Study on two-dimensional and three-dimensional secondary jet interactions with a supersonic flow

Engineering

• Turbulent Boundary Layer 100%
• Interaction Region 50%
• Experiments 33%
• Flow Field 33%
• Freestream 33%
• Pressure Ratio 33%
• Secondary Flow 33%
• Layer Interaction 33%
• Temperature 16%
• Thickness 16%
• Two Dimensional 16%
• Oil 16%
• Reynolds' Number 16%
• Flat Plate 16%
• Surface Pressure Distribution 16%
• Nozzle 16%
• Flow Structure 16%
• Nozzle Exit 16%
• Leading Edge 16%
• Schlieren Method 16%
• Circular Nozzle 16%
• Boundary Layer Separation 16%
• Bow Shock Wave 16%
• Separation Region 16%
• Jet Interaction 16%

Physics

• Supersonic Flow 100%
• Pressure 50%
• Injection 50%
• Shock Wave 50%
• Flow Distribution 33%
• Secondary Flow 33%
• Temperature 16%
• Differences 16%
• Width 16%
• Distance 16%
• Separated Flow 16%
• Reynolds Number 16%
• Mach Number 16%
• Flat Plates 16%