Combustion flow field analysis of a scramjet engine at high Mach number

Engineering

• Applicability 50%
• Combustion Mode 100%
• Commercial Software 50%
• Computational Fluid Dynamics 100%
• Engine Operating 50%
• Flow Condition 50%
• Flow Distribution 100%
• Flow Structure 50%
• Good Agreement 50%
• Heat Release 100%
• High Mach Number 100%
• Hypersonic Flows 50%
• Kinetic Model 50%
• Mach Number 50%
• Multiscale 50%
• Pressure Distribution 50%
• Reynolds-Averaged Navier-Stokes 50%
• Spatial Distribution 50%
• Wall-Pressure 50%