This article is cited in 14 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.

UDC: 532.517.2:532.533.601.155

Received: 28.03.2003
Accepted: 08.05.2003

 English version: Journal of Applied Mechanics and Technical Physics, 2004, 45:3, 358–366

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