Numerical Simulation of the Aerodynamic Influence of Aircrafts During Aerial Refueling with Engine Jet

Engineering

• Aerodynamic Characteristic 50%
• Aerodynamics 100%
• Angle-of-Attack 50%
• Downwash 50%
• Dynamic Pressure 50%
• Fighter Aircraft 50%
• Flow Distribution 50%
• Jet Engine 100%
• Lift Coefficient 50%
• Pitching Moment 50%
• Pitching Moment Coefficient 50%
• Pressure Difference 50%
• Rolling Moment 50%