刘国球.液体火箭发动机原理[M].北京:中国宇航出版社,2005. Liu Guoqiu. Principle of liquid rocket motor[M]. Beijing: China Astronautic Publishing House, 2005. (in Chinese)
[2]
Plastinin Y, Karabadzhak G, Khmelinin B, et al. Ultraviolet, visible and infrared spectral modeling for solid and liquid-fuel rocket exhausts //Proceedings of 39th Aerospace Sciences Meeting & Exhibit. Reno: AIAA, 2001:1651001-1651015.
[3]
Roblin A, Dubois I, Grisch F, et al. Comparison between computations and measurements of a H2/LOX rocket motor plume //Proceedings of 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. St. Louis: AIAA, 2002:310701-310710.
[4]
Roblin A, Baudoux P, Chervet P. UV missile plume signatures model[J]. SPIE, 2002,4718:344-355.
[5]
Turns S R. An introduction to combustion[M]. Singapore: McGraw-Hill Companies, 2000.
[6]
Fluent Inc. Fluent 6.3 user guide . http://my.fit.edu/intre-source/manuals/fluent6.3/help/html/ug/main_pre.htm.
[7]
Fiveland W A. Jamaluddin A S. Three-dimensional spectral radiative heat transfer solution by the discrete-ordinates method[J]. Journal of Thermophysics, 1991,5(3):335-339.
[8]
Rothman L S, Gorden I E, Barbe B, et al. The HITRAN 2008 molecular spectroscopic database[J]. Journal of Quantitative Spectroscopy and Radiative Transfer, 2009,110:533-572.