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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2004, Volume 45, Issue 3, Pages 61–71
(Mi pmtf2379)
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This article is cited in 13 scientific papers (total in 13 papers)
Computations of interaction of an incident oblique shock wave with a turbulent boundary layer on a flat plate
N. N. Fedorova, I. A. Fedorchenko Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
Abstract:
Results of numerical simulation of interaction between an oblique shock wave and a turbulent boundary layer formed in a supersonic (Mach number $\mathrm{M} =5$) flow past a flat plate are presented. The computations are performed for three cases of interaction of different intensity, which result in an attached or detached flow. Numerical results are compared with experimental data. The effect of flow turbulence and shock-wave unsteadiness on flow parameters is studied.
Keywords:
shock wave, boundary layer, separated flow, turbulence, heat transfer.
Received: 28.03.2003 Accepted: 08.05.2003
Citation:
N. N. Fedorova, I. A. Fedorchenko, “Computations of interaction of an incident oblique shock wave with a turbulent boundary layer on a flat plate”, Prikl. Mekh. Tekh. Fiz., 45:3 (2004), 61–71; J. Appl. Mech. Tech. Phys., 45:3 (2004), 358–366
Linking options:
https://www.mathnet.ru/eng/pmtf2379 https://www.mathnet.ru/eng/pmtf/v45/i3/p61
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