Authors Index

[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]

Author	Manuscripts
Ni Zao	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
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
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
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
Jian Zhang	39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Zou Zhicheng	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
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
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
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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