Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Ni Zao
68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Yuhui Zhang
94 IMU-based deformation reconstruction for highly flexible wings
83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Zhitao Zhang
11 Wind tunnel test of gust response for distributed propeller-wing system
156 Measurement and Control System Design for Propeller-Wing System Experiments
Jian Zhang
39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Tingyu Zhang
TUDelft
181 Nonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System
Duoyao Zhang
83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Zou Zhicheng
68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Chen Zhu
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
Zijian Zhu
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
Lipeng Zhu
41 Aerodynamic analysis of aircraft wings using a coupled PM-BL approach
Markus Zimmer
German Aerospace Center (DLR)
90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
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