Heat transfer near injection hole by shock and boundary layer interaction in the supersonic flow field

Engineering

• Heat Transfer 100%
• Supersonic Flow 66%
• Nozzle 33%
• Flow Structure 33%
• Research 33%
• Surfaces 33%
• Computer Simulation 16%
• Layer Interaction 16%
• Peak Value 16%
• Flow Field 16%
• Heat Transfer Coefficient 16%
• Momentum Flux 16%
• Numerical Method 16%
• Separation Point 16%
• Freestream 16%
• Expansion Ratio 16%
• Injection System 16%
• Shock Interaction 16%
• Facilities 16%
• Oil 16%
• Transients 16%
• Tunnels 16%

Physics

• Injection 83%
• Ratios 66%
• Momentum 50%
• Supersonics 33%
• Position (Location) 33%
• Penetration 16%
• Boundary Layer 16%
• Thermal Design 16%
• Flow Distribution 16%
• Mathematical Method 16%
• Thermography 16%
• Secondary Injection 16%
• Shock Layer 16%
• Increasing 16%
• Variations 16%
• Transients 16%
• Diameters 16%
• Expansion 16%
• Geometry 16%
• Tunnel 16%