DISTORTION OF A SUPERSONIC TURBULENT BOUNDARY LAYER BY BULK COMPRESSION AND SURFACE CURVATURE.

Keyphrases

• Normal Stress 100%
• Shear Stress 100%
• Supersonic Turbulent Boundary Layer 100%
• Bulk Compressibility 100%
• Surface Curvature 100%
• Boundary Layer 50%
• Mach number 50%
• Wall Model 50%
• Streamline Curvature 50%
• Curved Wall 50%
• Constant Radius 50%
• Unit Reynolds number 50%

Engineering

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

Physics

• Supersonics 100%
• Turbulent Boundary Layer 100%
• Mach Number 50%
• Reynolds Number 50%
• Boundary Layer 50%