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This is a Experimental Study study (also classified as: Quantitative Study).

Supersonic turbulent boundary layer on a plate. Universal velocity and temperature defect laws and skin-friction law at moderate free-stream Mach numbers

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Analysis reveals universal velocity and temperature defect laws in supersonic flow, suggesting new insights into skin-friction behavior.

The study derives universal laws for velocity and temperature profiles in supersonic turbulent boundary layers.
Key relationships in turbulent shear stress and enthalpy are formulated, enhancing our understanding of boundary-layer behavior.
Necessary matchings of solutions led to the formulation of skin-friction laws applicable across varied heat-transfer conditions.
The findings may influence future designs of aerodynamic surfaces operating under supersonic conditions.

И. И. Вигдорович (2025) studied this question.

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