Abstract
The acoustic excitation of the first and second boundary layer modes in the neighborhood of the sharp leading edge of a plate in a supersonic gas flow is analyzed.
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 67–74, July–August, 1991.
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Fedorov, A.V., Khokhlov, A.P. Excitation of unstable modes in a supersonic boundary layer by acoustic waves. Fluid Dyn 26, 531–537 (1991). https://doi.org/10.1007/BF01050314
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DOI: https://doi.org/10.1007/BF01050314