[1] S P Mahulikar, H R Sonawane, G A Rao. Infrared signature studies of aerospace vehicles. Progress in Aerospace Sciences, 43, 218-245(2007).

[2] G A Rao, S P Mahulikar. Integrated review of stealth technology and its role in airpower. The Aeronautical Journal, 106, 629-642(2002).

[3] H R Sonawane, S P Mahulikar. Tactical air warfare: Generic model for aircraft susceptibility to infrared guided missiles. Aerospace Science and Technology, 15, 249-260(2011).

[4] G A Rao, S P Mahulikar. New criterion for aircraft susceptibility to infrared guided missiles. Aerospace Science and Technology, 9, 701-712(2005).

[5] S P Mahulikar, H S S Prasad, S K Potnuru. Infrared signature suppression of helicopter engine duct based on" conceal and camouflage". Journal of Propulsion and Power, 24, 613-618(2008).

[6] Xinbo Song, Xueyan Lv, Jianjun Zhang. Study on the infrared stealth technology of plane. Laser & Infrared, 42, 3-7(2012).

[7] A Rogalski. Competitive technologies of third generation infrared photon detectors. Opto-electronics Review, 14, 84-98(2006).

[8] Xianwei Wang, Zhonghai Sun, Chuanshu Kuang. The anatomy of RAH-66 helicopter infrared suppressor. Helicopter Technique, 37, 23-28(2008).

[9] [9] Skebe S, Paterson R, Barber T. Experimental investigation of threedimensional fced mixer lobe flow fields [C]1st National Fluid Dynamics Conference, 1988: 3785.

[10] K Zaman, F Y Wang, N J Georgiadis. Noise, turbulence, and thrust of subsonic freejets from lobed nozzles. AIAA Journal, 41, 398-407(2003).

[11] Tonghui Wang, Xianwei Wang, Jingzhou Zhang, . Effect of covering shelter on infrared radiation characteristics of helicopter infrared radiation suppressor. Journal of Aerospace Power, 24, 1493-1499(2009).

[12] [12] Presz W, Werle M. Multistage mixereject systems [C]38 th AIAAASMESAEASEE Joint Propulsion Conference & Exhibit, 2002: 4064.

[13] Lifeng Ren, Jingzhou Zhang, Xianwei Wang, . Analysis of stealth properties on IR radiation suppressor embed inside helicopter rear airframe. Infrared and Laser Engineering, 40, 2091-2097(2011).

[14] Geng Chen, Xiaoming Tan, Yong Shan, . Impacts of two-dimensional curved mixing duct exit geometric parameters on flow dynamics and infrared radiation characteristics for IR suppressor. Infrared and Laser Engineering, 44, 1704-1711(2015).

[15] [15] Zheng Zhen. Research on structure of mixing duct in helicopter infrared suppress[D]. Nanjing: Nanjing University of Aeronautics Astronautics, 2020. (in Chinese)

[16] Kunhong Jiang, Jingzhou Zhang, Yong Shan, . Effects of sheltering and outlet shaping on surface temperature and infrared radiation characteristics of rear airframe with an intedrating infrared suppressor. Acta Aeronautica et Astronautica Sinica, 41, 152-162(2020).

[17] Zhongyao Yang, Jingzhou Zhang, Yong Shan. Effects of forward-flight speed on plume flow and infrared radiation of IRS-integrating helicopter. Chinese Journal of Aeronautics, 35, 155-168(2022).

[18] Chengxiong Pan, Jingzhou Zhang, Yong Shan. Modeling and analysis of helicopter thermal and infrared radiation. Chinese Journal of Aeronautics, 24, 558-567(2011).

[19] [19] Liu J. Investigation on infrared signatures of axisymmetric vecting exhaust nozzle effectiveness evaluation of aircraft infrared stealth[D]. Nanjing: Nanjing University of Aeronautics Astronautics, 2017. (in Chinese)