Abstract
Shock-wave/boundary-layer interactions (SWBLI) frequently occur in supersonic flows, the subject become increasingly important, especially for aerospace applications such as supersonic and hypersonic vehicles, which can have a significant influence on vehicles performance
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References
Liepmann, H.W., Roshko, A., Dhawam, S.: On reflection of shock waves from boundary layers. NACA Rep. 1100 (1952)
Curle, N.: The effect of heat transfer on the laminar boundary layer separation in supersonic flow. Aero.Quart. 12, 309–336 (1961)
Gadd, G.E., Holder, D.W., Regan, J.D.: An experimental investigation of the interaction between shock waves and boundary layers. Proc. Roy. Soc. A 226, 227–253 (1954)
Henderson, L.F.: The reflection of shock wave at a rigid will in the presence of a boundary layer. J. Fluid Mech. 30(4), 699–722 (1967)
Coles, D.E.: The law of the wake in turbulent boundary layer. J. Fluid Mech. 2, 191–226 (1956)
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Bordbar, M., Yao, Y.F. (2015). Analysis of 2D Shock-Wave/Boundary-Layer Intraction Phenomena. 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_66
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DOI: https://doi.org/10.1007/978-3-319-16838-8_66
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
Online ISBN: 978-3-319-16838-8
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