Abstract
Test data on heat transfer and friction are generalized for a wide range of the injection factor with the Mach number equal to 0.3, 2.05, 3.05, and 4. The test results agree with the theoretical analysis also given here.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 23, No. 5, pp. 785–791, November, 1972.
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Mironov, B.P., Yarigina, N.I. Heat transfer and friction in the turbulent boundary layer of a compressible gas at a permeable surface. Journal of Engineering Physics 23, 1359–1363 (1972). https://doi.org/10.1007/BF00834681
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DOI: https://doi.org/10.1007/BF00834681