Abstract
Shock Wave Boundary Layer Interactions (SWBLIs) can induce separation which causes loss of a control surface effectiveness, drop of an air intake efficiency and it may be the origin of large scale fluctuations such as air-intake buzz, buffeting or fluctuating side loads in separated propulsive nozzles
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Erdem, E., Kontis, K., Osuka, T., Majima, R., Tamba, T., Sasoh, A. (2015). Laser Energy Deposition for Shock Wave Boundary Layer Control at Supersonic Speeds. 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_100
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DOI: https://doi.org/10.1007/978-3-319-16838-8_100
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
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