Abstract
A method is proposed for solving the three-dimensional equations of laminar and turbulent boundary layers on a pointed rotating axisym-metric cone flying at an angle of attack α. New properties of the obtained solutions are found, and a comparison is made with the results of other authors.
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 34–39, May–June, 1984.
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Pokrovskii, A.N., Shmanenkov, V.N. & Shchuchinov, V.M. Determination of the parameters of the boundary layer on rotating axisymmetric cones. Fluid Dyn 19, 367–372 (1984). https://doi.org/10.1007/BF01093898
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DOI: https://doi.org/10.1007/BF01093898