Abstract
Results of experimental studies are shown concerning the aerodynamic characteristics of diffusers with the transition profile designed for a near-separating turbulent boundary layer. The test results are shown to agree closely with calculations.
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Additional information
Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 21, No. 3, pp. 518–523, September, 1971.
The author thanks A. S. Ginevskii for assistance in carrying out this work.
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Bychkova, L.A. Experimental study of diffuser channels with a near-separating turbulent boundary layer. Journal of Engineering Physics 21, 1176–1180 (1971). https://doi.org/10.1007/BF00826122
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DOI: https://doi.org/10.1007/BF00826122