Abstract
Prediction of swept-shock-wave induced 3-D turbulent-boundary-layer separation in the vicinity of a single sharp fin mounted on a flat plate (see Fig. 1a) at Mach numbers 3, 4 and 5 with fin inclination angles ranging from 9° to 30.6° has been carried out by steady 3-D compressible RANS computation with Reynolds Stress turbulence Model (RSM)
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Salin, A., Yao, Y.F., Zheltovodov, A.A. (2015). Numerical Prediction of 3-D Supersonic Turbulent Separation Initiated by a Single-Fin. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 2. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16838-8_76
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DOI: https://doi.org/10.1007/978-3-319-16838-8_76
Publisher Name: Springer, Cham
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