Abstract
A numerical method is developed for calculating the motion of a subsonic or transonic flow around a solid of revolution with due allowance for the effects of the reactive jet, the bottom projection, possible noncoincidence between the planes of the nozzle tip and the stern section, nonuniformity of the flow at the nozzle outlet, the ejecting action of the supersonic jet, and also the displacement of the boundary layer. Examples of such calculations are given for solids of revolution of different shapes and nozzles of different types; comparison is also made with experimental data.
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 2, pp. 97–104, March–April, 1974.
The author wishes to thank A. N. Kraiko and M. Ya. Ivanov for useful help and advice, and A. M. Konkina for setting up the paper.
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Tagirov, R.K. Transonic flow around a solid of revolution during the outflow of a reactive jet from its stern section. Fluid Dyn 9, 243–249 (1974). https://doi.org/10.1007/BF01092657
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DOI: https://doi.org/10.1007/BF01092657