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Experimental Study on Mach 4 Supersonic Internal Flow:Visualization of Shock Wave and Turbulent Boundary Layer Interaction

Koichi Fukuda, Hiromu Sugiyama, Kazuhide MIZOBATA, Kiyokazu Endo

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Key concepts: Boundary layer, Mach number, Shock wave, Supersonic speed, Mechanics, Mach wave, Flow visualization, Shock (circulatory)

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Experimental Study on Mach 4 Supersonic Internal Flow:Visualization of Shock Wave and Turbulent Boundary Layer Interaction — Research Paper | ScholarLens