palomares Mora, Ramón Abarca López 1 North Carolina State University, USA APU, Airbus, Madrid, Spain 2 University of Surrey, UK Marcus Barth, Airbus SAS, France IFASD‐2015‐093 IFASD‐2015‐036 IFASD‐2015‐131 Experimental identification of the flexibility Structural Damping Influence on Airplane Scaling laws in aeroservoelasticity influence matrixof the aircraft engine Dynamic Loads at Flight in Turbulence and at Raphael Klein (NLR‐TU Delft) mounted on pylon under the wing Run Bimo Prananta (NLR) and Roeland de Breuker Alexei Grigoriev, Victor Malyutin, Alexei Oleg Kuznetsov (TU Delft), The Netherlands Chizhov, Andrei Gubernatenko TsAGI, Russia TsAGI, Russia IFASD‐2015‐030 Isogeometric Framework for Aeroelastic Wind Turbine Rotor Analysis Etana A. Ferede, Mostafa M. Abdalla, Delft University, The Netherlands, Johannes K.S. Dillinger, DLR, Germany 17:30‐18:00 IFASD‐2015‐174 Analysis and Computational Study of the Dynamics and Aeroelasticity of Generic Flapping Wings Harijono Djojodihardjo Universiti Putra Malaysia IFASD‐2015‐001 IFASD‐2015‐107 IFASD‐2015‐115 Investigation about the improvement in the MultiObjective Optimization for Servoelastic Non‐linear structural dynamics aspects of data acquisition for aeroelastic analysis Response Predictions of a Flexible Aircraft the aerial refueling boom system through the use of PZT excitation and test Ashok Joshi, Prabha Srinivasan Félix Arévalo, Sebastián Claverías, and Héctor parameters definition IIT Bombay, India Climent Indira Narayanaswamy, Hemalatha E AIRBUS Defence & Space E. L. Oliveira1, A. Suleman1, R. G. A. da Silva2, Getafe, Madrid, Spain ADA, India A. G. Marto3, F. Afonso1 1 IST, Portugal 2 Aeronautics Institute of Technology, Solid Mechanics and Structures, Brazil 3 Aeronautics and Space Institute, Brazil 18:00‐18:30 Poster presentations 19:00‐22:00 Cruise on the Neva, Forum Furshet ifasd_2015_preliminary_programme_2015_05_07 Page 3 Tuesday 30th June 2015 Morning Ball Room 08:15‐09:00 Keynote lecture 3 Embraer, Brazil 09:00‐09:30 Coffee break 09:30‐10:00 10:00‐10:30 10:30‐11:00 Session 6 Session 7 Session 8 Session 9 Session 10 Computational Aeroelasticity 2 Aerodynamics/CFD 2 Aeroelastic Optimisation 1 GVT & Flight Test 1 Aeroelasticity in Aircraft Design 1 Carlos Cesnic Anders Karlsson Raymond Kolonay Eric Garrigues Sergio Ricci IFASD‐2015‐178 OpenFSI interface for strongly coupled steady and unsteady aeroelasticity C.Valente, D.Jones, A.Gaitonde, J. E.Cooper University of Bristol, UK Y. Lemmens Siemens Industry Software, Belgium IFASD‐2015‐060 Continuous‐time state‐space unsteady aerodynamic modelling for efficient aeroelastic load analysis Noud Werter , Roeland De Breukery and Mostafa Abdallaz Delft University, The Netherlands IFASD‐2015‐044 Optimization of an Aeroelastic Wing considering Airworthiness Requirements K. Seywald, A. Wildschek, F. Holzapfel Airbus Group Innovations, Germany IFASD‐2015‐154 Limit‐Cylcle‐Oscillation Simulations of AEROSTABIL Windtunnel Experiments II Bernd Stickan, Johannes Dillinger, Jens Nitzsche DLR, Germany IFASD‐2015‐011 Unsteady Viscous‐Inviscid Coupling Simulations Of Separated Laminar Flows Around 2D Airfoils Jose I. Rothkegel, Grigorios Dimitriadis Universite de Liege, Belgium IFASD‐2015‐140 IFASD‐2015‐079 State of the art of GVT technology in Russia Aeroelastic Optimization of a Passive Morphing Airfoil using Isogeometric Analysis and possible directions to increase accuracy Erik Gillebaart and Roeland De Breuker and reliability Delft University, The Netherlands P. Karkle, M. Pronin, M. Bogatyrev, TsAGI, Russia K.Dijkstra, Prodera, France IFASD‐2015‐056 IFASD‐2015‐156 A software for filtering ground vibration test Flutter Prediction and Optimization of an measurements and its use for