Reduced-order modeling for aeroelastic systems via nonlinear state-space identification

被引：0
|
作者：
Zhang, Jiaming [1 ]
Yang, Zhijun [1 ]
Huang, Rui [1 ]
机构：
[1] State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics | 2020年 / 52卷 / 01期
关键词：
Numerical methods - Transonic flow - Elastic waves - Neural networks - State space methods - Computational complexity - Flutter (aerodynamics) - Impulse response - Supersonic aircraft - Fluid structure interaction - Computational fluid dynamics - Forecasting - Convolution - Transonic aerodynamics;
D O I：
10.6052/0459-1879-19-287
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：150 / 161
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