Summary
The present contribution describes the Reynolds stress behaviour through a supersonic compression cornerflow. After a comparison between increasing complexity turbulence models (algebraîc-two equation and second order) for mean flow quantities in the 16° angle case, a more detailed analysis of the Reynolds stress anisotropy is made for the 20° angle flow.
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References
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© 1986 Springer-Verlag Berlin, Heidelberg
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Vandromme, D., Ha Minh, H. (1986). Physical Analysis of Turbulent Boundary-Layer/Shock-Wave Interactions Using Second Order Closure Predictions. In: Délery, J. (eds) Turbulent Shear-Layer/Shock-Wave Interactions. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82770-9_11
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DOI: https://doi.org/10.1007/978-3-642-82770-9_11
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82772-3
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