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Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream

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Abstract

The results are given of the calculation of a three-dimensional boundary layer on a triangular plate of finite length in a regime of strong viscous interaction with an external hypersonic stream for both symmetric flow as well as in the presence of an angle of slip. The influence of the change in the pressure on the trailing edge of the plate on the boundary layer characteristics is investigated.

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Authors and Affiliations

  1. Moscow

    G. N. Dudin

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  1. G. N. Dudin
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 46–52, September–October, 1982.

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Dudin, G.N. Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream. Fluid Dyn 17, 693–698 (1982). https://doi.org/10.1007/BF01090147

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  • DOI: https://doi.org/10.1007/BF01090147

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