跨速域大后掠角近距耦合翼气动干扰特性

Engineering

• Computer Simulation 100%
• Aerodynamic Interference 100%
• Vortex 66%
• Mach Number 66%
• Flow Field 66%
• Angle-of-Attack 66%
• Drag Coefficient 66%
• Lift Coefficient 66%
• Numerical Methods 33%
• Pressure Difference 33%
• Navier-Stokes Equation 33%
• Finite Volume Method 33%
• Flow Structure 33%
• Flow Condition 33%
• Reynolds-Averaged Navier-Stokes 33%
• Aerodynamic Coefficient 33%
• Pressure Coefficient 33%
• Transonic Flow 33%
• Subsonic Flow 33%
• Front Wing 33%