Experimental validation of flow field in the secondary combustor of a subscale ducted rocket

Engineering

• Combustor 100%
• Flow Distribution 100%
• Experimental Result 33%
• Simulation Method 33%
• Temperature Distribution 33%
• Hot Gas 33%
• Mass Flowrate 33%
• Structural Parameter 33%
• Boundary Condition 33%
• Rocket Engine 33%
• Flow Pressure 33%
• Combustion Temperature 33%
• Secondary Flow 33%
• Direct Connection 33%
• Primary Air 33%
• Primary Flow 33%