Abstract
Shock waves are generated around space vehicles under the re-entry environment and they interact with other shock waves or the boundary layer over the wing and flaps. The interactions between shock waves or shock wave/boundary layer cause high local heat flux on the surface. Edney classified the types of these interactions into six[1] and he discussed about the shock interaction patterns in detail.
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References
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Kuramoto, T., Muto, D., Tsuboi, N., Nagai, H., Asai, K. (2015). Numerical Study on Shock Wave Interaction over Compression Corner with 30 deg. in Hypersonic Flow. 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_64
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DOI: https://doi.org/10.1007/978-3-319-16838-8_64
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
Online ISBN: 978-3-319-16838-8
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