• Opto-Electronic Engineering
  • Vol. 37, Issue 10, 6 (2010)
JIN Wei1、2, LING Yong-shun3, and Lü Xiang-yin3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: Cite this Article
    JIN Wei, LING Yong-shun, Lü Xiang-yin. Numerical Simulation of the Infrared Radiation of Satellite Orbit-control Thruster Plume[J]. Opto-Electronic Engineering, 2010, 37(10): 6 Copy Citation Text show less
    References

    [1] DONG Shi-kui,YU Jian-guo,LI Dong-hui,et al. Numerical modeling of infrared radiation properties of exhaust plume by the Discrete Ordinates Method in body-fitted coordinates [J]. Journal of University of Shanghai for Science and Technology,2003,25(2):159-162.

    [2] FAN Shi-wei,ZHANG Xiao-ying,ZHU Ding-qiang,et al. Calculation of the infrared characteristics of the solid rocket plume with FVM method [J]. Journal of Astronautics,2005,26(6):793-797.

    [3] QI Xue-qin,WANG Ping-yang,ZHANG Jing-zhou,et al. Reverse Monte Carlo simulation on infrared radiation of lobed nozz1e/mixer plume [J]. Journal of Shanghai Jiao Tong University,2005,39(8):1229-1232, 1239.

    [4] RUAN Li-ming,QI Hong,WANG Sheng-gang,et al. Numerical simulation of the infrared characteristic of missile exhaust plume [J]. Infrared and Laser Engineering,2008,37(6):959-962.

    [5] Siegel R,Howell J R. Thermal Radiation Heat Transfer [M]. Washington D C:Hemisphere and McGraw-Hill,1981.

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    [7] statistical narrow-band model [J]. International Journal of Heat and Mass Transfer(S0017-9310),1998,37:759-768.

         Liu Fengshan,Güilder mer L,Smallwood Gregory J. Three-dimensional non-grey gas radiative transfer analyses using the

    [8] NIE Wan-sheng,YANG Jun-hui,HE Hao-bo,et al. The IR radiation characteristic of exhaust plume of the liquid rocket engine[J]. Journal of National University of Defense Technology,2005,27(5):91-94.

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    JIN Wei, LING Yong-shun, Lü Xiang-yin. Numerical Simulation of the Infrared Radiation of Satellite Orbit-control Thruster Plume[J]. Opto-Electronic Engineering, 2010, 37(10): 6
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