Numerical simulation of secondary combustion of hydrogen injected from preburner into supersonic airflow

Engineering

• Ignition 100%
• Computer Simulation 100%
• Experimental Result 50%
• Low-Temperature 50%
• Navier-Stokes Equation 50%
• Total Variation 50%
• Gauss 50%
• Wake Flow 50%
• Algebraic Turbulence Model 50%

Keyphrases

• Secondary Combustion 100%
• Preburner 100%
• Self-combustion 33%
• Supersonic Wake 33%
• Airflow Temperature 33%
• Wake Flow 33%