identification Aeroelastic Wing with respect to Wing‐Store Position of dynamic properties of aircraft structures Omer I. Bajwa, Haroon A. Baluch S.Hernandez1, E.Menga2, M.Cid1, S.Moledo1 1 AERO, Pakistan University of Coruna, Spain 2 EGLRG‐AIRBUS Operations, Getafe, Spain IFASD‐2015‐049 Modeling of Dynamic Behavior of Lattice Composite Aircraft Structures A.Bezuevskiy, I.Kondakov, A.Shanygin, M.Zichenkov TsAGI, Russia IFASD‐2015‐147 IFASD‐2015‐034 IFASD‐2015‐101 IFASD‐2015‐151 IFASD‐2015‐075 Efficient Analysis of HALE Aircraft Structure Transonic Limit Cycle Oscillation Analysis of Genetic and Gradient‐based Algorithms for Nonlinear ground vibration identification of Aeroelastic optimization of wing shape and the Multi‐objective Optimization of Aircraft an F‐16 aircraft. Part I: Fast nonparametric structural parameters for different aircraft for Static and Dynamic Aeroelastic Behavior Aerostabil Wind Tunnel Model Design with Aeroelastic Constraints Lu LIU, Taehyoun Kim configurations analysis of distortions in FRF measurements Hitoshi Arizono, Kenichi Saitoh, Masato S. Gemma, F. Mastroddi National University of Singapore Kirill Balunov, Vasily Chedrik, Fanil M.Vaes1, J.Schoukens1,B. Peeters2, Tamayama University of Rome La Sapienza, Italy Ishmuratov, Petr Karkle J.Debille2, T.Dossogne3, J.P.Noel3, Japan Aerospace Exploration Agency, Japan TsAGI, Russia G.Kerschen3 1Vrije Universiteit Brussel, Belgium 2 LMS ‐ Siemens PLM Software, Belgium 3University of Liege, Belgium ifasd_2015_preliminary_programme_2015_05_07 Page 4 11:00‐11:30 11:30‐12:00 IFASD‐2015‐048 Multiple Input Describing Function Analysis of Non‐Classical Aileron Buzz M. Irfan Zafar, Francesca Fusi and Giuseppe Quaranta Politecnico di Milano, Italy IFASD‐2015‐204 Non‐linear unsteady aerodynamics application for airliner flutter research Chuban A.V., Chuban V.D. JSC Irkut Corporation, Moscow, Russia 12:00‐13:30 ifasd_2015_preliminary_programme_2015_05_07 IFASD‐2015‐037 APF Sonic Fatigue Marcus BARTH, Simon TRAPIER, Mathieu BERTHOMET Airbus Operations SAS, France Saravanan RAJAN Airbus Engineering Centre, India IFASD‐2015‐129 IFASD‐2015‐035 IFASD‐2015‐123 Nonlinear ground vibration identification of Aeroelastic Tailoring using Crenelated Skins ‐ Design and testing of an aeroelastically tailored wing under manoeuvre loading Modelling and Experiment an F‐16 aircraft. Part II: Parameter Noud P.M. Werter, Jurij Sodja, Peter Loeffen G.François, J.E.Cooper & P.Weaver estimation using a frequency‐domain and Roeland De Breuker University of Bristol, UK subspace method Delft University, The Netherlands T. Dossogne, J.P. Noel, C. Grappasonni, G. Kerschen, University of Liege, B. Peeters, J. Debille, Siemens, Belgium M. Vaes, J. Schoukens Vrije Universiteit Brussel, Belgium IFASD‐2015‐019 Recent achievements towards aero‐ structure gradient computation using high‐fidelity CFD/CSM in the Onera/elsA software Christophe Blondeau Onera, France IFASD‐2015‐052 IFASD‐2015‐024 AIRBUS A320 NEO GVT and FEM updating. High Fidelity Simulation of the Folding Wing Tip State‐of‐the‐art techniques to perform an industrial vibration test campaign and a John Pattinson, Martin Herring, Tom rapid process to update renewed FEM for Wilson clearance of First Flight Test Airbus Group Innovations, UK S. Giclais, C. Stephan, P. Lubrina, ONERA; Y. Govers, M. Boeswald, DLR; T‐P Vo‐Hoang, A. Laporte, AIRBUS Lunch Page 5 Tuesday 30th June 2015 Afternoon 13:30‐14:00 14:00‐14:30 14:30‐15:00 Session 11 Session 12 Session 13 Session 14 Session 15 Nonlinearities & Uncertainties Loads alleviation Aeroelastic Response & Stability Experimental Methods & Bridges Rotation System Vincenzo Vaccaro Hector Climent Alexis Laporte Petr Karkle Alessandro Scotti IFASD‐2015‐182 Uncertainty quantification in aeroelastic response of idealized composite wing C.T. Nitschke, J. Maruani, A. Vincenti, D. Lucor, J.