[1] Chen Wei, Wang Zhongxian, Ma Donghui, et al. The infrared radiation characteristic calculation and simulation of non-uniform heat gas [J]. Infrared and Laser Engineering, 2010, 39(1): 18-20. (in Chinese) 陈卫, 汪中贤, 马东辉, 等. 非均匀热气体红外辐射特性计 算与仿真[J]. 红外与激光工程, 2010, 39(1): 18-20.
[2]
[3]
[4] Liu Zhen. Engine plume analysis based missile warning [J]. Land-Based Air Defence Weapons, 2006, 3: 20-22. (in Chinese) 刘真. 基于导弹预警的发动机羽流流场分析[J]. 地面防空 武器, 2006, 3: 20-22.
[5] Qin Si, He Xuzhao, Zeng Xuejun, et al. The simulation study on hypersonic vehicle tail plume [C]//The fifteenth National Conference of Shock and Shock Tube, 2012: 253-257. (in Chinese) 秦思, 贺旭照, 曾学军, 等. 高超声速飞行器后体尾喷焰数 值模拟研究[C]//第十五届全国激波与激波管学术会议, 2012: 253-257.
[6]
[7]
[8] Song Hua, Cai Timin, Li Bin. Three-dimensional numerical study on space launch rocket plume impact flow field [J]. Science Technology and Engineering, 2012, 12 (26): 6716-6718. (in Chinese) 宋华, 蔡体敏, 李彬. 航天发射火箭尾焰冲击流场三维数 值研究[J]. 科学技术与工程, 2012, 12(26): 6716-6718.
[9]
[10] Chu Hongwei, Xu Xiaojian. Theoretical computation of the infrared radiation from rocket plume [J]. Infrared and Laser Engineering, 2012, 41(1): 11-14. (in Chinese) 褚宏伟, 许小剑. 火箭尾喷焰红外辐射特性的理论计算[J]. 红外与激光工程, 2012, 41(1): 11-14.
[11]
[12] Xu Aihua, Wang Zhongxian, Yu Jian, et al. Numerical simulation of infrared radiation characteristics for plume of the high-altitude and high-speed UAV [J]. Infrared and Laser Engineering, 2012, 41(7): 1071-1073. (in Chinese) 许爱华,汪中贤,于坚, 等. 高空高速无人机尾焰红外辐 射特性计算研究[J]. 红外与激光工程, 2012, 41 (7): 1071-1073.
[13] Zhang Guangxi, Zhou Weimin, Zhang Gangchui, et al. Research on exhaust plume flow field characteristics of solid rocket engine [J]. Solid Rocket Technology, 2008, 31 (1): 20-23. (in Chinese) 张光喜,周为民, 张钢锤, 等. 固体火箭发动机尾焰流场 特性研究[J]. 固体火箭技术, 2008, 31(1): 20-23.
[14]
[15] Wang Mingdong, Tang Bin. Research on rocket tail plume flow field [J]. Journal of Institute of Command and Technology, 2001, 12(6): 104-107. (in Chinese) 王明东, 唐斌. 火箭尾喷焰流场的研究[J]. 指挥技术学院 学报, 2001, 12(6): 104-107.