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Teplofizika vysokikh temperatur, 2006, Volume 44, Issue 2, Pages 238–245
(Mi tvt1311)
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This article is cited in 16 scientific papers (total in 16 papers)
Heat and Mass Transfer and Physical Gasdynamics
The recovery factor in a supersonic flow of gas with a low Prandtl number
A. I. Leont'eva, V. G. Lushchikb, A. E. Yakubenkoc a Bauman Moscow State Technical University
b NPO Energomash, Khimki, Moscow region
c Institute of Mechanics, M. V. Lomonosov Moscow State University
Abstract:
A three-parameter differential model of turbulence supplemented with a transport equation for turbulent heat flux is used to perform calculations of the boundary layer on a heat-insulated wall in a supersonic gas flow with a value of Prandtl number $\mathrm{Pr}\le0.7$. The dependences on the values of Prandtl, Reynolds, and Mach numbers and of intensity of injection are obtained for the recovery factor.
Citation:
A. I. Leont'ev, V. G. Lushchik, A. E. Yakubenko, “The recovery factor in a supersonic flow of gas with a low Prandtl number”, TVT, 44:2 (2006), 238–245; High Temperature, 44:2 (2006), 234–242
Linking options:
https://www.mathnet.ru/eng/tvt1311 https://www.mathnet.ru/eng/tvt/v44/i2/p238
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