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Aeroelastic Model of Reduced-Order for a Slender Missile
Zhijun Yang, Rui Huang, Haojie Liu, Yonghui Zhao,
Haiyan Hu
, Le Wang
Nanjing University of Aeronautics and Astronautics
China Aerospace Science and Technology Corporation
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Engineering
Aerodynamic Load
100%
Computer Simulation
50%
Recursive
50%
Computational Fluid Dynamics
50%
Mach Number
25%
Finite Element Modeling
25%
Frequency Response
25%
Aerodynamic Model
25%
Accurate Prediction
25%
Levenberg-Marquardt Algorithm
25%
Flight Condition
25%
Airfoil
25%
Reduced Order Model
25%
Breakthrough
25%
Design Phase
25%
Model Airplane
25%