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Supersonic gas flow over a wavy surface

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Abstract

Exact numerical solutions of the problem are obtained for a compressible viscous heat-conducting gas flowing over a slightly wavy surface. The effect of the free-stream parameters on the stresses, the temperature fields and the heat fluxes at the wavy interface is studied in detail.

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Authors and Affiliations

  1. Krasnodar, Moscow

    E. A. Demekhin & V. Ya. Shkadov

Authors
  1. E. A. Demekhin
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  2. V. Ya. Shkadov
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 15–22, November–December, 1988.

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Demekhin, E.A., Shkadov, V.Y. Supersonic gas flow over a wavy surface. Fluid Dyn 23, 811–818 (1988). https://doi.org/10.1007/BF01051813

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  • DOI: https://doi.org/10.1007/BF01051813

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