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Teplofizika vysokikh temperatur, 2002, Volume 40, Issue 2, Pages 256–261
(Mi tvt1774)
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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
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
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
Linking options:
https://www.mathnet.ru/eng/tvt1774 https://www.mathnet.ru/eng/tvt/v40/i2/p256
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Abstract page: | 135 | Full-text PDF : | 76 |
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