LES study of flame stabilization in DLR hydrogen supersonic combustor with strut injection

Keyphrases

• Large Eddy Simulation 100%
• Simulation Study 100%
• Three Dimensional Model 100%
• Axial Velocity 100%
• Flame Stabilization 100%
• Supersonic Combustor 100%
• Strut Injection 100%
• Hydrogen Fuel 50%
• Combustion 50%
• Temperature Measurement 50%
• Two Dimensional 50%
• Reduced Model 50%
• Flow Condition 50%
• Two Dimensional Model 50%
• Computational Model 50%
• Turbulent Combustion 50%
• Span-wise 50%
• Static Temperature 50%
• Radical Transformation 50%
• Reacting Flow 50%
• Combustion Mode 50%
• Detailed Reaction Mechanism 50%
• Combustor 50%
• Flame Stabilization Mechanism 50%
• Supersonic Combustion 50%
• Combustion Stage 50%
• Three-stage Combustion 50%
• Heat Release Analysis 50%
• Hydrogen Combustion 50%
• Scramjet Combustor 50%
• Wall Pressure Measurements 50%
• Non-reacting Flow 50%

Engineering

• Combustor 100%
• Two Dimensional 66%
• Three-Dimensional Models 66%
• Reacting Flow 66%
• Axial Velocity 66%
• Heat Release 33%
• Flow Condition 33%
• Good Agreement 33%
• Static Temperature 33%
• Wall-Pressure 33%
• Spanwise Direction 33%
• Combustion Mode 33%
• Combustion Stage 33%
• Supersonic Combustion 33%
• Dimensional Model 33%