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Laser Energy Deposition for Shock Wave Boundary Layer Control at Supersonic Speeds

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29th International Symposium on Shock Waves 2 (ISSW 2013)

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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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References

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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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