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This article is cited in 16 scientific papers (total in 16 papers)
Heat and Mass Transfer and Physical Gasdynamics
Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate
V. G. Lushchik, M. S. Makarova Lomonosov Moscow State University, Institute of Mechanics
Abstract:
We performed a numerical study of the boundary layer on a wall in a supersonic gas flow using a differential turbulence model. The dependences of the recovery factor and the Reynolds analogy factor on the main flow parameters, such as the Reynolds, Mach, and Prandtl numbers, are obtained for a series of the temperature factor values. The results of calculations are approximated by the dependences of the recovery factor and the Reynolds analogy factor on the Prandtl number.
Received: 19.03.2015 Accepted: 16.06.2015
Citation:
V. G. Lushchik, M. S. Makarova, “Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate”, TVT, 54:3 (2016), 401–407; High Temperature, 54:3 (2016), 377–382
Linking options:
https://www.mathnet.ru/eng/tvt8557 https://www.mathnet.ru/eng/tvt/v54/i3/p401
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Abstract page: | 263 | Full-text PDF : | 127 | References: | 65 | First page: | 4 |
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