Numerical investigation of vented plume into a supersonic flow in the early stage of rocket hot separation

Engineering

• Angle-of-Attack 100%
• Combined Parameter 20%
• Early Stage 100%
• Flight Altitude 60%
• Flow Condition 20%
• Flow Distribution 40%
• Free-Stream Mach Number 40%
• Illustrates 20%
• Jet Interaction 20%
• Mach Number 20%
• Navier-Stokes Equation 20%
• Peak Pressure 40%
• Reynolds-Averaged Navier-Stokes 20%
• Separation Distance 40%
• Stage Rocket 20%
• Supersonic Flow 100%