Authors Index

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Author	Manuscripts
Christian Wallace DLR (German Aerospace Center)	163 Lidar-based gust load alleviation – increasing the load reduction potential through a two-degree-of-freedom controller architecture
Zhiqiang Wan	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Gaozhan Wang Beihang University	92 Hypersonic flutter analysis based on three-dimensional local piston theory
Wei Wang	156 Measurement and Control System Design for Propeller-Wing System Experiments
Xuerui Wang Delft University of Technology	181 Nonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System 183 Nonlinear analysis of combined rate and acceleration limits effect on actuator performance 164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
Xiaozhe Wang	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Peihan Wang Beihang University	45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
Guido Weber Liebherr-Aerospace Lindenberg	109 Decentralized Control of Ailerons for Gust Load Alleviation
Zsombor Wermeser	196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law
Michelle Westin Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Viresh Wickramasinghe NRC	73 Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
Hannes Wilke Technische Universität Berlin	195 On the preparation of a flexible real-time aircraft model for a flight simulator
Thomas Wilson Airbus Operations Ltd.	96 Parametric nonlinear flutter analysis of the semi-aeroelastic hinges during manoeuvres and gust encounters 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Kristoffer Wingstedt SAAB	218 Adaptive Euler - efficient and predictive aerodynamics: validation and prototype development toward aeroelasticity
Benjamin King Sutton Woods University of Bristol	166 Analysis of inertial gust load relief characteristics of high aspect ratio wings
Zhigang Wu Beihang University	102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test 45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
Matthias Wuestenhagen DLR - Institute of System Dynamics and Control	99 Flexible aircraft conceptual co-design based on the RCE framework
Matthias Wüstenhagen	103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]