The distortion of a supersonic turbulent boundary layer by bulk compression and surface curvature

Keyphrases

• Boundary Layer 50%
• Bulk Compressibility 100%
• Compression Corner 100%
• Constant Radius 50%
• Corner Flow 50%
• Curved Wall 50%
• Mach number 50%
• Normal Stress 100%
• Shear Stress 100%
• Streamline Curvature 50%
• Supersonic Turbulent Boundary Layer 100%
• Surface Curvature 100%
• Total Strain 50%
• Turbulence 100%
• Turning Angle 50%
• Unit Reynolds number 50%
• Wall Model 50%

Engineering

• Applied Strain 50%
• Boundary Layer 50%
• Compression Corner 100%
• Constant Radius 50%
• Experimental Investigation 50%
• Mach Number 50%
• Reynolds' Number 50%
• Streamlines 50%
• Turbulent Boundary Layer 100%