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Three-dimensional boundary layer on a plane delta wing in the intermediate hypersonic interaction regime

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Abstract

The results of calculating the three-dimensional boundary layer on a plane delta wing of finite length in the intermediate hypersonic interaction regime are presented. The effect of the hypersonic interaction parameter on the gas flow in the boundary layer and the aerodynamic characteristics is investigated.

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  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. 3, pp. 110–116, May–June, 1991.

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Dudin, G.N. Three-dimensional boundary layer on a plane delta wing in the intermediate hypersonic interaction regime. Fluid Dyn 26, 409–414 (1991). https://doi.org/10.1007/BF01059013

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  • DOI: https://doi.org/10.1007/BF01059013

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