唇口几何参数对短舱进气道性能影响数值研究

Engineering

• Numerical Study 100%
• Geometric Parameter 100%
• Computational Fluid Dynamics 50%
• Flow Distribution 50%
• Leading Edge 50%
• Greater Effect 50%
• Flow Characteristic 50%
• Air Flow 50%
• Design Parameter 50%
• Aspect Ratio 50%
• Aerodynamic Performance 50%
• Turbofan Engine 50%
• Initial Pressure 50%
• Pressure Loss 50%
• Pressure Recovery Coefficient 50%
• Performance Parameter 50%
• Friction Loss 50%