Influence of air mass flow rate ratio on combustion efficiency of solid rocket ramjet with two air inlets

Engineering

• Air Inlet 100%
• Air Mass Flow Rate 100%
• Eddy Dissipation Model 50%
• Flow Distribution 50%
• Mass Flowrate 50%
• Numerical Study 50%
• One Step 50%
• Reacting Flow 50%
• Secondary Air 50%
• Temperature Distribution 100%
• Thermal Protection 50%

Physics

• Air Mass 100%
• Combustion Efficiency 100%
• Combustion Temperature 33%
• Flow Distribution 33%
• Mass Flow Rate 100%
• Numerical Model 33%
• Reacting Flow 33%
• Temperature Distribution 66%
• Turbulence Model 33%