Abstract
In this paper computational results for two different types of shock wave / turbulent boundary layer interaction flows are presented. It is shown that upstream effects of the shock induced separation cannot be reproduced by Wilcox's (1991) k-ω-model, whereas downstream of the interaction, predictions of pressure distribution and skin friction are acceptable. The inclusion of the compressible part of the dissipation rate and the pressure dilatation in the model has noticeable, but not dramatic effects on wall pressure and skin friction in the selected flow cases.
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Haidinger, F.A., Friedrich, R. Computation of shock wave/turbulent boundary layer interactions using a two-equation model with compressibility corrections. Appl. Sci. Res. 51, 501–505 (1993). https://doi.org/10.1007/BF01082582
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DOI: https://doi.org/10.1007/BF01082582