Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Wei Xiao
102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
Changchuan Xie
93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory
92 Hypersonic flutter analysis based on three-dimensional local piston theory
94 IMU-based deformation reconstruction for highly flexible wings
83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
41 Aerodynamic analysis of aircraft wings using a coupled PM-BL approach
27 Nonlinear aeroelastic analysis of large wind turbine blades
11 Wind tunnel test of gust response for distributed propeller-wing system
156 Measurement and Control System Design for Propeller-Wing System Experiments
Italo Ximenes
Aeronautics Institute of Technology - ITA
70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
Pu Xing
240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
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