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Room 1.1
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Room 1.2
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Room 1.4/1.5
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Room 1.3
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Room 1.6
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08:30
Fleet Transition with an Aeroelasticity & Structural dynamics perspective - Kees Wijnberg
Chair: Jurij Sodja
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09:30
Short Break
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09:40
Aeroservoelasticity 2
Chair: Cedric Liauzun
09:40
30 mins
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Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
Fanglin Yu, Milán Barczi, Carlos Sebastia Saez, Béla Takarics, Yasser Meddaikar, Mirko Hornung
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10:10
30 mins
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Automated Tuning of a Baseline Flight Control System with Maneuver Load Alleviation for an Energy-Efficient Passenger Airplane
Till Strothteicher, Nicolas Fezans
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09:40
Distributed propulsion 2
Chair: Vincenzo Vaccaro
09:40
30 mins
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Aeroelastic analysis of distributed electric propulsion flexible wings
Samet Dede, Ali Tatar, Djamel Rezgui, Jonathan Cooper
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10:10
30 mins
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Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring
Mohammadreza Amoozgar, Grigorios Dimitriadis, Jonathan Cooper, Rafic Ajaj
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09:40
Loads 1
Chair: Felix Arevalo
09:40
30 mins
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Differentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators
Alvaro Cea, Rafael Palacios
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10:10
30 mins
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Comparative analysis of flight maneuver loads between flexible and rigid aircraft
Eduardo de Melo Pinto, Flávio Cardoso-Ribeiro, Fernando de Oliveira Moreira
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09:40
No session
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09:40
Reduced-order modelling
Chair: Lorenz Tichy
09:40
30 mins
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Machine learning-based parametric model order reduction for the gust load analysis
Sangmin Lee, SiHun Lee, Younggeun Park, Seung-Hoon Kang, Kijoo Jang, Haeseong Cho, SangJoon Shin
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10:10
30 mins
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Model order reduction for nonlinear aeroelastic dynamical system using automatic differentiation
Declan Clifford, Andrea Da Ronch
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10:40
Break
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11:00
Data driven methods 2
Chair: Cedric Liauzun
11:00
30 mins
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Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Vitor Borges Santos, Breno Soares da Costa Vieira, Flávio Luiz Cardoso-Ribeiro, Antônio Bernardo Guimarães Neto
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11:30
30 mins
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Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Nicolò Laureti, Luca Pustina, Marco Pizzoli, Francesco Saltari, Franco Mastroddi
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12:00
30 mins
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Machine learning to forecast unsteady, motion-induced unsteady forces
Reik Thormann, Hans Martin Bleecke
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11:00
Nonlinear control
Chair: Vincenzo Vaccaro
11:00
30 mins
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Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
Peihan Wang, Zhigang Wu, Chao Yang
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11:30
30 mins
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Nonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System
Tingyu Zhang, Xuerui Wang
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12:00
30 mins
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Nonlinear analysis of combined rate and acceleration limits effect on actuator performance
Luca Marino, Xuerui Wang, Jurij Sodja
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11:00
Gust 4
Chair: Felix Arevalo
11:00
30 mins
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Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Christoph Kaiser, David Quero, Jens Nitzsche, Bernd Stickan
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11:30
30 mins
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Effect of flow separation on discrete gust loads for a free-flying elastic aircraft
Johan Moritz Feldwisch
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12:00
30 mins
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Analysis of inertial gust load relief characteristics of high aspect ratio wings
Sanuja Jayatilake, Mark Lowenberg, Benjamin King Sutton Woods, Branislav Titurus
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11:00
No session
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11:00
Low/high order methods 2
Chair: Lorenz Tichy
11:00
30 mins
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Gust response analysis of supersonic aircraft based on three-dimensional piston theory
Chen Song, Changchuan Xie, Chenyu Liu, Yang Meng
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11:30
30 mins
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Development of a nonlinear FSI method for simulation of airfoil flutter with and without impact absorbers
Michael Pitzal, Johann Groß, Patrick Kopper, Andrea Beck, Malte Krack
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12:00
30 mins
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Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Zou Zhicheng, Xie Changchuan, An Chao, Yang Lan, Zhu Lipeng, Ni Zao
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12:30
Lunch
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13:30
Flutter testing
Chair: Holger Mai
13:30
30 mins
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Flight flutter test modal identification by using nature inspired algorithms: A classical mathematical modeling
Demian Gomes da Silva, Guilherme Castrignano Tavares
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14:00
30 mins
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Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Julius Bartasevicius, Daniel Teubl, Thomas Seren, Fanglin Yu, Mirko Hornung, Balint Vanek, Daniel Balogh, Szabolcs Toth, Mihaly Nagy, Balazs Fritsch, Keith Soal, Thiemo Kier, Özge Süelözgen
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14:30
30 mins
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Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Keith Soal, Jan Schwochow, Robin Volkmar, Martin TANG, Carsten Thiem, Yves Govers, Marc Böswald, Thiemo Kier, Özge Süelözgen, Nicolas Guerin, Daniel Teubl, Julius Bartasevicius, Balint Vanek, Szabolcs Toth, Misi Nagy
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15:00
30 mins
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Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Hao Wei, Elijah Ang, Jieli, Daryl Leo, Jun Kang Tan, Chien Ming, Jonathan Tay, Yongdong Cui, Bing Feng Ng
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13:30
Aeroelastic optimisation 3
Chair: Héctor Climent
13:30
30 mins
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Aeroelastic reliability based optimisation of composite plates via surrogate modeling
