Analysis of shockwave/turbulent boundary layer interaction using DNS and experimental data

Engineering

• Turbulent Boundary Layer 100%
• Layer Interaction 100%
• Shockwave 100%
• Boundary Layer 50%
• Flow Condition 50%
• Computer Simulation 50%
• Mach Number 50%
• Reattachment 50%
• Flow Separation 50%
• Pressure Distribution 50%
• Wall-Pressure 50%
• Mass Transfer 50%
• Velocity Profile 50%
• Turbulence Intensity 50%
• Direct Numerical Simulation 50%
• Experimental Data Set 50%

Physics

• Turbulent Boundary Layer 100%
• Mach Number 50%
• Boundary Layer 50%
• Direct Numerical Simulation 50%
• Laminar Boundary Layer 50%
• Pressure Distribution 50%
• Wall Pressure 50%

Keyphrases

• Compression Shock 50%
• Flow Reattachment 50%