Infrared and Laser Engineering, Volume. 46, Issue 2, 204004(2017)

Influence of lobed mixer on infrared character of serpentine 2-D exhaust system

Wang Ding, Ji Honghu, and Lu Haohao
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  • [in Chinese]
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    References(11)

    [1] [1] 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)

    [2] [2] 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)

    [4] [4] Zhang Jingzhou, Shan Yong, Li Liguo. Computation and validation of parameter effects on lobed mixer-ejector performances[J]. Chinese Journal of Aeronautics, 2005, 18(3): 193-198.

    [5] [5] Zhang Jingzhou, Shan Yong, Li Liguo. Investigation on lobed nozzle mixer ejector infrared suppressor for helicopter exhaust system[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(1): 32-36. (in Chinese)

    [9] [9] Du Liwei, Liu Youhong, Shao Wanren, et al. Effect of lobe number on aerothermodynamic performance of lobed S-shaped two-dimensional nozzle[J]. Journal of Aerospace Power, 2015, 30(4): 916-926. (in Chinese)

    [11] [11] Huang Wei, Ji Honghu, Si Ren, et al. Infrared characteristics calculating of turbofan engine exhaust system[J]. Journal of Propulsion Technology, 2010, 31(6): 745-750. (in Chinese)

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    Wang Ding, Ji Honghu, Lu Haohao. Influence of lobed mixer on infrared character of serpentine 2-D exhaust system[J]. Infrared and Laser Engineering, 2017, 46(2): 204004

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    Paper Information

    Category: 红外技术及应用

    Received: Jun. 6, 2016

    Accepted: Jul. 10, 2016

    Published Online: Mar. 31, 2017

    The Author Email:

    DOI:10.3788/irla201746.0204004

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