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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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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