• Infrared and Laser Engineering
  • Vol. 50, Issue 11, 20210084 (2021)
Yuheng Wang, Honghu Ji, Wen Cheng, and Jiquan Li
Author Affiliations
  • College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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    DOI: 10.3788/IRLA20210084 Cite this Article
    Yuheng Wang, Honghu Ji, Wen Cheng, Jiquan Li. Influence of design of convergent-divergent nozzle on aerodynamic and infrared characteristics of serpentine 2-D exhaust system[J]. Infrared and Laser Engineering, 2021, 50(11): 20210084 Copy Citation Text show less
    References

    [1] Hao Wang, Honghu Ji, Xueyi Sang, et al. Effects of fully shielded guiding strut on infrared signatures of the exhaust system. Journal of Aerospace Power, 35, 2078-2088(2020).

    [2] Bo Zhang, Jingjing Li, Shuai Yuan, et al. Experimental investigation of infrared sup-pressing characteristics of different nozzles. Infrared and Laser Engineering, 46, 0404005(2017).

    [3] Xiaojuan Shi, Honghu Ji. Numerical investigation of influence of two-dimensional convergent and divergent nozzle’s design parameters on infrared characteristics. Journal of Aerospace Power, 35, 944-955(2020).

    [4] Jingzhou Zhang, Xu Wang, Yong Shan. Effects of plug rear-body film cooling on infrared radiation and aero-dynamics per-formance of axisymmetric plug nozzle. Journal of Aeronautics, 36, 2601-2608(2015).

    [5] Na Li, Honghu Ji, Wei Huang. Study on matching method for core and bypass mass flux of 2-D convergent nozzle of mixed flow. Journal of Aerospace Power, 26, 2563-2570(2011).

    [6] Bru E, Seine N S, Daris T, et al. Exhaust assembly fming a hizontal propulsion gas elbow in an aircraft: US, 007784284B2[P].20100831.

    [7] Changchun Liu, Honghu Ji. Experiment on infrared radiation characteristics of shaped 2D nozzle. Journal of Aerospace Power, 34, 1493-1500(2019).

    [8] Xueyi Sang, Honghu Ji, Ding Wang. Influence of length-diameter ratio and off-set-diameter ratio on performance of ser-pentine 2-D nozzle.. Infrared Technology, 41, 443-449(2019).

    [9] Feifei Cao, Honghu Ji, Kaijun Wu. Effects of low emissivity material coating site on wall temperature and infrared characteristics of exhaust system. Infrared and Laser Engineering, 49, 20190131(2020).

    [10] C J Rusher, A S Magstadt, M G Berry, et al. Investigation of a Supersonic Jet from a three-stream engine nozzle. AIAA Journal, 56, 1554-1568(2018).

    [11] Li Zhou, Yubo Meng, Zhanxue Wang. Numerical study on flow characteristics of serpentine convergent divergent nozzle. Journal of Propulsion Technology, 42, 103-113(2021).

    [12] Wang Ding. Research on flow acteristic infrared suppression of serpentine 2D exhaust system[D]. Nanjing: Nanjing University of Aeronautics Astronautics, 2016. (in Chinese)

    [13] Lee C C, Louis S, Boedicker M C. Subsonic diffuser design perfmance f advanced fighter aircraft[C]Aircraft Design Systems Operations Meeting, 1985.

    [14] Zhang Xiaoying. Numerical research of infrared radiation acteristics of aircraft engine exhaust system[D]. Beijing: Beijing University of Aeronautics Astronautics, 1999. (in Chinese)

    [15] Wei Huang, Honghu Ji, Ren Si, et al. Infrared characteristics calculating of turbofan engine exhaust system. Journal of Propulsion Technology, 31, 745-750(2010).

    [16] Ding Wang, Honghu Ji, Wei Huang. A serpentine 2-D exhaust system with high thrust and low infrared signature. Journal of Engineering Thermophysics, 1944-1951(2017).

    Yuheng Wang, Honghu Ji, Wen Cheng, Jiquan Li. Influence of design of convergent-divergent nozzle on aerodynamic and infrared characteristics of serpentine 2-D exhaust system[J]. Infrared and Laser Engineering, 2021, 50(11): 20210084
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