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基于VOF方法分析离心式喷嘴结构参数对性能影响

刘娟 孙明波 李清廉 王振国

刘娟, 孙明波, 李清廉, 王振国. 基于VOF方法分析离心式喷嘴结构参数对性能影响[J]. 航空动力学报, 2011, 26(12): 2826-2833.
引用本文: 刘娟, 孙明波, 李清廉, 王振国. 基于VOF方法分析离心式喷嘴结构参数对性能影响[J]. 航空动力学报, 2011, 26(12): 2826-2833.
LIU Juan, SUN Ming-bo, LI Qing-lian, WANG Zhen-guo. Analysis of geometric parameters influence on pressure swirl injector performance based on VOF interface tracking method[J]. Journal of Aerospace Power, 2011, 26(12): 2826-2833.
Citation: LIU Juan, SUN Ming-bo, LI Qing-lian, WANG Zhen-guo. Analysis of geometric parameters influence on pressure swirl injector performance based on VOF interface tracking method[J]. Journal of Aerospace Power, 2011, 26(12): 2826-2833.

基于VOF方法分析离心式喷嘴结构参数对性能影响

基金项目: 国家自然科学基金(10802095)

Analysis of geometric parameters influence on pressure swirl injector performance based on VOF interface tracking method

  • 摘要: 基于两相界面追踪流体体积(volume of fluid,简称VOF)方法模拟了离心式喷嘴内部的流动过程,在数值方法可靠性验证基础上,得到了15个喷嘴构型的流量系数、液膜厚度以及雾化锥角.定义无量纲影响因子η,比较喷嘴结构参数对喷嘴性能的影响程度.除了喷嘴直径和旋流室直径外,重点研究了出口扩张角、等直段长径比等结构参数的影响,通过与试验相对比,综合以往经验公式,得到如下结论:增大旋流室长度,能够增大雾化锥角;在喷嘴出口增加扩张角,能够显著地减小液膜厚度,减小雾化锥角;增大切向口距喷嘴顶部距离,能够改善喷嘴性能;切向口个数和等直段长度对喷嘴性能影响不大.该工作为下一步优化喷嘴构型打下了基础.

     

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出版历程
  • 收稿日期:  2011-05-04
  • 修回日期:  2011-11-24
  • 刊出日期:  2011-12-28

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