航天推进技术研究院主办
FEI Jun,SUN Fan,YANG Wei-dong,et al.Experimental analysis on movement and size distribution of atomized droplets from impinging liquid jet[J].Journal of Rocket Propulsion,2015,41(01):10-14.
射流撞击雾化液滴运动过程与粒径分布特性的试验研究
- Title:
- Experimental analysis on movement and size distribution of atomized droplets from impinging liquid jet
- Keywords:
- impinging injector; atomized droplets; liquid sheet; velocity distri
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 在大气环境下,以水为介质,采用PDPA和高速动态分析系统,针对直流撞击式喷注单元的雾场结构进行试验研究,获得了雾化液滴速度分布、粒径分布等试验参数。从液滴运动及液滴大小分布的角度针对撞击雾化液膜破碎成液滴的过程进行了分析,发现水平面上雾化液滴的径向速度以原点为中心对称,且随离原点距离增大而增大;初始雾化阶段的粒径大小分布则与径向速度分布相反。分析认为是液膜运动过程赋予了雾化液滴的初始速度,并影响了初始雾化液滴的分布特性。
- Abstract:
- The experimental study on atomization formation and size distribution of water droplets from the impinging liquid jets was executed in atmosphere environment by using PDPA and high speed dynamic analysis system. The movement and the size distribution of droplets were analyzed. It is found that the radial velocity of droplets on horizontal plane is centrosymmetric and increases as the increasing distance from the center to the measuring point. The size distribution of droplets in the initial stage of atomization is contrary to that of radial velocity. It is believed that the initial velocity of atomization droplets and the size distribution of droplets during the initial stage of atomization are both influenced by the movement of liquid sheet.
参考文献/References:
[1]ANDERSON W E, RYAN H M, PAL S, et al. Fundamental studies of impinging liquid jets, AIAA92-0458[R]. USA: AIAA, 1992.
[2]RYAN H M, ANDERSON W E, PAL S, et al. Atomization characteristics of impinging liquid jets, AIAA93-0230 [R]. USA: AIAA, 1993.
[3]STRAKEY P A, TALLY D G. Spray characteristics of impinging jet injectors at high back-pressure[C]//Eighth Internaltional Conference on Liquid Atomization and Spray Systems. Pasadena, CA, USA: [s.n.], 2000: 11-16.
[4]VASSALLO P, ASHGRIZ N, BOORADY F A. Effect of flow rate on the spray characteristics of impinging water jets[J]. Journal of Propulsion and Power, 1992, 8(5): 980- 986.
[5]张蒙正, 张泽平, 李鳌, 等. 两股互击式喷嘴雾化性能实验研究[J]. 推进技术, 2000, 21(1): 57-59.
[6]张蒙正, 杨伟东, 王玫. 双股互击式喷嘴凝胶水雾化特性试[J]. 推进技术, 2008 , 29 (1): 22-24,61.
[7]CHEN Xiao-dong, MA Dong-jun, YANG Vigor. High-fidelity numercial simulations of impinging jet atomization, AIAA 2012-4328 [R]. USA: AIAA, 2012.
[8]MA Dong-jun, CHEN Xiao-dong, KHARE Prashant, et al. Atomization patterns and breakup characteristics of liquid sheets formed by two impinging jets, AIAA 2011-97[R]. USA: AIAA, 2011.
[9]强洪夫, 刘虎, 陈福振, 等. 基于SPH方法的射流撞击仿真[J]. 推进技术. 2012, 33(3):424-429.
[10]CHIHIRO Inoue, TOSHINORI Watanabe, TAKEHIRO Himeno. Study on atomization process of liquid sheet formed by impinging Jets, AIAA 2008-4847[R]. USA: AIAA, 2008.
[11]CHEN Xiao-dong, MA Dong-jun, YANG Vigor. Mechaism study of impact wave in impinging jets atomization, AIAA 2012-1089 [R]. USA: AIAA, 2012.
备注/Memo
收稿日期:2014-06-13;修回日期:2014-07-09 基金项目: 国家重大基础研究项目(613193) 作者简介:费俊(1981—),女,博士,研究领域为液体火箭发动机基础理论