Summary
The paper deals with the interaction of a weak oblique shock and a turbulent boundary layer at a flat plate at purely supersonic speeds. Except for a small region where nonlinear transonic effects are of importance analytical expressions for the pressure- and skin friction distributions are derived.
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Kluwick, A., Stross, N. Interaction between a weak oblique shock wave and a turbulent boundary layer in purely supersonic flow. Acta Mechanica 53, 37–56 (1984). https://doi.org/10.1007/BF01176249
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DOI: https://doi.org/10.1007/BF01176249