Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Authors Index

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Author Manuscripts
Martin TANG
DLR
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Bela Takarics
SZTAKI
103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
Béla Takarics
HUN-REN Institute for Computer Science and Control
10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law
99 Flexible aircraft conceptual co-design based on the RCE framework
Jun Kang Tan
108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Martin Tang
German Aerospace Center (DLR), Institute of Aeroelasticity
77 A Procedure for Flutter Analysis with Nonlinear Experimental Modal Parameters
190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Ali Tatar
Istanbul Technical University
129 Aeroelastic analysis of distributed electric propulsion flexible wings
80 Aeroelastic optimisation of a cantilevered plate with local damping application
Chien Ming, Jonathan Tay
108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Robert Taylor
University of Texas Arlington
13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Daniel Teubl
TU Munich
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Andrew Thelen
NASA Langley Research Center
69 Gradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints
Frank Thielecke
Hamburg University of Technology
46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Carsten Thiem
DLR
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Reik Thormann
Airbus Operations
30 Machine learning to forecast unsteady, motion-induced unsteady forces
Fabrice Thouverez
LTDS
150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Xinhai Tian
210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
Branislav Titurus
School of Civil, Aerospace and Design Engineering, University of Bristol
166 Analysis of inertial gust load relief characteristics of high aspect ratio wings
208 Experimental investigation into the dynamic characteristics of a tilting multirotor system
Francesco Toffol
Politecnico di Milano
167 Passive and active load alleviation technologies for UHARW wings
MIguel Torralba
Airbus Defence and Space
171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Szabolcs Toth
SZTAKI
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Natsuki Tsushima
Japan Aerospace Exploration Agency
85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization
200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing

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