Citation: | Liu Yu, Zhang Zhengke, Cheng Xianchen, et al. Experimental and Numerical Studies on Aerospike Nozzles[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6): 676-679. (in Chinese) |
1. 左克罗M J,霍夫曼J D.气体动力学(上、下册).王汝诵等译.北京:国防工业出版社,1984 2. Rao G V R. Exhaust nozzle contour for optimum thrust. Jet Propulsion, 1958,28(6):377~382 3. Sauer R.General characteristic of the flow through nozzles at near critical speeds. NACA TM No.1147,1947 4. 刘 宇.火箭发动机内流场计算.北京航空航天大学博士后研究报告,1994 5. 张正科.多部件复杂飞行器分块网格生成及其大迎角绕流场Euler方程分区解.北京航空航天大学博士后研究报告,1996
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