Cold-flow tests on 1-cell 2D linear plug nozzle

[1] Silver R. Final report, advanced aerodynamic spike configurations:volum1, analytical and cold flow studies . USA:Rockwell International Corporation, Rocketdyne Division, Report AFRPL-TR-67-246-Vol I, 1967 [2] Tomita T, Takahashi M, Onodera T. Visualization of shock wave interaction on the surface of clustered plug nozzles . AIAA Paper 98-3523,1998 [3] Sakamoto H, Takahashi M, Sasaki M, et al. An experimental study on a 14 kN linear aerospike nozzle combustor . AIAA Paper 99-2761,1999 [4] Onofri M. Plug nozzles:summary of flow features and engine performance . AIAA Paper 2002-0584,2002 [5] 戴梧叶. 塞式喷管的实验与数值模拟研究 . 北京:北京航空航天大学 航学院,2002 Dai Wuye. Experimental and numerical studies of aerospike nozzles . Beijing:School of Astronautics, Beijing University of Aeronautics and Astronautics, 2002(in Chinese) [6] 覃粒子, 刘 宇, 王一白. 塞式喷管多参数性能优化计算[J] 宇航学报, 2002, 23(2):28~33 Qin Lizi, Liu Yu, Wang Yibai. Optimized performance calculation in multi-parameter for aerospike nozzle [J] Journal of Astronautics, 2002, 23(2):28~33(in Chinese) [7] 戴梧叶, 刘 宇, 马 彬. 瓦状塞式喷管冷流实验研究[J] 推进技术, 2002, 23(5):420~424 Dai Wuye, Liu Yu, Ma Bin. Cold-flow tests on tile-shaped aerospike nozzle . Journal of Propulsion Technology, 2002, 23(5):420~424(in Chinese)