[1] Levin D A. Multi spectral shock layer radiance from a hypersonic slender body[R]. AIAA 99-3747, 1999.

[2] Park C. Calculation of non-equilibrium radiation in AOTV flight regimes[R]. AIAA Paper 84-0306, 1984.

[3] Park C. Radiation enhancement by nonequilibrium in Earth’s atmosphere [J]. Journal of Spacecraft and Rockets, 1985,22(1): 27-36.

[4] Gocken T. N2-CH4-Ar chemical reaction model for simulations of atmospheric entry to Titan[R]. AIAA Paper 2004-2469, 2004.

[5] Park C. Assessment of two-temperature kinetic model for dissociating and weakly ionizing nitrogen [J]. Journal of Thermophysics and Heat Transfer, 1988,2(1): 8-16.

[6] Park C. Assessment of two-temperature kinetic model for ionizing air [J]. Journal of Thermophysics and Heat Transfer, 1989, 3(3): 233-244.

[7] Gnoffo P A, Gupta R N, Shinn J L. Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium[R]. NASA TP-2867, 1989.

[8] Hartung L C, Mitcheltree R A, Gnoffo P A. Stagnation point nonequilibrium radiative heating and the influence of energy exchange models [J]. Journal Thermophysics and Heat Transfer, 1992, 6(3): 412-418.

[9] Hartung L C. Development of a nonequilibrium radiative heating prediction method for coupled flowfield solutions [J]. Journal Thermophysics and Heat Transfer, 1992, 6(4): 618-625.

[10] Gally T A. Development of engineering methods for nonequilibrium radiative phenomena about aeroassisted entry vehicles [D]. College Station: Texas A&M University, 1992.

[11] Sharma S. Assessment of nonequilibrium radiation computational methods for hypersonic flows [R]. NASA TM-103994, 1993.

[12] Sharma S. Modeling of nonequilibrium radiation phenomena: an assessment [J]. Journal of Thermophysics and Heat Transfer, 1996, 10(3): 385-396.

[13] 杜磊, 赵剡, 安永泉, 等. 高超声速激波辐射对红外成像系统的影响分析[J]. 红外与激光工程, 2012, 41(2):291-296. (Du Lei, Zhao Yan, An Yongquan, et al. Analysis of hypersonic shock layer radiance effect on an IR imaging system. Infrared and Laser Engineering, 2012, 41(2): 291-296)

[14] 王亚辉, 王强, 高磊, 等. 高超声速飞行器气动热辐射特性[J]. 红外与激光工程, 2013, 42(6): 1399-1403. (Wang Yahui, Wang Qiang, Gao Lei, et al. Aero-thermo-radiation of a hypersonic vehicle. Infrared and Laser Engineering, 2013, 42(6): 1399-1403)

[15] Johnston C O. Nonequilibrium shock-layer radiative heating for earth and titan entry [D]. Blacksburg: Virginia Polytechnic Institute and State University, 2006.

[16] 胡兰芳. 高速飞行器非平衡绕流及光辐射特性模拟[D]. 哈尔滨: 哈尔滨工业大学, 2011. (Hu Lanfang. Numerically simulation of non-equilibrium flow and optical radiation characteristic of hypersonic vehicle. Harbin: Harbin Institute of Technology, 2011)