Abstract
The one-parameter method of calculating the turbulent boundary layer of a compressible gas with positive axial pressure gradient is analyzed. Theory is compared with experiment. One of the advantages of this method is its simplicity.
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Mironov, B.P. Turbulent boundary layer in a supersonic diffuser. Journal of Engineering Physics 9, 1–4 (1965). https://doi.org/10.1007/BF00831824
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DOI: https://doi.org/10.1007/BF00831824