Film cooling with normal injection into a supersonic flow

Engineering

• Boundary Layer 100%
• Supersonic Flow 100%
• Mach Number 50%
• Good Agreement 50%
• Mass Velocity 50%
• Fluid Property 50%
• Incompressible Flow 50%
• Flat Plate 50%
• Gas Injection 50%
• Two-Dimensional Turbulent Boundary Layer 50%
• Porosity 50%
• Free Flow 50%

Keyphrases

• Supersonic Flow 100%
• Film Cooling 100%
• Secondary Fluid 66%
• Turbulent Boundary Layers 33%
• Boundary Layer 33%
• In-stream 33%
• Two Dimensional 33%
• Incompressible Flow 33%
• Mach number 33%
• Free Stream 33%
• Flat Plate 33%
• High-speed Boundary Layer 33%
• Adiabatic Wall Temperature 33%
• Mass Velocity 33%
• Gas Injection 33%
• Fluid Property Variation 33%