New experimental data of STBLI at DNS/LES accessible reynolds numbers

Engineering

• Boundary Layer 100%
• Compression Corner 100%
• Dimensional Image 50%
• Experimental Investigation 50%
• Good Agreement 50%
• Layer Interaction 50%
• Mach Number 50%
• Reflected Shock 50%
• Reynolds' Number 100%
• Separated Region 50%
• Shock Interaction 50%
• Statistical Data 50%
• Streamwise 50%
• Surface Flow Visualization 50%
• Surface Pressure Distribution 50%
• Turbulent Boundary Layer 50%
• Two Dimensional 50%

Keyphrases

• Direction Giving 33%