[1] Honghu Ji. Fundamental issues of aircraft/engine integration for low observability. Aerospace Power, 67-71(2018).

[2] Hongwei Deng, Shoutang Shang, Hai Jin, . Analysis and discussion on stealth technology of aero engine. Aeronautical Science and Technology, 28, 1-7(2017).

[3] Jun Chen, Honghu Ji, Ren Si, . Experiment of IR suppression for nozzle with low infrared emissivity coating. Infrared Technology, 33, 395-400(2011).

[4] Jian Liu, Honghu Ji. Investigation on infrared signature of axisymmetric vectoring exhaust system with film cooling and low-emissivity coating. AIAA Journal of Thermophysics and Heat Transfer, 32, 627-636(2018).

[5] Ding Wang, Honghu Ji. Model experiment and numerical analysis on in infrared character of lobed mixer exhaust system. Infrared and Laser Engineering, 46, 0104003(2017).

[6] Lifeng Ren, Wanren Shao, Su Xu, . Numerical study of infrared radiation characteristics for aero-engine exhaust system. Gas Turbine Experiment and Research, 31, 19-24, 52(2018).

[7] Haiyang Hu, Qiang Wang. Calculation of wall temperature for aircraft exhaust system with considering gas radiation heat transfer. Chinese Journal of Aeronautics, 22, 590-598, 707(2009).

[9] Xiaoyu Liu, Yong Jiang, Zu Li, . Numerical research on infrared radiation characteristics and infrared restraint of aero-engine. Infrared and Laser Engineering, 43, 2482-2488(2014).

[10] Haohao Lu, Honghu Ji, Ding Wang, . Experiment on infrared characteristics suppression by component cooling of two-dimensional convergent-divergent vectoring nozzle exhaust system. Journal of Aerospace Power, 32, 2070-2079(2017).

[11] Haohao Lu, Honghu Ji, Jian Liu, . Experiment on infrared signature of two dimensional convergent-divergent vectoring nozzle exhaust system. Journal of Aerospace Power, 32, 1861-1868(2017).