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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2005, Volume 46, Issue 3, Pages 23–28 (Mi pmtf2261)  
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 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
Full-text PDF (1805 kB) Citations (1)
Abstract: New data on the base pressure in a two-dimensional ow with a Mach number 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
English version:
Journal of Applied Mechanics and Technical Physics, 2005, Volume 46, Issue 3, Pages 324–328
DOI: https://doi.org/10.1007/s10808-005-0081-x
Bibliographic databases:
Document Type: Article
UDC: 533.6.011
Language: Russian
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 M=5”, Prikl. Mekh. Tekh. Fiz., 46:3 (2005), 23–28; J. Appl. Mech. Tech. Phys., 46:3 (2005), 324–328
Citation in format AMSBIB
\Bibitem{KtaMal05}
\by M.~G.~Ktalkherman, V.~M.~Mal'kov
\paper Effect of the boundary layer on the base pressure in a two-dimensional flow with a Mach number $\mathrm{M}=5$
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2005
\vol 46
\issue 3
\pages 23--28
\mathnet{http://mi.mathnet.ru/pmtf2261}
\elib{https://elibrary.ru/item.asp?id=15175925}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2005
\vol 46
\issue 3
\pages 324--328
\crossref{https://doi.org/10.1007/s10808-005-0081-x}
Linking options:
  • https://www.mathnet.ru/eng/pmtf2261
  • https://www.mathnet.ru/eng/pmtf/v46/i3/p23
    • This publication is cited in the following 1 articles:
    1. V Lijo, H D Kim, T Setoguchi, “Numerical investigation of the effects of base size on supersonic flow through a sudden duct enlargement”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 226:12 (2012), 1562  crossref
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
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