| 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
DLR German Aerospace Center
|
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
49 Research shake test on an Airbus helicopter technology demonstrator
|
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 German Aerospace Center
|
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
49 Research shake test on an Airbus helicopter technology demonstrator
|
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
|
Huub Timmermans
Netherlands Aerospace Centre
|
230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
|
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
|