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Semiempirical method of calculating overexpanded turbulent separated flow in a conical laval nozzle

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Abstract

A mathematical model of separated nozzle flow is developed. The model takes into account the effect of the boundary layer and the pressure variation over the entire separation zone inside the nozzle. The effect of the geometric and gas dynamic factors on the separated flow pattern is investigated numerically.

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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 60–66, November–December, 1988.

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Malik, T.I., Tagirov, R.K. Semiempirical method of calculating overexpanded turbulent separated flow in a conical laval nozzle. Fluid Dyn 23, 851–856 (1988). https://doi.org/10.1007/BF01051818

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  • DOI: https://doi.org/10.1007/BF01051818

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