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西北工业大学 国内
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Error analysis of lateral jet interaction flow field of supersonic vehicle with traditional numerical method
Lei Yang,
Zheng Yin Ye
航空学院
Northwestern Polytechnical University Xian
科研成果
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探究 'Error analysis of lateral jet interaction flow field of supersonic vehicle with traditional numerical method' 的科研主题。它们共同构成独一无二的指纹。
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Physics
Boundary Condition
100%
Charge Flow Device
14%
Computational Fluid Dynamics
14%
Cross Flow
14%
Error Analysis
100%
Flow Distribution
100%
Jet Flow
14%
Mathematical Method
100%
Pitching Moment
14%
Shock Wave
14%
Supersonics
100%
Turbulence Model
14%
Engineering
Boundary Condition
100%
Computational Fluid Dynamics
14%
Experimental Result
14%
Flow Distribution
100%
Good Agreement
14%
Interaction Force
14%
Jet Interaction
100%
Normal Force
14%
Nozzle Exit
14%
Numerical Method
100%
Pitching Moment
14%
Pressure Ratio
14%
Spatial Discretization
14%
Static Thrust
14%
Vortex
14%