Roger Ballester Claret, Nicolo Fabbiane, Christian Fagiano, Cédric Julien, Didier Lucor
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14:00
30 mins
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Unified model of sandwich panel core and faces for aeroelastic optimization
Vladimír Hostinský, Jurij Sodja, Ivo Jebáček, Jan Navrátil
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14:30
30 mins
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A Panel-Free Aeroelastic Solver with Adjoint Sensitivities
Hollis Smith, Joshua Deaton
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15:00
30 mins
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Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Oleh Havaza, Vitalii Sukhov, Ruslan Nikitin
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13:30
Loads 2
Chair: Mohammadreza Amoozgar
13:30
30 mins
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Influence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport Configuration
Vega Handojo, Sunpeth Cumnuantip
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14:00
30 mins
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Robust design through identification of main components from multivariate random loads
Cyrille Vidy, Carlo Aquilini
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14:30
30 mins
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Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Leif Rieck, Benjamin Herrmann, Frank Thielecke
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15:00
30 mins
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Lidar-based gust load alleviation – increasing the load reduction potential through a two-degree-of-freedom controller architecture
Christian Wallace, Nicolas Fezans
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13:30
No session
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13:30
Aeroelastic testing 5
Chair: Jack Hagelin
13:30
30 mins
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Experimental investigation of a highly flexible wing
Giuliano Coppotelli, Roberto Sbarra, Ludovic Onofri, Marcello Righi
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14:00
30 mins
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Flight shape determination of the highly flexible up wing wind tunnel model using high and low fidelity aerodynamic methods in conjunction with nonlinear structural methods
Jos Aalbers, Peter Blom, Huub Timmermans
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14:30
30 mins
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Design and experimental tests of a flexible wing of high-aspect ratio for investigating flutter mechanisms
Cyrille Stephan, Xavier Amandolese
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15:00
30 mins
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Experimental Comparison of Real-Time Shape Estimation Methods on Very Flexible Wings
Francisco P. Reis, Bilal Sharqi, Leandro Lustosa, Charles Poussot-Vassal, Carlos E. S. Cesnik
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15:30
Break
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16:00
Data-driven testing
Chair: Holger Mai
16:00
30 mins
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Aircraft vibration from React to Predict
Hoang Thien Phu VO, Völker Johannes
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16:30
30 mins
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A Calibration Method for Camera-Aided Inertial Estimation of Wing Shape
Leandro Lustosa
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17:00
30 mins
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Estimation of slender body elastic rates and accelerations using a combination of measured data
Ilya Genkin, Daniella E. Raveh
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17:30
30 mins
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Prediction of Limit Cycle Oscillations Based on Dynamic Eigen Decomposition of Flight Test Data
TAEHYOUN KIM
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16:00
Gust 5
Chair: Héctor Climent
16:00
30 mins
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Design of a High Aspect Ratio Windtunnel Model for Transonic Gust Load Alleviation
Huub Timmermans, Andres Jurisson, Wolf Krueger, Johannes Dillinger, Kees Kapeteijn, Felix Stalla
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16:30
30 mins
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Gust load alleviation wind tunnel tests of a folding wing tip configuration
Luca Marchetti, Sergio Ricci, Luca Riccobene, Donato Grassi, Paolo Mantegazza, Stephan Adden, Huaiyuan Gu, Jonathan Cooper
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17:00
30 mins
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Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Arnaud Lepage, Nicola Paletta, Serena Russo, Sergio Ricci, Eric Rantet, Arnaud Barnique
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17:30
30 mins
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Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
Vincent Bouillaut, Alex Dos Reis De Souza, Pierre Vuillemin, Charles Poussot-Vassal, Arnaud Lepage
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16:00
Flutter control
Chair: Mohammadreza Amoozgar
16:00
30 mins
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Control design for active flutter suppression flight testing
Bálint Patartics, Béla Takarics, Bálint Vanek, Ramesh Konatala, Matthias Wüstenhagen, Özge Süleözgen, Manuel Pusch, Thiemo Kier
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16:30
30 mins
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Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics
Boris Micheli, Jens Neumann, Jürgen Arnold
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17:00
30 mins
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Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
Thiemo Kier, Matthias Wüstenhagen, Özge Süelözgen, Ramesh Konatala, Yasser Meddaikar, Keith Soal, Nicolas Guerin, Julius Bartasevicius, Bela Takarics, Daniel Balogh, Balint Vanek
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17:30
30 mins
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Aeroelastic aircraft design and flight control methods applicable for flutter suppression: The flipased perspective
Balint Vanek, Virag Bodor, Bela Takarics, Thiemo Kier, Keith Soal, Charles Poussot-Vassal, Nicolas Guerin, Mirko Hornung, Christian Roessler
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16:00
No session
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16:00
Ground vibration testing
Chair: Jack Hagelin
16:00
30 mins
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Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Nicolas Guérin, Keith Soal, Cyrille Stephan, Martin Tang, Pascal Lubrina, Robin Volkmar, Yves Govers, Julius Bartasevicius, Daniel Teubl, Szabolcs Toth, Thiemo Kier, Balint Vanek
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16:30
30 mins
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Explainable nonlinear state-space modelling: analysing the GVT of a battery-operated aircraft
Péter Zoltán Csurcsia, Tim De Troyer
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17:00
30 mins
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Ground Vibration Testing and Model Update of a Transonic Flutter Wind Tunnel Model
Anders Ellmo
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17:30
30 mins
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Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
Wei Xiao, Changkun Yu, Zhigang Wu, Chao Yang
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18:00
Closure & drinks
Chair: Bart Eussen
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