[1] 邵业涛, 王健平, 唐新猛, 等.连续爆轰发动机的二维数值模拟研究[J]. 航空动力学报, 2009, 24(5): 980-986.
[2] 邵业涛, 刘勐, 王健平. 圆柱坐标系下连续旋转爆轰发动机的数值模拟[J]. 推进技术, 2009, 30(6): 717-721.(SHAO Ye-tao, LIU Meng, WANG Jian-ping. Numerical Simulation of Continuous Rotating Detonation Engine in Column Coordinate[J]. Journal of Propulsion Technology, 2009, 30(6): 717-721.)
[3] Tang Xin-Meng,Shao Ye-Tao,Wang Jian-Ping. Three-Dimensional Numerical Simulation of Rotating Detonation Engine with the Hollow Combustion Chamber[C]. Big Island, Hawaii: Seventh International Conference on Computational Fluid Dynamics (ICCFD7), 2012.
[4] 邵业涛, 王健平, 唐新猛, 等. 连续旋转爆轰发动机流场三维数值模拟[J]. 航空动力学报, 2010, 25(8): 1717-1722.
[5] 张旭东, 范宝春, 潘振华, 等. 旋转爆轰胞格结构的实验和数值研究[J]. 爆炸与冲击, 2011, 31(4): 337-342.
[6] 张旭东, 范宝春, 潘振华, 等. 旋转爆轰自持机理的数值研究[J]. 弹道学报, 2011, 23(1): 1-8.
[7] 姜孝海, 范宝春, 董刚, 等. 旋转爆轰流场的数值模拟[J]. 推进技术, 2007, 28(4): 403-407.(JIANG Xiao-hai, FAN Bao-chun, DONG Gang, et al. Numerical Investigation on the Flow Field of Rotating Detonation Wave[J].Journal of Propulsion Technology, 2007, 28(4): 403-407.)
[8] 归明月, 范宝春, 张旭东, 等. 旋转爆轰的三维数值模拟[J]. 推进技术, 2010, 31(1): 82-86.(GUI Ming-yue, FAN Bao-chun, ZHANG Xu-dong, et al. Three-Dimensional Simulation of Continuous Spin Detonation[J]. Journal of Propulsion Technology, 2010, 31(1): 82-86.)
[9] Hishida M, Fujiwara T, Wolansk P. Fundamentals of Rotating Detonations[J]. Shock Waves, 2009, 19: 1-10.
[10] Uemura Y, Hayashi A K, Asahara M, et.al. Transverse Wave Generation Mechanism in Rotating Detonation[J]. Proceedings of the Combustion Institute, 2013, 34(2).
[11] 王春, 姜宗林, 韩肇元. 爆轰波不稳定性的自激振荡机理研究[C]. 安徽, 黄山: 第十四届全国激波与激波管学术会议, 2010.
[12] 滕宏辉, 刘云峰, 姜宗林. 一维脉冲爆轰波的能量释放规律研究[J]. 空气动力学学报, 2012, 30: 731-736.
[13] Hayashi A K, Kimura Y, Yamada T, et al. Sensitivity Analysis of Rotating Detonation Engine with a Detailed Reaction Model[R]. AIAA 2009-0633.
[14] LIU Shi-Jie, LIN Zhi-Yong, SUN Ming-Bo, et al. Thrust Vectoring of a Continuous Rotating Detonation Engine by Changing the Local Injection Pressure[J]. Chinese Physics?Letter, 2011, 28(9).
[15] Davidenko D M, G?kalp I, Kudryavtsev A N. Numerical Simulation of the Contimuous Rotation Hydrogen-Oxygen Detonation with a Detailed Chemical Mechanism[C]. Moscow, Russia: West-East High Speed Flow Field Conference, 2007.
[16] Schwer D, Kailasanath K. Numerical Investigation of the Physics of Rotating-Detonation-Engines[J].Proceedings of the Combustion Institute, 2011, 33(2): 2195-2202.
[17] Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous Spin Detonation of Hydrogen-Oxygen Mixtures.1. Annular Cylindrical Combustors[J]. Combustion, Explosion, and Shock Waves, 2008, 44(2): 150-162.
[18] Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous Spin Detonation in Annular Combustors[J]. Combustion, Explosion, and Shock Waves, 2005, 41(4): 449-459.
[19] Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous Spin Detonation of Hydrogen-Oxygen Mixtures.2. Combustor with an Expanding Annular Channel[J]. Combustion, Explosion, and Shock Waves, 2008, 44(3): 330-342.
[20] Kindracki J, Wola'nski P, Gut Z. Experimental Research on the Rotating Detonation in Gaseous Fuels-Oxygen Mixtures[J]. Shock Waves, 2011, 21(2): 75-84.
[21] 马虎, 武晓松, 王栋, 等. 旋转爆震发动机数值研究[J]. 推进技术, 2012, 33(5): 820-825.(MA Hu, WU Xiao-song, WANG Dong, et al. Numerical Investigation for Rotating Detonation Engine[J]. Journal of Propulsion Technology, 2012, 33(5): 820-825.)
[22] Wolan'ski P. Detonative Propulsion [J]. Proceedings of the Combustion Institute, 2013, 34(1): 125-158.(编辑:史亚红) 收稿日期:2013-10-31;修订日期:2013-11-28。作者简介:刘倩(1987—),女,博士生,研究领域为旋转爆轰燃烧。E-mail:liuqian_mingbai@163.com
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