Authors Index

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Author	Manuscripts
Jérôme BAZILE AIRBUS	8 Wind Law Proposal for Aircraft Control in Turbulence
Davide Balatti	33 Aeroelastic hybrid testing for industrial applications
Roger Ballester Claret	17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
ignacio Ballesteros Ruiz Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Daniel Balogh SZTAKI	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
Guilherme C. Barbosa TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Milán Barczi SZTAKI, Budapest, Kende u. 13-17, 1111, Hungary	10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
Arnaud Barnique Cedrat Technologies	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Leonardo Barros da Luz Instituto Tecnológico de Aeronáutica	118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures
Julius Bartasevicius TU Munich	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
Martin Bauer German Aerospace Center DLR, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, 38108, Braunschweig Germany	205 High-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR
Antônio Bernardo Guimarães Neto Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Ying Bi	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
Anna Biancotto Royal Netherlands Aerospace Centre	101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip
Laurent Blanc LTDS	150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Hans Bleecke Airbus Operations	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
Hans Martin Bleecke Airbus Operations	30 Machine learning to forecast unsteady, motion-induced unsteady forces
Brianna Blocher The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
Peter Blom Netherlands Aerospace Centre	230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
Christophe Blondeau ONERA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA 34 A modular TSM solver for aeroelastic analysis and optimizations
Bernd Boche Technische Universität Berlin	195 On the preparation of a flexible real-time aircraft model for a flight simulator
Stefan de Boer TU Delft	57 Continuous parametrisation of wing movable layout for design optimisation
Vitor Borges Santos Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Vincent Bouillaut DAAA, ONERA, Institut Polytechnique de Paris, 92320 Chatillon, France	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
Carsten Braun FH Aachen University of Applied Sciences	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Marc Braune German Aerospace Center (DLR) - Institute of Aeroelasticity	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
Roeland de Breuker Delft University of Technology	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
Roeland De Breuker Delft University of Technology	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
Elsa Bréus Dassault Aviation	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
Ralf Buchbach DLR German Aerospace Center	49 Research shake test on an Airbus helicopter technology demonstrator
Gabriel Buendia Airbus Defence	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Thomas Buete German Aerospace Center	200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing
Heiko Böhlken	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Nils Böhnisch FH Aachen University of Applied Sciences	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Marc Böswald DLR German Aerospace Center	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 49 Research shake test on an Airbus helicopter technology demonstrator
Thomas Büte	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil

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