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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2005, Volume 46, Issue 3, Pages 23–28
(Mi pmtf2261)
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This article is cited in 1 scientific paper (total in 1 paper)
Effect of the boundary layer on the base pressure in a two-dimensional flow with a Mach number $\mathrm{M}=5$
M. G. Ktalkhermana, V. M. Mal'kovb a Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b Ustinov Baltic State Technical University (Voenmekh), St. Petersburg, 190005
Abstract:
New data on the base pressure in a two-dimensional ow with a Mach number $\mathrm{M}=5$ are obtained for a wide range of variation of the normalized boundary-layer thickness in the flow-separation cross section. The test results are compared with Tanner’s theory, and a conclusion is made that this numerical model has to be corrected.
Keywords:
supersonic flow, turbulent boundary layer, base pressure.
Received: 21.06.2004 Accepted: 07.10.2004
Citation:
M. G. Ktalkherman, V. M. Mal'kov, “Effect of the boundary layer on the base pressure in a two-dimensional flow with a Mach number $\mathrm{M}=5$”, Prikl. Mekh. Tekh. Fiz., 46:3 (2005), 23–28; J. Appl. Mech. Tech. Phys., 46:3 (2005), 324–328
Linking options:
https://www.mathnet.ru/eng/pmtf2261 https://www.mathnet.ru/eng/pmtf/v46/i3/p23
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Abstract page: | 37 | Full-text PDF : | 7 |
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