Open Access
Issue |
Volume 11, 2019
Progress in Propulsion Physics – Volume 11
|
|
---|---|---|
Page(s) | 729 - 746 | |
DOI | https://doi.org/10.1051/eucass/201911729 | |
Published online | 08 February 2019 |
- Emami, S., C. A. Trexler, A. H. Auslender, and J. P. Weidner. 1995. Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach Number of 4 NASA Technical Pater 3502. [Google Scholar]
- Falempin, F., E. Wendling, M. Goldfield, et al. 2007. Comparative tests of adjusted inlet in blow-down and hot-shot wind tunnels. 8th Symposium (International) on Experimental and Computational Aerothermodynamics of Internal Flows Proceedings. Lyon. ISAIF8-0049. [Google Scholar]
- Smart, M. K. 2001. Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition. J. Propul. Power 17(2):276–283. [Google Scholar]
- Smart, M. K., and C. A. Trexler. 2004. Mach 4 performance of hypersonic inlet with rectangular-to-elliptical shape transition. J. Propul. Power 20(9.2):289–293. [Google Scholar]
- Nan, X., K. Zhang, Z. Jin, and Y. Li. 2012. Start characteristics of hypersonic inlets with rectangular to circular shape transition at Ma 5 with attack angle 8.. J. Nanjing University of Aeronautics & Astronautics 44(2):146–151. (In Chinese.) [Google Scholar]
- Neaves, M. D, D. S. McRae, and J. R Edwards. 2001. High-speed inlet unstart calculations using an implicit solution adaptive mesh algorithm. AIAA Paper No. 2001-825. [Google Scholar]
- Timofeev, E. V, P. A. Voinovich, K. Takayama, R. B. Tahir, and S. Molder. 2001. Adaptive unstructured Euler simulations of hypersonic inlet flow starting. AIAA Paper No. 2001-1896. [Google Scholar]
- Yuan, H., and D. Liang. 2004. Characteristic analysis of unstart performance for hypersonic side-wall inlet model. J. Nanjing University of Aeronautics & Astronautics 36(6):683–687. (In Chinese.) [Google Scholar]
- Barber, T. J, D. Hiett, and S. Fastenberg. 2006. CFD modeling of the hypersonic inlet starting problem. AIAA Paper No. 2006-123. [Google Scholar]
- Yuan, H., and D. Liang. 2006. Analysis of characteristics of restart performance for a hypersonic inlet. J. Propul. Technol. 127(15):390–398. (In Chinese.) [Google Scholar]
- Veillard, X., R. Tahir, E. Timofeev, and S. Mölder. 2008. Limiting contractions for starting simple ramp-type scramjet intakes with overboard spillage. J. Propul. Power 24(5):1042–1049. [Google Scholar]
- He, Y., J. Wu, and A. Yu. 2014. Self-start simulation of a hypersonic inlet with variable incoming flow conditions[C]. IHFC2014-PaperList 64. [Google Scholar]
- Yu, A., and J. Le. 2005. The preliminary 2D numerical simulation research on start problem of a hypersonic inlet. 1st Chinese Conference of Hypersonic Inlets Techniques. Nanjing City, Jiangsu Province. 34–41. (In Chinese.) [Google Scholar]
- Huang, T., A. Yu, and J. Le. 2006. The research on the start characteristics of a 2D hypersonic inlet. 12th National Shock and Shock Tube Conference. Luoyang City, Henan Province. 42–46. [Google Scholar]
- Zhang, Y., G. Wang, and Y. He. 2007. Design and optimization of 2D hypersonic inlet. J Aerodynamics Phys. Theory Appl. 2:82–86. (In Chinese.) [Google Scholar]
- Yu, A., J. Le, T. Huang, and H. Ni. 2008. Experimental investigation of starting characteristics for a hypersonic inlet at Mach 4. 7th Congress of SRHRC (Sino-Russia High-Speed Flow Conference). Novosibirsk, Russia. 266. [Google Scholar]