| Citation: | DU Zheng-gang, JIN Ping, YANG Li-jun, CAI Guo-biao, ZHANG Meng-zheng. Experimental investigation of flowrate characteristics of gas-gas injector[J]. Journal of Aerospace Power, 2007, 22(3): 500-504. |
| [1] |
Nagai C K.Cold-flow optimization of gaseous oxygen/gaseous hydrogen injector for the space shuttle APS thruster[R].AIAA71-673.
|
| [2] |
Smith Timothy D,Kelm Mark D,Breisacher Kevin J.Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector[R].Glenn Research Center,Cleveland,Ohio NASA/TM-2002-211982.
|
| [3] |
Foust M J,Deshpande M,Pal S.Experimental and analytical characterization of a shear coaxial combusting GO2/GH2 flowfield[R].The Pennsylvania State University,University Park,PA AIAA 96-0646.
|
| [4] |
Farhangi S,Yu T,Sprouse K.et al.Gas-gas injector technology for full flow combustion cycle application[R].AIAA 99-2757.
|
| [5] |
孙纪国.氢氧同轴式喷嘴流量特性试验和理论分析[J].航空动力学报,2005,20(4):689-691.SUN jiguo.Experimental investigation and analysis of coaxial injector discharge coefficient[J].Journal of Aerospace Power,2005,20(4):689-691.
|
| [6] |
李清廉,田章福,王振国.模型三组元喷嘴流量特性实验[J].推进技术,2002,23(4):268-272.LI Qinglian,TIAN Zhangfu,WANG Zhenguo.Experimental study of import pass ways for model tripropellant injector[J].Journal of Propulsion Technology,2002,23(4):268-272.
|
| [7] |
潘锦珊.气体动力学基础[M].北京:国防工业出版社,2000.
|
| [8] |
杨晓琼.传热学-计算机辅助教学丛书[M].西安:西安交通大学出版社,1992.
|