[1] [1] WANG Wei-chen, WEI Zhi-jun, ZHANG Qiao, et al. Influence of afterburning on infrared signature of rocket motor exhaust plume［J］. Journal of Aerospace Power, 2010, 25(11): 2612-2618.

[2] [2] JIANG Yi, FU De-bin. Numerical simulation for non equilibrium chemically reacting fuid field of the solid rocket motor exhaust plume［J］. Journal of Astronautics, 2008, 29(2): 615-620.

[3] [3] SURZHIKOV S T. Monte carlo simulation of plumes spectral emission［R］. Institute for Problems in Mechanics Russian Academy of Sciences (IPMech RAS), 2006.

[4] [4] LIU L H. Backward monte carlo method based on radiation distribution factor［J］. AIAA Journal of Thermophys, 2004, 18(4): 151-153.

[5] [5] 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.

[6] [6] CAI G B, ZHU D Q, ZHANG X Y. Numerical simulation of the infrared radiative signatures of liquid and solid rocket plumes［J］. Aerospace Science and Technology, 2007(11): 473-480.

[7] [7] ZHANG Xiao-ying, ZHU Ding-qiang, CAI Guo-biao. Study the infrared characteristics of the solid rocket plume with DOM method and the influence of altitude［J］. Journal of Astronautics, 2007, 28(3): 702-706.

[8] [8] ZONG Jing-guo, ZHANG Jian-qi, LIU De-lian. Infrared radiation characteristics of stealth aircraft［J］. Acta Phtonica Sinica, 2011, 40(2): 289-294.

[9] [9] TROYES J, DUBOIS I, BORIE V, et al. Multi-phase reactive numerical simulations of a model solid rocket motor exhaust jet［C］. Sacramento, California: AIAA, 2006: 2006-4414.

[10] [10] LAUNDER B E, SPALDING D B. Lectures in mathematical models of turbulence［M］. London: Academic Press, 1972.

[11] [11] WANG Wei-chen, WEI Zhi-jun, ZHANG Qiao, et al. Study on infrared signature of solid rocket motor afterburning exhaust plume［C］. Nashville, TN: AIAA, 2010: 2010-6847.

[12] [12] DONG Shi-kui, TAN He-ping, YU Qi-zheng, et al. Infrared radiative spectral band-model parameters for water vapor in the 300-3000 K temperature range［J］. Journal of Engineering for Tehrmal Energy and Power, 2001, 16(1): 33-38.

[13] [13] DONG Shi-kui, YU Qi-zheng, TAN He-ping, et al. Narrow band model parameters of high temperature radiation for carbon dioxide of combustion products［J］. Journal of Aerospace Power, 2001, 16(4): 355-359.

[14] [14] SIEGEL R, HOWELL R J. Thermal radiation heat transfer［M］. Washington D C: Hemisphere and McGraw-Hill, 1981.

[16] [16] FERZIGER H J, PERIC M. Computational methods for fluid dynamics［M］. Berlin: Springer, 1996.

[17] [17] SIMMONS F S. Rocket exhaust plume phenomenology［M］. EI Segundo: CA: The Aerospace Press and American Institute of Aeronautics and Astronautics, 2000.