[1] Haulman D L. USAF manned aircraft combat Losses 1990-2002 [R]. AD A434084, 2002.

[2] 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.

[3] Marlene Johansson. Propulsion Integration in an UAV[R].AIAA 2006-2834, 2006.

[4] 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)

[5] 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)

[6] 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)

[7] 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)

[8] 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)

[9] 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)

[10] 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)

[11] 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)

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

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

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