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Uncertainty and global sensitivity analysis of hypersonic control surface aerothermoelastic
Kun Ye,
Zhengyin Ye
, Zhan Qu, Xiaojin Wu,
Weiwei Zhang
航空学院
Northwestern Polytechnical University Xian
科研成果
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Physics
Control Surface
100%
Hypersonics
100%
Temperature Distribution
75%
Flutter Analysis
50%
Resonant Frequency
50%
Monte Carlo Method
50%
Numerical Integration
50%
Aerothermodynamics
50%
Charge Flow Device
25%
Computational Fluid Dynamics
25%
Aerodynamics
25%
Aeroelasticity
25%
Piston Theory
25%
Thermal Stress
25%
Engineering
Control Surface
100%
Temperature Distribution
75%
Simulation Method
50%
Resonant Frequency
50%
Coefficient of Variation
50%
Integration Method
50%
Numerical Integration
50%
Aerothermodynamics
50%
Aerodynamics
25%
Parameter Uncertainty
25%
Computational Fluid Dynamics
25%
Thermal Stress
25%
Aeroelasticity
25%
Model Uncertainty
25%
Parameterized Model
25%