Citation: | Xiao Yingchao, Tang Haibin, Liu Yuet al. Numerical study on hydrazine arcjet thruster working exchangeability[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(09): 831-834. (in Chinese) |
[1] Capecchi G. Numerical model of equilibrium composition and transport coefficients of hydrazine under dissociation and ionization .AIAA-94-2868,1994 [2] 汤海滨.电弧喷射推力器数值模拟与实验研究 .北京:北京航空航天大学宇航学院,2001 Tang Haibin. Numerical simulation and experimental study on arcjet thrusters .Beijing:School of Astronautics, Beijing University of Aeronautics and Astronautics, 2001(in Chinese) [3] Rhodes R P, Keefer D. Numerical modeling of an arcjet thruster .AIAA-90-2614,1990 [4] 陶文铨.数值传热学[M].西安:西安交通大学出版社,1988 Tao Wenquan. Numerical heat transfer[M].Xi’an:Xi’an Jiao Tong University Press,1998(in Chinese) [5] Fujita K. Performance computation of a low-power hydrogen arcjet .AIAA-96-3183,1996
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