‐C. Chassaing Sorbonne Universités, Paris, France IFASD‐2015‐057 Wind Tunnel Experimental Validation of Future Green Regional A/C Gust Load Alleviation Control System S.Ricci, S.Adden, C.Servadio, M.Karpel and J.Cooper Politecnico di Milano, Italy; Technion, Israel; University of Bristol, UK IFASD‐2015‐091 Computational Benchmark of Commercial Fluid‐Structure Interaction Software Nicholas F. Giannelis and Gareth A. Vio The University of Sydney, Australia Oleg Levinski Air Vehicles Division, Defence, Science and Technologies Organisation, Australia IFASD‐2015‐050 An over view of aeroelastic experiments on the Active Aeroelastic Test Bench (AATB) Julien Ertveldt, Johan Schoukens, Rik Pintelon, Steve Vanlanduit Vrije Universiteit Brussel, Belgium IFASD‐2015‐025 Periodic Output Feedback Control for Helicopter’s Vibration Reduction Claudio Brillante, Marco Morandini, Paolo Mantegazza Politecnico di Milano, Italy IFASD‐2015‐005 Aeroelastic Modeling and Simulation of Flexible Jet Transport Aircraft with High‐Aspect‐Ratio Wings Ryan C. Kitson and Carlos E.S. Cesnik University of Michigan, USA IFASD‐2015‐077 Probabilistic Robust Control Strategy for Gust Load Alleviation Yuting Dai, Chao Yang Beijing University of Aeronautics and Astronautics, China IFASD‐2015‐027 IFASD‐2015‐068 A comparison of modeling methods for the Research on Dynamic Stability of an Elastic simulation of free flying highly elastic Model Using Tests in Artificial Flow aircraft G.V.Liseykin, M.M.Bogatyrev, M.A.Pronin, K. Seywald, F. Holzapfe V.I.Smyslov Airbus Group Innovations, Germany TsAGI, Russia IFASD‐2015‐023 CROR blade deformation, part 1: Experimental results by Strain Pattern Analysis Arnaud GEERAERT, Cyrille STEPHAN Onera, France IFASD‐2015‐009 Asymmetric limit cycle oscillations in systems with symmetric freeplay G.Dimitriadis University of Liège, Belgium 15:00‐15:30 15:30‐16:00 ifasd_2015_preliminary_programme_2015_05_07 IFASD‐2015‐043 IFASD‐2015‐143 IFASD‐2015‐103 IFASD‐2015‐192 CROR blade deformation, part 2: A complete experimental investigation of The Aeroelastic Impact of Engine Thrust and Aeroelastic investigation using piezoelectric Aeroelastic computations and comparison materials as sensor and actuator gust load: from generation to active control Gyroscopics on Aircraft Flutter Instabilities Stefan Waitz — DLR, Germany with experiments Arnaud LEPAGE, Yannick AMOSSE, Dominique E. L. Oliveira1, A. Suleman1, R. G. A. da Silva2, Yann MAUFFREY, Arnaud GEERAERT Le Bihan, Charles POUSSOT‐VASSAL, Vincent A. G. Marto3, F. Afonso1 ‐ 1IST, Portugal Onera, France BRION ‐ ONERA, FRANCE 2 Aeronautics Institute of Technology, Solid Eric RANTET ‐ AVIATION DESIGN, FRANCE Mechanics and Structures, Brazil 3 Aeronautics and Space Institute, Brazil IFASD‐2015‐133 IFASD‐2015‐193 IFASD‐2015‐105 IFASD‐2015‐106 Dynamic Load Alleviation of Flexible Aircraft Influence of gyroscopic forces on Alternative Problem Formulations for Wind Tunnel Test of a Morphing Wingtip Leading Edge in Wake Vortex Encounters aeroelasticity characteristics of an airplane Identification of Mathematical Model of R C M Cheung, C Wales, J E Cooper, Henrik Hesse ‐ ETH Zurich with engines on pylons under the wing Helicopter Rotor Blade and Some Problems University of Bristol, UK Rafael Palacios ‐ Imperial College London, UK A.Kuznetsov, S.Kuzmina, F.Ishmuratov, of Aeroelasticity Analysis V.Eremin, S. Paryshev S Vasista, J Riemenschneider, B van de Kamp, V.Mosunov TsAGI, Russia H P Monner TsAGI, Russia DLR, Germany Coffee break Page 6 16:00‐16:30 16:30‐17:00 17:00‐17:30 17:30‐18:00 IFASD‐2015‐207 Limit‐cycle Oscillations of a Pre‐tensed Membrane