Abstract
This article considers the problem of strong blowing on the surface of a body immersed in a supersonic gas flow. It is not difficult to show that for intense blowing the motion of the blown gas can be described by the Euler equations, and viscosity and transport effects appear only in the neighborhood of the contact surface separating the oncoming flow and the blown gas. It is shown that to a first approximation the pressure is constant across the layer and equal to the pressure at the contact surface.
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, pp. 97–104, No. 5, September–October, 1973.
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Levin, V.A. Strong blowing on the surfaces of a body immersed in a supersonic gas stream. Fluid Dyn 8, 760–766 (1973). https://doi.org/10.1007/BF01023576
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DOI: https://doi.org/10.1007/BF01023576