[1] 施红辉, 王柏懿, 戴振卿. 水下超声速气体射流的力学机制研究[J]. 中国科学:物理学力学天文学, 2010, 40(1): 92-100.
[2] 王柏懿, 戴振卿, 戚隆溪, 等. 水下超声速气体射流回击现象的实验研究[J]. 力学学报, 2007, 39(2): 267-272.
[3] 朱卫兵, 陈宏, 黄舜. 水下高速射流气泡变化过程数值研究[J]. 推进技术, 2010, 31(4): 496-502. (ZHU Wei-bing, CHEN Hong, HUANG Shun. Numerical Study of the Process of the Evolution of Bubble of High-Speed Jet Underwater[J]. Journal of Propulsion Technology, 2010, 31(4): 496-502.)
[4] TANG Jia-ning, WANG Ning-fei, Shyy W. Flow Structures of Gaseous Jets Injected into Water for Underwater Propulsion[J]. Acta Mechanica Sinica, 2011, 27(4): 461-472.
[5] 何淼生, 覃粒子, 何佳磊, 等. 水下超声速喷嘴起动/关机过程射流的动态不稳定性研究[J]. 推进技术, 2014, 35(4): 523-529. (HE Miao-sheng, QIN Li-zi, HE Jia-lei, et al. Instability of a Transient Submerged Jet in Supersonic Nozzle During Its Start-Up and Shut-Down Process[J]. Journal of Propulsion Technology, 2014, 35(4): 523-529.)
[6] YU Yong-gang, CHANG Xue-xia, ZHAO Na, et al. Study of Bulk-Loaded Liquid Propellant Combustion Propulsion Processes with Stepped-Wall Combustion Chamber[J]. Journal of Applied Mechanics, 2011, 78(5): 051001-051008.
[7] YU Yong-gang, YAN Shan-heng, LU Xin, et al. Study on Expansion Process and Interaction of High Speed Twin Combustion-Gas Jets in Liquid[J]. Journal of Applied Mechanics, 2010, 77(5): 051404-1~7.
[8] 莽珊珊, 余永刚. 高压燃气射流在整装液体中扩展过程的实验和数值模拟[J]. 爆炸与冲击, 2011, 31(3): 300-305.
[9] 莽珊珊, 余永刚. 高压热气流与整装式液体工质相互作用的实验研究[J]. 工程热物理学报, 2009, 30(12): 2017-2020.
[10] XUE Xiao-chun, YU Yong-gang, ZHANG Qi. Expansion Characteristics of Twin Combustion Gas Jets with High Pressure in Cylindrical Filling Liquid Chamber[J].Journal of Hydrodynamics, 2013, 25(5): 763-771.
[11] XUE Xiao-chun, YU Yong-gang, ZHANG Qi. Study on Expansion Characteristic of Twin Combustion Gas Jets in Five-Stage Cylindrical Stepped-Wall Observation Chamber[J]. Flow Turbulence and Combustion, 2013, 91(1): 139-155.
[12] Wilson K J, Gutmark E, Schadow K C, et al. Supersonic Submerged Heated Jets[R]. AIAA 92-3138.
[13] Vaibhav K Arghode, Ashwani K Gupta. Jet Characteristics from a Submerged Combustion System[J]. Applied Energy, 2012, 89(1): 246-253.
[14] Rembold B, Adams N A, Kleiser L. Direct Numerical Simulation of a Transitional Rectangular Jet[J]. International Journal of Heat and Fluid Flow, 2002, 23(5): 547-553.
[15] 蒋平, 郭印诚, 张会强, 等. 矩形射流流动的大涡模拟[J]. 清华大学学报(自然科学版), 2004, 44(5): 689-692.
[16] Faghani Ehsan, Maddahian Reza, Faghani Pedram, et al. Numerical Investigation of Turbulent Free Jet Flows Issuing from Rectangular Nozzles: The Influence of Small Aspect Ratio[J]. Archive of Applied Mechanics, 2010, 80(7): 727-745.
[17] WANG P C, Mcguirk J J. Large Eddy Simulation of Supersonic Jet Plumes from Rectangular Con-Di Nozzles[J]. International Journal of Heat and Fluid Flow, 2013, 43: 62-73.
[18] CHEN Nan, YU Hui-dan. Mechanism of Axis Switching in Low Aspect-Ratio Rectangular Jets[J]. Computers & Mathematics with Applications, 2014, 67(2): 437-444.
[19] 王诚, 叶取源, 何友声. 导弹水下发射燃气泡计算[J]. 应用力学学报, 1997, 14(3): 3-9.(编辑:史亚红) * 收稿日期:2015-08-11;修订日期:2015-11-26。基金项目:国家自然科学基金项目(11372139)。作者简介:胡志涛,男,博士生,研究领域为含能液体燃烧推进理论与技术。E-mail: starry_dust@163.com
|