Strip Ariel Drachinsky and Daniella E. Ravehy Technion, Haifa, Israel IFASD‐2015‐199 Integrated Optimization of Ailerons for Active Gust Load Alleviation Manuel Pusch, Andreas Knoblach, Martin Leitner, Thiemo Kier DLR, Germany IFASD‐2015‐013 A parametric and topological study on the use of viscoelastic material for flutter suppression Mauricio V. Donadon, Roberto G.A. da Silva, ITA, Brazil André G.C. Filho, Antonio M.G. de Lima Federal University of Uberlândia, Brazil IFASD‐2015‐014 Flutter and buffeting of long span suspension bridges in fully erected and partially erected conditions Matteo Massaro, Konstantinos N. Bakis, David J.N. Limebeer ‐ Oxford University, UK Michael J.R. Graham Imperial College London, UK IFASD‐2015‐153 Installed counter‐rotating open rotor whirl flutter phenomenon investigations using elsA solver Simon Verley, Alain Dugeai ONERA, France IFASD‐2015‐144 IFASD‐2015‐080 IFASD‐2015‐090 System Identi cation of the Aeroelastic Gust Alleviation of a Simulated Regional Jet Dynamics of a Large Ring‐Shaped Structure Towed via a Heavy Rope Galloping Problem via Convex Optimisation Model using Multiple Control Surfaces Abhinav R. Dehadrai, Ishan Sharma and Nicholas F. Giannelis, Gareth A. Vio, Ian R. C.Howcroft, D.Calderon, J.E.Cooper, Shakti S. Gupta Manchester A.Richards Indian Institute of Technology Kanpur The University of Sydney, Australia University of Bristol, UK IFASD‐2015‐164 IFASD‐2015‐038 Investigation of loading parameters of a Rotor dynamics of compact gas turbine unit with gas bearings investigation trunk‐route airplane wing in a wind tunnel Temis J.M., Temis M.J., Egorov A.M., Gavrilov near to buffet boundary V.V., Ogorodov V.N. Bragin N., Garifullin M., Skomorokhov S., CIAM, Russia Yanin V. TsAGI, Russia IFASD‐2015‐195 Experimental and Numerical LCO Analysis of a Cropped Wing with External Store Considering Various Parameters M.MousaviSani ‐ Ferdowsi University of Mashhad, Iran H.Golparvar, S.Irani ‐ K.N. Toosi University Technology, Tehran, Iran IFASD‐2015‐102 Influence of Controllability and Stability Augmentation Systems on Loads Frequencies T.I. Orlova, V.I. Tsimbalyuk, A.S. Ustinov TsAGI, Russia IFASD‐2015‐017 Comprehensive Study of Geometric Nonlinearities of Rotating Beams Zahra Sotoudeh Rensselaer Polytechnic Institute Troy, NY, USA IFASD‐2015‐148 Structural dynamic investigations of adaptive wing demonstrator within SADE project G.A. Amiryants, V.P. Kulesh, V.A. Malyutin, A.V. Smotrov, A.V. Chedrik TsAGI, Russia IFASD‐2015‐176 Aeroelastic Analysis of A Helicopter Blade Under Arbitrary Time‐Dependent External Excitations Özge Özdemir Istanbul Technical University, Turkey IFASD‐2015‐130 Embedding a Multi‐Body Model of a Fixed‐ Wing Aircraft in a Nonlinear State Observer Tuur Benoit, Yves Lemmens SISW N.V, Belgium Wim Desmet ‐ KU Leuven, Belgium IFASD‐2015‐062 Aeroelastic Analysis Modelling Process to Predict the Critical Loads in an MDO Environment René LIEPELT, Diliana DIMITROV, Thomas KLIMMEK DLR, Germany IFASD‐2015‐007 Flight mechanic modeling and analysis of multi‐body‐aircraft Alexander Köthe, Robert Luckner TU Berlin, Germany IFASD‐2015‐169 Noncontact diagnostic of the aeroelastic oscillations turbomachinery blades A.A. Khorikov, S.Y. Danilkin CIAM, Russia IFASD‐2015‐188 Compressor blade and disc optimal structural design Joury Temis, Denis Yakushev CIAM, Russia IFASD‐2015‐205 Vibration Analysis of Rotating Composite Pretwisted Blades Serhat Uzun, Özge Özdemir Istanbul Technical University, Turkey 18:00‐18:30 19:00‐22:00 ifasd_2015_preliminary_programme_2015_05_07 Forum Banquet in Petro‐Pavlovsky Fortrees Page 7 Wednesday 01 July 2015 Morning 09:00‐09:30 Session 16 Session 17 Session 18 Session 19 Session 20 Computational Aeroelasticity 3 