Citation: | Li Mao, Gao Yushan, Jin Ping, et al. Effects of propellants temperature in gas-gas injector inleton combustion performance and wall temperature[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(9): 1091-1094,1099. (in Chinese) |
[1] Davis J A,Campbell R L.Advantages of a full-flow staged combustion cycle engine system[R].AIAA 97-3318,1997 [2] Farhangi S,Yu T,Rojas L,et al.Gas-gas injector technology for full flow stage combustion cycle application[R].AIAA 99-2757,1999 [3] Hueter U,Hutt J J.NASA-s Next generation launch technology program-next generation space access roadmap[R].AIAA 2003-6941,2003 [4] Vaidyanathan A,Gustavsson J,Segal C.Oxygen/Hydrogen-planar-laser-induced fluorescence measurements and accuracy investigation in high-pressure combustion[J].Journal of Propulsion and Power,2009,25(4):864-874 [5] Lian C,Merkle C L.Contrast between steady and time-averaged unsteady combustion simulation[R].AIAA 2010-371,2001 [6] Marshall W M,Pal S,Woodward R D,et al.Benchmark wall heat flux data for a GO2/GH2 single element combustor[R].AIAA 2005-3572,2005 [7] Lin J,West J S,Williams R W,et al.CFD code validation of wall heat fluxes for a GO2/GH2 single element combustor[R].AIAA 2005-4524,2005 [8] 杜正刚,高玉闪,李茂,等.同轴双剪切气-气喷嘴数值模拟[J].北京航空航天大学学报,2009,35(6):683-686 Du Zhenggang,Gao Yushan,Li Mao,et al.Numerical simulation of dual shear coaxial gas-gas injector[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(6):683-686(in Chinese) [9] 杜正刚,李茂,金平,等.大流量气气喷嘴响应面法优化设计[J].北京航空航天大学学报,2010,36(4):395-398 Du Zhenggang,Li Mao,Jin Ping,et al.Large mass flowrate gas-gas injector optimization design with response surface methodology[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(4):395-398(in Chinese) [10] Shang M,Chen Y, Paul L.Investigation of chemical kinetics integration algorithms for reacting flows[R].AIAA 95-0806,1995
|