Nonlinear Aerodynamic Reduced-Order Model for Limit-Cycle Oscillation and Flutter

Authors :: Jiaqing Kou
Ziyi Wang
Weiwei Zhang
Source :: AIAA Journal. 54:3304-3311
Publication Year :: 2016
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2016.

Subjects :: 020301 aerospace & aeronautics
Lift coefficient
Computer science
Aerospace Engineering
Particle swarm optimization
02 engineering and technology
Aerodynamics
Mechanics
01 natural sciences
010305 fluids & plasmas
Aerodynamic force
Nonlinear system
0203 mechanical engineering
0103 physical sciences
Fluid–structure interaction
Flutter
Feedforward neural network

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