[1] [1] Kang Lizhu, Zhao Jinsong, Li Zhenhua, et al. The overview of the research work developments on infrared signature of aircrafts[J]. Infrared Technology, 2017, 39(2): 105-115. (in Chinese)

[2] [2] Lv Jianwei, Wang Qiang. Numerical calculation and analysis of infrared radiation characteristics from aircraft skin by using RMC method[J]. Infrared and Laser Engineering, 2009, 38(2): 232-237. (in Chinese)

[3] [3] Wang Xingtao, Zhang Jingzhou, Shan Yong. Numerical investigation of solar radiation effects on aircraft skin infrared characteristics[J]. Journal of Propulsion Technology, 2016, 37(2): 235-241. (in Chinese)

[4] [4] Huang Wei, Ji Honghu. Effect of reflected background radiation by skin on infrared signature of subsonic aircraft (I): methodology [J]. Infrared and Laser Engineering, 2015, 44(6): 1699-1703. (in Chinese)

[5] [5] Huang Wei, Ji Honghu. Effect of reflected background radiation by skin on infrared signature of subsonic aircraft (II): application [J]. Infrared and Laser Engineering, 2015, 44(7): 2039-2043. (in Chinese)

[6] [6] Li Huihui. Research on IR suppressant of hot exhaust with the discrete particles in flight[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009. (in Chinese)

[7] [7] Feng Yunsong, Li Xiaoxia, Lu Yuan, et al. Numerical calculation of infrared radiation characteristics of the exhaust plume outside a rectangular nozzle [J]. Acta Armamentarii, 2013, 34(4): 437-442. (in Chinese)

[8] [8] Tang Heping, Xia Xingling, Liu Hualing, et al. Numerical Calculation of Infrared Radiation and Transmission-Calculation of Thermal Radiation[M]. Harbin: Harbin Institute of Technology Press, 2006: 107-118. (in Chinese)

[9] [9] Qi Xueqin, Wang Pingyang, Zhang Jingzhou, et al. Reverse Monte Carlo simulation on infrared radiation of lobed nozzle/mixer plume[J]. Journal of Shanghai Jiaotong University, 2005, 39(8): 1229-1232． (in Chinese)

[10] [10] Wang Xingtao, Zhang Jingzhou, Shan Yong. Numerical investigation of aircraft infrared characteristicsin 8-14 μm band[J]. Infrared and Laser Engineering, 2014, 43(1): 6-12. (in Chinese)

[11] [11] Wang Xingtao. Research on infrared radiation performance of air vehicle and temperature reduction disciplinarian of engine nacelle skin[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese)

[12] [12] Lin Jie, Jiang Yong, Fang Haobai, et al. Modeling and analysis on self-infrared radiation characteristics of whole aircraft skin[J]. Inrared Technology, 2012, 34(5): 286-291． (in Chinese)

[13] [13] Zhang Shengtao. The research on numerical simulation of infrared radiant properties of flow field around near space hypersonic vehicle[D]. Shanghai: Shanghai Jiaotong University, 2009. (in Chinese)

[14] [14] Lv Jianwei, Wang Qiang. Coupled analysis on flow field temperature distribution of aircraft skin[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 938-941．(in Chinese)

[15] [15] Zheng Jiansheng, Zhang Jingzhou, Shan Yong, et al. Inverstigation on aerodynamic and infrared performance of a spherical convergent two-dimensional vectoring nazzle: simulating high altitude status[J]. Journal of Aerospace,2017, 32(2): 390-397. (in Chinese)

[16] [16] Ding Liang. Research on stealth aircraft exhaust plume infrared detection simulation technique[D]. Chengdu: University of Electronic Science and Technology, 2016. (in Chinese)