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西北工业大学 国内
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Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model
Liuqing Ye,
Zhengyin Ye
, Kun Ye, Jie Wu
航空学院
Northwestern Polytechnical University Xian
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Engineering
Aerodynamics
100%
Dynamic Pressure
100%
Oblique Shock
100%
Stability Analysis
100%
Analytical Model
100%
Static Pressure
100%
Dimensionless
75%
Differential Pressure
50%
Nonlinearity
25%
Pressure Difference
25%
Superposition
25%
Plate Theory
25%
Deep Understanding
25%
Indirect Method
25%
Stability Boundary
25%