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Analysis of the three-dimensional turbulent boundary layer on the suface of an arbitrary body at large angles of attack

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Abstract

Three-dimensional compressible gas flow past an arbitrary model body at large angles of attack is analyzed in the framework of the boundary layer theory with allowance for heat transfer. The equations of a three-dimensional turbulent boundary layer are solved using computer codes, the data on the external inviscid flow, and the body geometry.

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  1. Moscow

    V. A. Aleksin

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  1. V. A. Aleksin
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Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 3, pp. 55–66, May–June, 1995.

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Aleksin, V.A. Analysis of the three-dimensional turbulent boundary layer on the suface of an arbitrary body at large angles of attack. Fluid Dyn 30, 378–386 (1995). https://doi.org/10.1007/BF02282450

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  • DOI: https://doi.org/10.1007/BF02282450

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