Introduction
The UFAST project is centred on three main configurations with shock induced separations: transonic flow around a profile; normal shock on a flat plate or on a curved surface; and an oblique shock reflection, as summarized in figure 13.1. For each case, the effect of control devices was also investigated. Experimental data were compared to (U)RANS, DES, and LES simulations, for all these configurations. This section is focused on the issues related to (U)RANS simulations.
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References
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Bruce, P.J.K., Babinsky, H., Tartinville, B., Hirsch, C.: An experimental and numerical study of an oscillating transonic shock wave in a duct. In: Proc. 48th Aerospace Sciences Meeting, Orlando, AIAA Paper-2010-xxxx (2010)
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Doerffer, P., Hirsch, C., Dussauge, JP., Babinsky, H., Barakos, G.N. (2010). WP-4 RANS/URANS Simulations (Charles Hirsch). In: Unsteady Effects of Shock Wave Induced Separation. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 114. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03004-8_13
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DOI: https://doi.org/10.1007/978-3-642-03004-8_13
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