• Infrared and Laser Engineering
  • Vol. 47, Issue 9, 904003 (2018)
Li Xia1、2、3, Liu Jianguo1, Wang Jun2、3, and Liu Xingrun2、3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3788/irla201847.0904003 Cite this Article
    Li Xia, Liu Jianguo, Wang Jun, Liu Xingrun. Afterburning and infrared radiation effects of exhaust plumes for solid rocket motors[J]. Infrared and Laser Engineering, 2018, 47(9): 904003 Copy Citation Text show less
    References

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    [9] Li Jianxun, Tong Zhongxiang, Liu Wanjun, et al. Infrared radiation characteristic experiment and simulation of aero engine[J]. Infrared and Laser Engineering, 2013, 42(3): 550-553. (in Chinese)

    [10] Leone D M, Turns S R. Active Chlorine and nitric oxide formation from chemical rocket plume afterburning[R]. AIAA 94-0788,1994.

    [11] Liu Zunyang, Shao Li, Wang Yafu, et al. Influence on afterburning on infrared radiation of solid rocket exhaust Plume[J]. Acta Optica Sinaca, 2013, 33(6): 0604001. (in Chinese)

    [12] Ruan Liming, Qi Hong, Wang Shenggang, et al. Numerical simulation of the infrared characteristic of missile exhaust plume[J]. Infrared and Laser Engineering, 2008, 37(6): 959-962. (in Chinese)

    [13] Dong Shikui, Shuai Yong, Tan Heping, et al. Computation of radiative heat transfer in participating media using Backward Monte Carlo method[J]. Journal of Harbin Institute of Technolog, 2004, 36(12): 1602-1604. (in Chinese)

    [14] Shuai Yong, Dong Shikui, Liu Linhua. Simulation of infrared radiation characteristics of high temperature free stream flow including particles by using backward Monte-Carlo method[J]. Journal of Infrared and Millimeter Waves, 2005, 24(2): 100-104. (in Chinese)

    [15] Tan Heping, Xia Xinlin, Liu Linhua, et al. Numerical Computation of Infrared Radiation Characteristics and Transmission: Computational Radiation[M]. Harbin: Harbin Institute of Technology Press, 2006: 147. (in Chinese)

    Li Xia, Liu Jianguo, Wang Jun, Liu Xingrun. Afterburning and infrared radiation effects of exhaust plumes for solid rocket motors[J]. Infrared and Laser Engineering, 2018, 47(9): 904003
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