Numerical simulation about the effect of initial separation condition on safety of aerial bomb separated from an aircraft

Engineering

• Computer Simulation 100%
• Initial Separation 100%
• Mach Number 66%
• Angle-of-Attack 66%
• Angular Velocity ω 66%
• Flight Altitude 66%
• Aerodynamic Characteristic 33%
• Simulation Method 33%
• Computational Fluid Dynamics 33%
• Great Influence 33%
• Attack Angle 33%
• Aerodynamic Interference 33%