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
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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
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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
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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
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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
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