Funder
National Natural Science Foundation of China
the Graduate Innovation Grant of Hunan Province , China
Publisher
Zhejiang University Press
Reference29 articles.
1. Anderson JD, 2003. Modern Compressible Flow: with Historical Perspective, 3rd Edition. McGraw Hill Education, New York, USA, p. 127–187.
2. Babinsky H, Harvey JK, 2011. Shock Wave-Boundary-Layer Interactions. Cambridge University Press, Cambridge, UK, p.5–86.
3. Bodner JP, Greber I, Davis DO, et al., 1996. Experimental investigation of the effect of a single bleed hole on a supersonic turbulent boundary-layer. Proceedings of the 32nd Joint Propulsion Conference and Exhibit. https://doi.org/10.2514/6.1996-2797
4. MS Thesis;S Bunnag,2010
5. Chang JT, Li N, Xu KJ, et al., 2017. Recent research progress on unstart mechanism, detection and control of hypersonic inlet. Progress in Aerospace Sciences, 89:1–20. https://doi.org/10.1016/j.paerosci.2016.12.001
Cited by
14 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献