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Shape of the subsonic part of a nozzle with a flat acoustic surface with allowance for viscosity in the boundary-layer approximation

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Abstract

A numerical construction is proposed for the shape of the wall of the subsonic part of a nozzle. The design realizes nonseparated flow with an absence of local supersonic zones. The method is based on the simultaneous numerical solution of boundary-layer equations and equations of motion of an inviscid gas.

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Literature cited

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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 42, No. 5, pp. 724–729, May, 1982.

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Osipov, I.L., Shipilin, A.V. & Shulishnina, N.P. Shape of the subsonic part of a nozzle with a flat acoustic surface with allowance for viscosity in the boundary-layer approximation. Journal of Engineering Physics 42, 491–495 (1982). https://doi.org/10.1007/BF00824937

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  • DOI: https://doi.org/10.1007/BF00824937

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