Aerodynamics/CFD 3 Aeroelastic Optimization 2 Aeroelasticity in Aircraft Design 2 GVT & Flight Test 2 David Schuster Jonathan Cooper Vasily Chedrik Vitaly Chuban Sergey Paryshev IFASD‐2015‐168 Influence of the boundary layer on flutter of elastic plate in supersonic gas flow Vsevolod Bondarev, Vasily Vedeneev Moscow State University, Russia IFASD‐2015‐186 Accelerated Flutter and Gust Response Calculation using DLR‐TAU S. Xu , S. Timmey and K. J. Badcockz University of Liverpool, UK 09:30‐10:00 10:00‐10:30 ifasd_2015_preliminary_programme_2015_05_07 IFASD‐2015‐087 IFASD‐2015‐181 IFASD‐2015‐116 Static Aeroelastic Sti ness Optimization of a Enhanced free vibration analysis of An Advanced Panel Method for Forward Swept Composite Wing with CFD composite wing‐box structures by one‐ Compressible Subsonic Unsteady Corrected Aero Loads dimensional component‐wise and dynamic Flow Past Complex Geometries stiffness formulations Steven Fiddes, Chris Burkett, Johannes Dillinger1, Mostafa Abdalla1, Yasser E. Carrera, A. Pagani Flow Solutions Limited, Bristol, UK Meddaikar1, Thomas Klimmek1 Politecnico di Torino, Italy. Thiemo Kier ‐ DLR, Germany 1 DLR, Germany P.H. Cabral, G. Caprio and A. Prado 2 Delft University of Technology, The Embraer, Brazil Netherlands IFASD‐2015‐179 Integrated Flexible Dynamic Loads Models based on Aerodynamic Influence Coefficients of a 3D Panel Method Thiemo Kier, Mark Verveld DLR, Germany Chris Burkett Flow Solutions Limited, Bristol, UK IFASD‐2015‐121 A Dassault industrial approach for aero‐ structural optimization S. Meldrum, P. Hardy, G. Broux, E.Garrigues Dassault Aviation, FRANCE IFASD‐2015‐061 Ensuring Flutter Safety of Sukhoi SSJ‐100 Regional Aircraft Alexey Orlov, Sergey Shalaev, TsAGI, Russia Sergey Kalabuchov Gromov Flight Research Institute, Russia IFASD‐2015‐095 An efficient approach for in‐operation modal analysis of flutter flight tests Beatrice JACQUIER Onera, S. LEROY, D. WALKER AIRBUS OPERATIONS SAS, France IFASD‐2015‐122 The Use of Dynamic Strain Sensors and Measurements on the Ground Vibration Testing of an F‐16 Aircraft F.L.M.Santos1,2,3, B. Peeters1, J.Debille1, C.Salzano4, L.C.S.Góes2, W.Desmet3 1 SISW, Leuven, Belgium, 2ITA, Brazil 3 KU Leuven, Leuven, Belgium 4 PCB Piezotronics Inc., Depew, USA Coffee break Page 8 10:30‐11:00 11:00‐11:30 11:30‐12:00 IFASD‐2015‐134 Dynamic instabilities of circulation controlled aerofoils Ian Krukow, Dieter Dinkler, Nora Neuert TU Braunschweig, Germany IFASD‐2015‐045 A transfer function approach to model unsteady aerodynamics T. De Troyer, J. Decuyper, and M.C. Runacres Vrije Universiteit Brussel, Belgium IFASD‐2015‐081 A Novel Method for the Vibration Optimisation of Structures Subjected to Dynamic Loading David J. Munk, Gareth A. Vio, Grant Steven The University of Sydney, Australia IFASD‐2015‐162 IFASD‐2015‐032 Multidisciplinary Computational System Application of a modern on‐board excitation "PARUS‐INT" for Design and Certification of system during the in‐flight vibration testing of a business jet Airplanes in Static and Dynamic Strength and Gomes da Silva, Demian; Service Life Padovese C., Gustavo G.I.Turchannikov, M.M.Levchenko, EMBRAER S.A., Brazil V.V.Chedrik, D.V.Chemisov TsAGI, Russia IFASD‐2015‐175 A correlation study of modal parameters between flutter testing and CFD simulation Stefano Orlando, Marc Brughmans Siemens SISW, Belgium Taylan KARAAĞAÇLI, Muhammed Emin, Ümit CEYHAN Tubitak –SAGE, Turkey IFASD‐2015‐004 On the Validity Range of Piston Theory Marius‐Corné MEIJER, Laurent DALA University of Pretoria, South Africa IFASD‐2015‐137 Aeroelastic tailoring and structural optimisation using an advanced dynamic aeroelastic framework Noud Werter and Roeland De Breuker Delft University of Technology, The