Abstract：The characteristics of supersonic cold flows over cavities were investigated experimentally and numerically, and the effects of cavities of different sizes on supersonic flow field were analyzed. The results indicate that the ratio
出版日期: 2008-12-05
引用本文:
. Supersonic flows over cavities[J]. Frontiers of Energy and Power Engineering in China, 2008, 2(4): 528-533.
FANG Tianwen, DING Meng, ZHOU Jin. Supersonic flows over cavities. Front. Energy, 2008, 2(4): 528-533.
Ben-Yakar A, Hanson R K . Cavity flame-holders forignition and flame stabilization in scramjets: An overview. Journal of Propulsion and Power, 2001, 17(4): 869–877. doi:10.2514/2.5818
2
Gruber M R, Baurle R A, Mathur T, et al.. Fundamental studies of cavity-based flameholderconcepts for supersonic combustors. Journalof Propulsion and Power, 2001, 17(1): 146–153. doi:10.2514/2.5720
3
Mathur T, Gruber M, Jackson K, et al.. Supersonic combustion experiments with a cavity-basedfuel injector. Journal of Propulsion andPower, 2001, 17(6): 1305–1312. doi:10.2514/2.5879
4
Ding Meng, Wang Zhen-guo . Experimental Investigationof drag of cavity flame holder. Acta Aeronauticaet Astronautica Sinica, 2006, 27(4): 556–560 (in Chinese)
5
Lai Lin . Investigation of spray and flowfield characteristics of cavity-basedscramjet engine. Dissertation for the Doctoral Degree.Changsha: National Universityof Defense Technology, 2003 (in Chinese)
6
Sun Mingbo, Liang Jianhan, Wang Zhenguo . Hybrid RANS/LES simulation of the supersonic flow overtwo-dimensional cavities. Journal of PropulsionTechnology, 2006, 27(2): 119–123 (in Chinese)
