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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2001, Volume 42, Issue 5, Pages 27–36
(Mi pmtf2816)
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This article is cited in 16 scientific papers (total in 16 papers)
Flow regimes formed by a counterflow jet in a supersonic flow
V. M. Fomina, A. A. Maslova, A. P. Shashkina, T. A. Korotaevaa, N. D. Malmuthb a Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b Rockwell Research Center, Thousand Oaks, California, U.S.A
Abstract:
Results on the effect of the dynamic pressure, Mach number, and temperature of a jet injected from a body upstream in a free supersonic flow on the formation of flow regimes are presented. Flow regimes that ensure the greatest decrease in the drag of the body are given, the mechanism of formation of the LPM flow structure is described, and an approximate criterion is found, which allows determination of the range of existence of various modes of jet penetration into the flow.
Received: 28.05.2001
Citation:
V. M. Fomin, A. A. Maslov, A. P. Shashkin, T. A. Korotaeva, N. D. Malmuth, “Flow regimes formed by a counterflow jet in a supersonic flow”, Prikl. Mekh. Tekh. Fiz., 42:5 (2001), 27–36; J. Appl. Mech. Tech. Phys., 42:5 (2001), 757–764
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https://www.mathnet.ru/eng/pmtf2816 https://www.mathnet.ru/eng/pmtf/v42/i5/p27
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Abstract page: | 41 | Full-text PDF : | 36 |
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