Numerical Study of Air-Intake Performance of a Scramjet with Various Cowl Lip Length
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-6874-9_8
Reference18 articles.
1. Fujio C, Hideaki O (2022) Scramjet intake design based on exit flow profile via global optimization and deep learning toward inverse design. In: AIAA SCITECH 2022 forum. https://doi.org/10.2514/6.2022-1408.
2. Devaraj MKK, Jutur P, Rao SMV, Jagadeesh G, Anavardham GTK (2021) Investigation of local unstart in a hypersonic scramjet intake at a Mach number of 6. Aerosp Sci Technol 115. https://doi.org/10.1016/j.ast.2021.106789
3. Flock AK, Ali G (2019) Modified kantrowitz starting criteria for mixed compression supersonic intakes. AIAA J 57(5). https://doi.org/10.2514/1.J057283
4. Kumar A, Singh DJ, Carl AT (1992) Numerical study of the effects of reverse sweep on scramjet inlet performance. J Propuls Power 8(3). https://doi.org/10.2514/3.23537
5. Nguyen T, Marek B, Birgit R, Oliver H, Ali G (2013) Effects of sidewall compression and relaminarization in a scramjet inlet. J Propuls Power 29(3). https://doi.org/10.2514/1.B34740
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