Abstract
The efficient computational prediction of supersonic flow is of interest to both the aerospace and energy industries, with internal and external flow applications including flow through engines, intake ducts and nozzles
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Asproulias, I., Revell, A.J., Craft, T.J. (2015). Modelling Shock Wave/Boundary Layer Interactions Using Advanced RANS Models. 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_71
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DOI: https://doi.org/10.1007/978-3-319-16838-8_71
Publisher Name: Springer, Cham
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