Experiment and simulation of impinging coaxial gas-gas injector

[1] Farhangi S,Yu T,Rojas L,et al.Gas-Gas injector technology for full flow combustion cycle application .AIAA-1999-2757,1999 [2] Foust M J,pal S,Santoro R J.Gaseous propellant rocket studies using raman spectroscopy .AIAA-1996-2766,1996 [3] Archambault M R,Talley D,Peroomian O.Computational analysis of a single-element,shear-coaxial,GH2/GO2 engine .AIAA -2002-1088,2002 [4] Vaidyanathan A,Gustavsson J,Segal C.Heat fluxes/OH PLIF measurements in a GO2/GH2 single-element,shear injector .AIAA-2007-5591,2007 [5] Wang Xiaowei,Cai Guobiao,Jin Ping.Scaling of the flowfield in a combustion chamber with a gas-gas injector[J].Chin Phys B,2010,19(1):345-352 [6] 杜正刚,高玉闪,蔡国飙.氧压降对气-气喷嘴燃烧过程的影响[J].宇航学报,2009,30(2):675-679 Du Zhenggang,Gao Yushan,Cai Guobiao.The effect of oxygen drop on combustion process gas-gas injector[J].Journal of Astronautics,2009,30(2) :675-679(in Chinese) [7] 杜正刚,高玉闪,金平,等.速度比对气-气喷嘴燃烧性能的影响[J].推进技术,2009,30(5):551-554 Du Zhenggang,Gao Yushan,Jin Ping,et al.Effect of velocity ratio on combustion process gas-gas injector[J].Journal of Propulsion Technology,2009,30(5):551-554(in Chinese) [8] Vaidyanathan R,Tucker P K,Papila N,et al.CFD-based design optimization for a single element rocket injector .AIAA-2003-296,2003 [9] Vaidyanathan R,Tucker P K,Papila N,et al.Computational-fluid-dynamics-based design optimization for single-element rocket injector[J].Journal of Propulsion and Power,2004,20(4):705-717 [10] Vaidyanathan R,Goel T,Shyy W,et al.Global sensitivity and trade-off analyses for multi-objective liquid rocket injector design .AIAA-2004-4007,2004 [11] Goel T,Vaidyanathan R,Shyy W,et al.Response surface approximation of pareto optimal front in multi-objective optimization .AIAA-2004-4501,2004