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Three-dimensional interference of oblique shock with boundary and high-entropy layers (M = 6, free boundary layer transition)

Project: Visualization of Mechanical Processes

Journal: Visualization of Mechanical Processes: An International Online Journal

Article: HYPERSONIC TURBULENT HEATING OF SHARP AND BLUNT PLATES NEAR A WEDGE

Topics: Heat transfer coefficient, Aerodynamics, Supersonic flows

Three-dimensional interference of oblique shock with boundary and high-entropy layers (M=6, free boundary layer transition). Distribution of a nondimensional heat-transfer coefficient (Stanton number) over the plate surface near a 15 degree wedge depends on the plate leading edge bluntness radius r. Mach number M=6, Reynolds number Re∞L=20×106, total pressure Ро=85 bar, total temperature То=650 К, induced boundary layer transition.

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