摘要
一个舵栓注射者为扼杀一台液体火箭引擎并且减少引擎重量是有益的。这研究为液体气体燃料在舵栓注射者的水花特征上以各种各样的注射条件探索动量比率和威伯数字的效果。一张液体表从一张中心舵栓嘴被注射，它被一口煤气的喷气从环形的差距打破。燃料的压力落下，和舵栓洞距离被看作控制变量；使用 0.1 1.0 液体注射作为为压力的一个酒吧落下，为为舵栓洞距离的煤气的喷气和 0.2 1.0 公里的压力落下的 0.010.2 酒吧。分泌物系数在 0.75 公里的舵栓洞距离前线性地被减少然后，系数稍微被增加。水花图象被一个互补金属氧化物半导体照相机与高分辨率捕获。然后，阴影和反映的图象被分析。水花分布被 patternator 从一个舵栓尖端与 50 公里的轴的距离测量。最后，角度有指数地减少的水花一半动量比率由威伯数字划分了的关联。另外，水花一半从水花分发的角度与从捕获的图象测量的那些相比被低估。
A pintle injector is advantageous for throttling a liquid rocket engine and reducing engine weight. This study ex- plores the effects of momentum ratio and Weber number at various injection conditions on spray characteristics of the pintle injector for liquid-gas propellants. A liquid sheet is injected from a center pintle nozzle and it is broken by a gas jet from an annular gap. The pressure drops of propellants, and the pintle opening distance were consi- dered as control variables; using 0.1 -1.0 as a bar for the pressure drop of the liquid injection, a 0.01-4）.2 bar for the pressure drop of gas jet and a 0.2 - 1.0 mm for the pintle opening distance. The discharge coefficient was de- creased linearly before the pintle opening distance of 0.75 mm and then, the coefficient was slightly increased. Spray images were captured by a CMOS camera with high resolution. Then, the shadow and reflected images were analyzed. Spray distributions were measured by a pattemator with an axial distance of 50 mm from a pintle tip. Finally, the spray half angles had an exponentially decreasing correlation as a momentum ratio divided by the Weber number. Also, the spray half angles from the spray distribution were underestimated compared to those measured from the captured images.
基金
supported by Advanced Research Center Program(NRF-2013R1A5A1073861)through the National Research Foundation of Korea(NRF)
grant funded by the Korea government(MSIP)contracted through Advanced Space Propulsion Research Center at Seoul National University
