Author |
Manuscripts |
Jérôme BAZILE
AIRBUS
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8 Wind Law Proposal for Aircraft Control in Turbulence
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Davide Balatti
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33 Aeroelastic hybrid testing for industrial applications
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Roger Ballester Claret
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17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
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ignacio Ballesteros Ruiz
Airbus UK
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26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
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Daniel Balogh
SZTAKI
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116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
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Guilherme C. Barbosa
TU-Berlin
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58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
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Milán Barczi
SZTAKI, Budapest, Kende u. 13-17, 1111, Hungary
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10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
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Arnaud Barnique
Cedrat Technologies
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231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
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Leonardo Barros da Luz
Instituto Tecnológico de Aeronáutica
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118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures
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Julius Bartasevicius
TU Munich
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116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
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
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Martin Bauer
German Aerospace Center DLR, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, 38108, Braunschweig Germany
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205 High-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR
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Antônio Bernardo Guimarães Neto
Instituto Tecnológico de Aeronáutica
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132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
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Ying Bi
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38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities
37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play
39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
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Anna Biancotto
Royal Netherlands Aerospace Centre
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101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip
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Laurent Blanc
LTDS
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150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
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Hans Bleecke
Airbus Operations
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50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
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Hans Martin Bleecke
Airbus Operations
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30 Machine learning to forecast unsteady, motion-induced unsteady forces
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Brianna Blocher
The University of Texas at Austin
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185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
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Christophe Blondeau
ONERA
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162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
34 A modular TSM solver for aeroelastic analysis and optimizations
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Bernd Boche
Technische Universität Berlin
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195 On the preparation of a flexible real-time aircraft model for a flight simulator
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Stefan de Boer
TU Delft
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57 Continuous parametrisation of wing movable layout for design optimisation
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Vitor Borges Santos
Instituto Tecnológico de Aeronáutica
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132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
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Vincent Bouillaut
DAAA, ONERA, Institut Polytechnique de Paris, 92320 Chatillon, France
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157 Aeroelastic design of a drone for research on active flutter control
227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
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Carsten Braun
FH Aachen University of Applied Sciences
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89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
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Marc Braune
German Aerospace Center (DLR) - Institute of Aeroelasticity
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200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing
202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB
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Roeland De Breuker
Delft University of Technology
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142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
57 Continuous parametrisation of wing movable layout for design optimisation
207 Application of aeroelastic tailoring for control surface reversal
164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
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Roeland de Breuker
Delft University of Technology
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198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
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Elsa Bréus
Dassault Aviation
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165 T-tail transonic flutter wind tunnel test part 1: Sealing system design and model testing
104 Flutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up
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Gabriel Buendia
Airbus Defence
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171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
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Thomas Buete
German Aerospace Center
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200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing
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Heiko Böhlken
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202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
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Nils Böhnisch
FH Aachen University of Applied Sciences
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89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
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Marc Böswald
DLR - German Aerospace Center
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113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter
114 An Incremental Modal Shape Sensing Method for Geometrically Non-Linear Deformed Wings
77 A Procedure for Flutter Analysis with Nonlinear Experimental Modal Parameters
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
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Thomas Büte
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202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
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