Netherlands IFASD‐2015‐022 Estimating the elastic‐mass characteristics of lifting surface at early design stages A.V. Boldyrev, V.A. Komarov Samara State Aerospace University, Russia IFASD‐2015‐101 Nonlinear ground vibration identification of an F‐16 aircraft. Part I: Fast nonparametric analysis of distortions in FRF measurements M.Vaes1, J.Schoukens1,B. Peeters2, J.Debille2, T.Dossogne3, J.P.Noel3, G.Kerschen3 1 Vrije Universiteit Brussel, Belgium 2 LMS ‐ Siemens PLM Software, Belgium 3 University of Liege, Belgium IFASD‐2015‐053 Design of elastically scaled model using digital technologies O. A. Orlova TsAGI, Russia IFASD‐2015‐158 Ground tests of the airplane with reproduction of a rotating force Regina Leonteva TsAGI, Russia IFASD‐2015‐166 Prediction of aeroelastic limit‐cycle oscillations based on harmonic forced motion oscillations A.C.L.M. van Rooij, J. Nitzsche DLR, Germany 12:00‐13:30 ifasd_2015_preliminary_programme_2015_05_07 IFASD‐2015‐055 IFASD‐2015‐078 Evolutionary approach to structural design Using 2D‐PIV measurements to compute of wing under stress, buckling and unsteady aerodynamic loads on a flat plate aeroelasticity requirements at high angle of attack Chedrik V.V., Tuktarov S.A. A. Guissart , L. Bernal & V.E. Terrapon TsAGI, Russia University of Liege, Belgium Lunch Page 9 Wednesday 01 July 2015 Afternoon 13:30‐14:00 14:00‐14:30 14:30‐15:00 15:00‐15:30 15:30‐16:00 Session 21 Session 22 Aeroservolasticity & Activ Control Crashworthiness Bimo Prananta Flavio Silvestre Session 23 Session 24 Aeroelasticity of Morphing Reduced Order Modelling Jean‐Pierre Grisval Aircraft Moti Karpel Luca Benassi IFASD‐2015‐018 IFASD‐2015‐172 IFASD‐2015‐082 IFASD‐2015‐139 Investigating the Benefits of Morphing Wing Research experience of aeroelastic LCO of Nonlinear Reduced‐Order Modeling of Experimental Ditching Loads Tip Devices‐‐‐A Case Study maneuverable missile with electrical Unsteady Aerodynamic Loadsbased on H. Climent, G. Pastor, J.T. Viana, L. Benitez actuator of control fin Airbus Defence and Space. Military Transport Chen Wang, Hamed H Khodaparast, Michael I DynamicLocal Linear Neuro‐Fuzzy Models Friswell A. Bykov, G. Kondrashev Maximilian Winter, Christian Breitsamter Aircraft, Spain Swansea Univerisity, UK Vympel Design Bureau JSC, Russia TU München, Germany A.Iafrati ‐ CNR‐INSEAN, Italy V. Smyslov ‐ TsAGI, Russia IFASD‐2015‐039 IFASD‐2015‐028 Nonlinear Aeroservoelastic Analysis for a Numerical Simulation of Ditching Dynamic Three‐Dimensional Horizontal Stabilizer with Loads an Actuator Composed of Elastic Links J.T.Viana, J.Romera, G.Pastor, L.Benitez, Yoo Jin Kang, Jae Hyeok Jeon, Chan Hoon H.Climent Chung, Sang Joon Shin, Young Ho Na Airbus Defence and Space. Military Transport Aircraft, Spain. Seoul National University, Korea M. Siemann German Aerospace Center, Germany IFASD‐2015‐098 Sensitivity Based Approach for Improved Predictions of Servo‐elastic Response of a Flexible Aircraft Ashok Joshi, Prabha Srinivasan IIT Bombay, India Indira Narayanaswamy and Hemalatha E ADA, Rameshnagar, Bengaluru, India IFASD‐2015‐136 Experimental and numerical study of an autonomous flap Lars O. Bernhammer1, Sachin T. Navalkar2, Jurij Sodja1, Moti Karpel2, Roeland De Breuker1 1 Delft University of Technology, The Netherlands 2 Technion, Haifa, Israel IFASD‐2015‐020 A generalised beam formulation for the dynamic analysis of camber‐morphing helicopter blades Luca Cirrottola, Marco Morandini, Giuseppe Quaranta Politecnico di Milano, Italy IFASD‐2015‐190 IFASD‐2015‐118 Time‐resolved PIV measurements of a Analysis of the conditions of dynamic hybrid morphing NACA4412 airfoil loading a helicopter skid landing gear when the landing and ditching in autorotation Johannes Schellera,b, Karl‐Joseph Rizzoa, main