Experimental investigation of an embedded separated flow region between two supersonic streams

Keyphrases

• Shear Layer 100%
• Separated Flow Region 100%
• Flow Field 66%
• Two-component 33%
• Velocity Profile 33%
• Two Dimensional 33%
• Kinematics 33%
• Strong Interaction 33%
• Boundary Layer 33%
• Turbulence 33%
• Velocity Field 33%
• Mixing Layer 33%
• Finite Thickness 33%
• Pressure Measurement 33%
• Missile 33%
• Mean Velocity 33%
• Turbulent Field 33%
• Recompression 33%
• Schlieren Photography 33%
• Complex Interactions 33%
• Turbulence Intensity 33%
• Reynolds Stress 33%
• Interaction Region 33%
• Laser Doppler Velocimeter 33%
• Truncated Boundary 33%
• Constant Pressure Mixing 33%
• Mixing Region 33%
• Low-velocity Regions 33%
• Negative Velocity 33%
• High-speed Flight 33%
• Runnel 33%

Engineering

• Experimental Investigation 100%
• Shear Layer 100%
• Separated Flow Region 100%
• Velocity Profile 33%
• Two Dimensional 33%
• Doppler Velocimeter 33%
• Strong Interaction 33%
• Boundary Layer 33%
• Velocity Field 33%
• Schlieren 33%
• Turbulence Intensity 33%
• Reynolds Stress 33%
• Interaction Region 33%
• Recompression Region 33%
• Mixing Region 33%