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西北工业大学 国内
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The effect of structural geometric nonlinearities on the flutter of the straight and swept wing configurations
Guo Qing,
Song Bifeng
航空学院
Northwestern Polytechnical University Xian
科研成果
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探究 'The effect of structural geometric nonlinearities on the flutter of the straight and swept wing configurations' 的科研主题。它们共同构成独一无二的指纹。
分类
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Engineering
Swept Wings
100%
Geometric Nonlinearity
100%
High Aspect Ratio
50%
Unmanned Aerial Vehicle
25%
Large Deformation
25%
Engineering Application
25%
Computational Fluid Dynamics
25%
Nonlinearity
25%
Aerodynamic Force
25%
Flutter Speed
25%
Aeroelasticity
25%
Sweep Angle
25%
Flexible Wings
25%
Stronger Effect
25%
Vehicle Design
25%