rotor Gurvan Jodina,b, Eric Duhayona, Jean‐Francois D.V. Nedel’ko, S.A. Alimov Rouchona, Gilles Harranb, Marianna Brazab J.S.C. «Kazan Helicopters Plant», Russia (a) LAPLACE, Toulouse, France L.G.Gontsova ‐ TsAGI, Russia (b) IMFT, Toulouse, France IFASD‐2015‐069 Certification of Landing Gear Structure under UERF Event Esteban Gómez Viñas, José M. Chorro Martínez, Angel Martínez Pérez, Jose M. Pérez Hernandez, Jorge Pérez San‐Jose Airbus Defence & Space, Spain IFASD‐2015‐149 Aeroelastic analysis of a regional aircraft with active camber morphing wings Alessandro De Gaspari, Sergio Ricci and Lorenzo Travaglini Politenico di Milano, Italy Session 25 Structural Dynamics & Shimmy IFASD‐2015‐073 The influence of local nonlinearities on landing gear wheel shimmy of an airplane S. Paryshev, A. Krapivko TsAGI, Russia IFASD‐2015‐125 Nonlinear Reduced Order Modelling of Nonlinear Aircraft Structures G. Gai , S. Timmey and K. J. Badcockz University of Liverpool, UK IFASD‐2015‐083 Study of shimmy in industrial context Ludovic MARTIN, Vincent JACQUES, Eric GARRIGUES Dassault Aviation, France IFASD‐2015‐152 Surrogate Reduced‐Order Modeling of Structural Dynamic Systems Undergoing Parameter Variations Taehyoun Kim National University of Singapore IFASD‐2015‐114 Main Landing Gear Door dynamic loads due to unsteady aerodynamics: a predictive and validated methodology R. Abarca, D. Arenillas, O. Castro, B.Masia, E.Menga Airbus Operations SL, Getafe, Spain M.Barth Airbus Operations SAS, Toulouse, France IFASD‐2015‐208 Parametric Reduced Order Model Approach for Worst Case Dynamic Loads Prediction Michele Castellani, Yves Lemmens, Siemens Industry Software NV, Belgium. Jonathan Cooper, University of Bristol, UK IFASD‐2015‐155 Nonlinear dynamic analysis of assembled aircraft structures with concentrated nonlinearities E.Menga EGLRG‐AIRBUS Operations, Getafe, Spain S.Hernandez, S.Moledo, C.Lopez University of Coruna, Spain IFASD‐2015‐150 IFASD‐2015‐141 IFASD‐2015‐198 IFASD‐2015‐160 IFASD‐2015‐165 Suppression of Self‐Excited Oscillation Using Composite fan blade bird strike analysis Turbulent flow around a flat plate deformed A Reduced Order Model of a free elastic Aerial Delivery Dynamic Loads Smart Material on Flexible Wing Structure using experimental and numerical methods by shape memory alloys aircraft for dynamic loads prediction A. Pérez de la Serna, A. J. Rodríguez Jiménez Norizham A. Razak, Nazreen Shah Nasip including aerodynamic nonlinearities Karimbayev Telman, Chernyshov Artyom, Altran, Madrid, Spain Y. HOARAUa, T. DELOZEb, E. DERIb, M. Oliver and H. Climent Universiti Sains Malaysia Afanasyev Dmitry, Yezhov Alexey J.SCHELLERc, J.F. ROUCHONc AND M. BRAZAb David Quero Martín, Wolf Reiner Krüger, DLR, G. Dimitriadis Guillermo Jenaro Rabadán, Airbus Airbus Defence and Space. Military Transport CIAM, Russia a ICUBE, Strasbourg, France Aircraft. Getafe, Spain University of Liege, Belgium. Operations, Germany b IMFT, Toulouse, France c LAPLACE, Toulouse, France ifasd_2015_preliminary_programme_2015_05_07 Page 10 Coffee break 16:00‐16:30 Ball Room Keynote lecture 4 Aeroelasticity and MDO: A USAF Perspective Dr. Raymond Koloney, USAF, AFRL/RQVC, USA 16:30‐17:15 Closing and Announcement of IFASD2017 17:15‐17:30 List of poster presentations IFASD-2015-002 IFASD-2015-003 IFASD-2015-006 IFASD-2015-033 IFASD-2015-058 IFASD-2015-059 IFASD-2015-063 IFASD-2015-064 IFASD-2015-067 IFASD-2015-076 IFASD-2015-099 IFASD-2015-113 IFASD-2015-120 IFASD-2015-126 IFASD-2015-127 IFASD-2015-128 IFASD-2015-135 IFASD-2015-138 IFASD-2015-146 IFASD-2015-170 IFASD-2015-187 IFASD-2015-191 IFASD-2015-200 IFASD-2015-201 A High‐efficiency Aeroelastic Optimization Method Based on Kriging Model and Genetic Algorithm, Wang Xiaozhe , BUAA, China Nonlinear Aeroelastic Scaling for an Airfoil Based on Unsteady Vortex Lattice Model, Du Ziliang , Beihang University, China Static aeroelastic analysis of a wing including geometric nonlinearities based on ROM, An Chao, Xie Changchuan, Liu Yi, Yang Chao , Beihang University, Beijing, P.R.China Method for Measuring Structural Deformation Based on Distributed Fiber Optic Instruments, Yang Meng , Beihang University, China Study on transfer characteristics of engine vibration isolation system impacted with rotating excitation, Erdun Su, Wenchao Huang, Yonghui Chen, Yu You , ASRI of China, Xi’an Influence of the structural elasticity on the static and dynamic effectiveness of control surfaces with geared tab, O.Zubakova, M.Zichenkov, F.Ishmuratov, Yu.Nayko TsAGI, A.Khalo , Ilyushin Aviation Complex, Russia Aeroelastic Analysis of Composite Missile Folding Fins, B.Rasuo, M.Dinulovic, University of Belgrade, Serbia, B.Krstic, P.Andric , University of Defence, Belgrade, Serbia Aeroelastic Trim and Static Stability Analysis of Highly Flexible Aircraft, Hu Rui, Xie Changchuan, Liu Yi , Beihang University, Beijing, China Correlation between Stiffness Distribution and Aeroelastic Characteristics of High‐aspect‐ratio Wings, Ziliang Du, Zhiqiang Wan, Beihang University, Beijing, China Geometrical nonlinear aeroelastic analysis of large aircraft wing, Zhang Chao, Xie Changchuan, Liu Yi, He Jingwu , Beihang University, Beijing, China Experimental Methods of Studying Dynamic Characteristics of Airplane Landing Gears, A.V. Krapivko, V.N. Zadonskaya, E.S. Kolyshev, TsAGI, Russia Experimental investigation of control surfaces of unmanned aerial vehicles, S. Gartsev, A. Dolgopolov, V. Smyslov , TsAGI, Russia Hypersonic aerothermoelastic response simulation using CFD/CSD approach, Zhi Chen, Jinan Lv, Bangcheng Ai, Jijun Yu , CAAA, Beijing, China Nonlinear gust response analysis and wind tunnel test for high‐aspect ratio wing, Liu Yi, Xie Changchuan, Yang Chao, Beihang University, Beijing, China Aeroelastic optimization design for high‐aspect ratio wing under large deformation, Wang Fei, Xie Changchuan , Beihang University, Beijing, China A Static Aerothermoelastic Response Analysis Method Considering Heat Flux Uncertainty, Yi Nan, Zhiqiang Wan , Beihang University, Beijing, China Speciality of a Variable Loads on an Airplane and Vibration Suppression Ability, K.A. Mitenkov, T.I. Orlova, V.I. Tsimbalyuk , TsAGI, Russia Application of imposed motion method for model flutter tests in high‐speed wind tunnels, Boris D. Bryantsev , TsAGI, Russia CFD/CSD approach to evaluate the aeroelastic response of a hypersonic vehicle wing, Jinan Lv, Zhanjun Chen, Yingyu Hou, Ziqiang Liu , CAAA, Beijing, China Development of an UAV with a Variable‐Span Morphing Wing, Jae‐Sung Bae, Jong‐Hwan Kim , Korea Aerospace Engineering, Goyang‐city, Korea On the influence of aircraft engine components damage caused by foreign objects ingestion on the aeroelastic characteristics of compressors, Victor Matsarenko, Boris Shorr, Galina Melnikova , CIAM, Russia Flight Dynamic Modelling and Numerical Simulation of a Generic Ornithopter with Pitching and Flapping Phase Lag, Harijono Djojodihardjo , Universiti Putra Malaysia Development of Flight Parameters Simulation Technology for an Aircraft with Complex Control System on Flight Simulators for More Precise Definition of In‐Service Loads to Effectively Solve the Strength Structural and Life Problems, G.I. Turchannikov , TsAGI, Russia Experience of Research on Aeroelastic Stability of Single and Closely Spaced Long Bridges in Russian Federation, K.Strelkov, M.Komarov, A.Bykovsky, A.Kozichev, B.Logunov, L.Teperin , TsAGI, Russia ifasd_2015_preliminary_programme_2015_05_07 Page 11
