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TVT, 2002, Volume 40, Issue 2, Pages 256–261 (Mi tvt1774)  

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

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.

Full text: PDF file (1264 kB)

English version:
High Temperature, 2002, 40:2, 228–233

Bibliographic databases:

UDC: 532.526
Received: 06.03.2001

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
\Bibitem{Pop02}
\by T.~V.~Poplavskaya
\paper Viscous Shock Layer on a Cone in Hypersonic Flow
\jour TVT
\yr 2002
\vol 40
\issue 2
\pages 256--261
\mathnet{http://mi.mathnet.ru/tvt1774}
\transl
\jour High Temperature
\yr 2002
\vol 40
\issue 2
\pages 228--233
\crossref{https://doi.org/10.1023/A:1015203206949}
\isi{http://gateway.isiknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&DestLinkType=FullRecord&DestApp=ALL_WOS&KeyUT=000175472200013}


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