[1] 严传俊, 范玮, 等. 脉冲爆震发动机原理及关键技术[M]. 西安:西北工业大学出版社, 2005.
[2] Roy G D, Frolov S M, Borisov A A, et al. Pulsed Detonation Propulsion: Challenges, Current Status, and Future Perspective[J]. Progress in Energy and Combustion Science, 2004, (30): 545-672.
[3] Kishige H,Teshima K,Nishida M. Focusing of Shock Waves Reflected from and Axisymmetric Parabolic Wall[J]. Shock Waves, 1991, (1): 341-345.
[4] Izumi K, Aso S, Nishida M. Experimental and Computational Studies Focusing Processes of Shock Waves Reflected from Parabolic Reflectors[J]. Shock Waves 1994, (3): 213-222.
[5] Liang S M, Wu L N , Hsu R L. Numerical Investigation of Axisymmetric Shock Wave Focusing over Paraboloidal Reflectors[J]. Shock Waves, 1999, 9: 367-379.
[6] Shugaev F V, Serov A O , Shtemenko L S. Formation of a Jet and Vortices Behind a Shock Wave Reflected from a Concave Body[J]. Shock Waves, 1999, 9: 31-35.
[7] Gr?nig H. Past,Present and Future of Shock Focusing Research[J]. Proc.of the Int, 1989: 1-37.
[8] Chan C K, Lau D, Thibault P A, et al. Ignition and Detonation Initiation by Shock Focusing[C]. AIP Conference Proceedings, 1989: 161-166.
[9] Gelfand1 B E, Khomik1 S V, Bartenev A M. Detonation and Deflagration Initiation at the Focusing of Shock Waves in Combustible Gaseous Mixture[J]. Shock Waves, 2000, (10): 197-204.
[10] Achasov O V, Penyazkov O G. Some Gasdynamic Method for Control of Detonation Initiation and Propagation[C]. Moscow: High-Speed Deflagration and Detonation: Fundamentals and Control, 2001: 31-44.
[11] Chiping Li, Kailasanath K. Detonation Initiation by Annular-Jet-Induced Imploding Shocks[J]. Journal of Propulsion and Power, 2005,21(1): 183-186.
[12] Jackson S I, Shepherd J E. Detonation Initiation via Imploding Shock Waves[R]. AIAA 2004-3919
[13] Jackson S I, Shepherd J E. Detonation Initiation in a Tube via Imploding Toroidal Shock Waves[J]. AIAA Journal, 2008, 46(9): 2357-2367.
[14] Levin V A, Nechaev J N, Tarasov A I. A New Approach to Organizing Operation Cycles in Pulse Detonation Engines[C]. Moscow: High-Speed Deflagration and Detonation: Fundamentals and Control, 2001.
[15] Ivett A Leyva, Venkat Tangirala, Anthony J Dean. Investigation of Unsteady Flow Field in a 2-Stage PDE Resonator[R]. AIAA 2003-0715.
[16] Keith R McManus, Anthony J Dean. Experiment Evaluation of a Two-Stage Pulse Detonation Combustor[R]. AIAA 2005-3773.
[17] 王栋. 脉冲爆震发动机工作过程数值模拟研究[D]. 南京:南京理工大学, 2007.
[18] 姜日红, 武晓松, 王栋. 共振型PDE谐振腔喷嘴匹配关系研究[J]. 航空动力学报, 2009, 24(5).
[19] 李海鹏, 何立明, 陈鑫, 等. 凹面腔内激波聚焦起爆爆震波过程的数值模拟[J]. 推进技术, 2010, 31(1): 87-91. (LI Hai-Peng, HE Ling-Ming, CHEN Xin, et al. Numerical Investigation of Detonation Initiation by Shock Wave Focusing over Parabolic Reflector[J]. Journal of Propulsion Technology, 2010, 31(1): 87-91.)
[20] 王春, 司徒明, 韩肇元. 用于爆震引燃的激波聚焦无反应流场数值模拟[J]. 推进技术, 2003, 24(2): 156-159. (WANG Chun, SITU Ming, HAN Zhao-yuan. Numerical Investigations on Cold Flow Fields of Shock Focusing for Ignition of Pulse Detonation[J]. Journal of Propulsion Technology, 2003, 24(2): 156-159.)
[21] Kee R J, Rupley F M, Miller J A, et al. CHEMKIN Release 4.0[M]. San Diego,CA: Reaction Design, Inc., 2004.(编辑:史亚红) 收稿日期:2013-12-22;修订日期:2014-03-13。基金项目:国家自然科学基金青年科学基金(51106178)。作者简介:李海鹏(1981—) 男,博士,工程师,研究领域为航空宇航推进。E-mail: lhp1210@163.com
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