Teplofizika vysokikh temperatur
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Teplofizika vysokikh temperatur, 2002, Volume 40, Issue 2, Pages 256–261 (Mi tvt1774)  
This article is cited in 1 scientific paper (total in 1 paper)

Heat and Mass Transfer and Physical Gasdynamics

Viscous Shock Layer on a Cone in Hypersonic Flow

T. V. Poplavskaya

Institute of Theoretical and Applied Mechanics, Novosibirsk
Full-text PDF (1264 kB) Citations (1)
Abstract: The results are given of a theoretical investigation of hypersonic flow past a pointed cone at zero angle of attack. The flow characteristics are calculated using equations of complete viscous shock layer. The universal dimensionless dependence of the Stanton number on the determining parameters of the problem is obtained.
Received: 06.03.2001
English version:
High Temperature, 2002, Volume 40, Issue 2, Pages 228–233
DOI: https://doi.org/10.1023/A:1015203206949
Bibliographic databases:
Document Type: Article
UDC: 532.526
Language: Russian
Citation: T. V. Poplavskaya, “Viscous Shock Layer on a Cone in Hypersonic Flow”, TVT, 40:2 (2002), 256–261; High Temperature, 40:2 (2002), 228–233
Citation in format AMSBIB
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\paper Viscous Shock Layer on a Cone in Hypersonic Flow
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\pages 256--261
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\jour High Temperature
\yr 2002
\vol 40
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\pages 228--233
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  • https://www.mathnet.ru/eng/tvt/v40/i2/p256
    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Teplofizika vysokikh temperatur Teplofizika vysokikh temperatur
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