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Stability of a supersonic boundary layer on a permeable surface with heat transfer

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Abstract

The effect of cooling of a permeable surface on the stability of a supersonic boundary layer on it is investigated. As distinct from the case of an impermeable surface, deep cooling can reduce the critical Reynolds number. Common points of the continuous and discrete spectra are found in the region of the disturbance parameters.

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  1. Novosibirsk

    S. A. Gaponov

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  1. S. A. Gaponov
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 41–46, January–February, 1977.

The work was carried out at the Department of Applied Mathematics of the University of Western Ontario in Canada. I am grateful to the Head of the Department Professor J. Blackwell for suggesting the investigation of this problem.

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Gaponov, S.A. Stability of a supersonic boundary layer on a permeable surface with heat transfer. Fluid Dyn 12, 33–38 (1977). https://doi.org/10.1007/BF01074621

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  • DOI: https://doi.org/10.1007/BF01074621

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