[1]
[2] Haulman D L. USAF manned aircraft combat Losses 1990-2002 [R]. AD A434084, 2002.
[3] Mahulikar S P, Sonawance H R, Rao G A. Infrared signature studies of aero space vehicles[J]. Progress in Aerospace Sciences, 2007, 43(7): 218-245.
[4]
[5]
[6] Marlene Johansson. Propulsion Integration in an UAV[R].AIAA 2006-2834, 2006.
[7]
[8] Liu Changchun, Ji Honghu, Huang Wei, et al. Numerical simulation on infrared radiation characteristics of serpentine 2-D nozzle[J]. Journal of Aerospace Power, 2013, 28(7): 1482-1488. (in Chinese) 刘常春, 吉洪湖, 黄伟, 等. 一种双S弯二元喷管的红外辐射特性数值研究[J].航空动力学报, 2013, 28(7): 1482-1488.
[9] Zhang Yechuan, Wang Zhanxue, Shi Jingwei, et al. Analysis on flow and infrared radiation characteristics of double S-nozzle [J]. Journal of Aerospace Power, 2013, 28(11): 2468-2474. (in Chinese) 章叶川, 王占学, 史经纬, 等. 双S弯喷管流动特性及红外辐射特性分析[J].航空动力学报, 2013, 28(11): 2468-2474.
[10]
[11] Li Yuefeng, Yang Qingzhen. Huan Xia, et al. Influence on radar cross-section of S-shaped two dimensional convergent nozzles with different outlet width-height ratios[J]. Journal of Aerospace Power, 2014, 29(3): 645-651. (in Chinese) 李岳锋, 杨青真, 环夏, 等. 出口宽高比对S形二元收敛喷管雷达散射截面的影响[J]. 航空动力学报, 2014, 29(3): 645-651.
[12]
[13]
[14] Li Wei, Zhang Bo, Wang Fei, et al. Numerical simulation on infrared radiation characteristics of round to rectangular nozzles with different chevrons considering engine components[J]. Journal of Aerospace Power, 2014, 29(8): 1810-1816. (in Chinese) 李伟, 张勃, 王飞, 等. 不同锯齿对圆转矩形喷管红外辐射特征影响数值模[J]. 航空动力学报, 2014, 29(8): 1810-1816.
[15]
[16] Li Yuefeng, Yang Qingzhen, Li Xiang, et al. RCS characteristic of S-shaped nozzle with different outlet shapes[J]. Journal of Aerospace Power, 2013, 28(12): 2671-2677. (in Chinese) 李岳锋, 杨青真, 李翔, 等. 不同出口形状S形喷管的RCS特性[J]. 航空动力学报, 2013, 28(12): 2671-2677.
[17]
[18] Gao Xiang, Yang Qingzhen, Mu Hongrui. Numerical simulation of radar scattering characteristics for 2-D nozzles with different aspect ratios[J]. Journal of Propulsion Technology, 2014, 35(6): 735-741. (in Chinese) 高翔, 杨青真, 母鸿瑞. 不同宽高比的二元喷管电磁散射特性数值研究[J]. 推进技术, 2014, 35(6): 735-741.
[19] Chen Lihai, Yang Qingzhen, Chen Lingling. Numerical simulation of RCS for 2D convergent nozzle with different trailing edges[J]. Journal of Aerospace Power, 2012, 27(3): 513-520. (in Chinese) 陈立海, 杨青真, 陈玲玲. 不同喷口修形的二元收敛喷管RCS数值模拟[J]. 航空动力学报, 2012, 27(3): 513-520.
[20]
[21]
[22] Huang Wei, Ji Honghu, Si Ren. Infrared characteristics calculating of turbofan engine exhaust system[J]. Journal of Propulsion Technology, 2010, 31(6): 745-772. (in Chinese) 黄伟, 吉洪湖, 斯仁. 涡扇发动机排气系统红外特征[J]. 推进技术, 2010, 31(6): 745-772.
[23]

Wang K C. Prediction of rocket plume radioactive heating using backward monte-carlo method[R]. AIAA 93-0137, 1993.
[24]
[25]

Chen Lihai. Numerical simulation on the infrared radiation characteristics of exhaust system of the aircraft[D]. Xi'an:Northwestern Polytechnical University, 2013.
[26]
[27]

Rao G A, Mahulikar S P. Effect of atmospheric transmission and radiance on aircraft infrared signatures[J]. Journal of Aircraft, 2005, 42: 1046-1054.