[1] Ludwing C B, Malkmus W, Walker J, et al. A theoretical model for absorbing, emitting and scattering plume radiation. Horton T E (Ed). Spacecraft Radative Transfer and Temperature Control. New York: AIAA Progress Series in Astronautics and Aeronautics, 1982, 83: 111-127

[4] Piesik E T. Aluminized propellants and a method defining low-altitude exhaust plumes. J. of Spacecraft and Rocket, 1986, 23: 215-221

[5] Scutaru D. Measurements and calculations of CO2 absorption at high temperature in the 4.3 and 2.7μm regions. J.of Quantitative Spectroscopy and Radiative Transfer, 1993, 50(2): 179-191

[8] Thompson J F, Warsi U A, Masin C W. Numerical grid generation: Foundations and applications. New York: North-Holland, 1985,95-169

[9] Ferziger J H, Peric M. Computational Methods for Fluid Dynamics. Verlag Berlin Heidelbery: Springer, 1996, 104-107

[11] Baek S W, Kim M Y. Analysis of radiative heating of a rocket plume base with the finite volume method. Int.J.of Heat and Mass Transfer, 1997, 40(7): 1501-1508

[12] Fiveland W A. The selection of discrete ordinate quadrature sets for anisotropic scattering. ASME HTD-160, 1991, 89-96