Modeling the effect of shock unsteadiness in shock-wave/ turbulent boundary layer interactions

Abstract

Reynolds averaged Navier-Stokes methods often cannot predict shock/turbulence interaction correctly. This may be because RANS models do not account for the unsteady motion of the shock wave that is inherent in these interactions. Sinha et al. [Phys. Fluids, Vol. 15, No. 8 (2003)] propose a shock-unsteadiness correction that significantly improves turbulence… (More)

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Cite this paper

@inproceedings{Sinha2004ModelingTE, title={Modeling the effect of shock unsteadiness in shock-wave/ turbulent boundary layer interactions}, author={Krishnendu Sinha and Krishnan Mahesh and Graham V. Candler}, year={2004} }