Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Author Manuscripts
Chao Yang
102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
32 Stall flutter suppression with active camber morphing based on reinforcement learning
87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles
45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
156 Measurement and Control System Design for Propeller-Wing System Experiments
64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Zhichun Yang
210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
Zhuolin Ying
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
Tomohiro Yokozeki
85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization
Jie Yu
136 The Design and Analysis of Tensegrity Morphing Wing
Fanglin Yu
Technical University of Munich
10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
99 Flexible aircraft conceptual co-design based on the RCE framework
Changkun Yu
102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
Kaihua Yuan
Institute of Beijing Mechanics and Electronics
5 The simulation and flight verification of active aeroelastic control

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