Effects of bump parameters on hypersonic inlet starting performance
Author:
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2200155.pdf
Reference37 articles.
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4. Colliss SP, Babinsky H, Nübler K, et al., 2014. Joint experimental and numerical approach to three-dimensional shock control bump research. AIAA Journal, 52(2):436–446. https://doi.org/10.2514/1.J052582
5. Curran ET, 2001. Scramjet engines: the first forty years. Journal of Propulsion and Power, 17(6):1138–1148. https://doi.org/10.2514/2.5875
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