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敞口式离心喷嘴内部及近喷口区域的流动特性

陈晨 杨样 高宏力 晏至辉 杨顺华

陈晨, 杨样, 高宏力, 晏至辉, 杨顺华. 敞口式离心喷嘴内部及近喷口区域的流动特性[J]. 航空动力学报, 2016, 31(12): 2988-2995. doi: 10.13224/j.cnki.jasp.2016.12.022
引用本文: 陈晨, 杨样, 高宏力, 晏至辉, 杨顺华. 敞口式离心喷嘴内部及近喷口区域的流动特性[J]. 航空动力学报, 2016, 31(12): 2988-2995. doi: 10.13224/j.cnki.jasp.2016.12.022
CHEN Chen, YANG Yang, GAO Hong-li, YAN Zhi-hui, YANG Shun-hua. Flow field in and near the open-end swirl injector[J]. Journal of Aerospace Power, 2016, 31(12): 2988-2995. doi: 10.13224/j.cnki.jasp.2016.12.022
Citation: CHEN Chen, YANG Yang, GAO Hong-li, YAN Zhi-hui, YANG Shun-hua. Flow field in and near the open-end swirl injector[J]. Journal of Aerospace Power, 2016, 31(12): 2988-2995. doi: 10.13224/j.cnki.jasp.2016.12.022

敞口式离心喷嘴内部及近喷口区域的流动特性

doi: 10.13224/j.cnki.jasp.2016.12.022
详细信息
    作者简介:

    陈晨(1990-),男,江苏徐州人,博士生,研究方向为喷雾燃烧.E-mail:472914230@163.com

  • 中图分类号: V233.22

Flow field in and near the open-end swirl injector

  • 摘要: 为了深入理解敞口式离心喷嘴雾化机制,基于界面追踪法VOF(volume of fluid)和RNG(renormalization group)湍流模型对敞口式离心喷嘴进行数值模拟,计算结果与PDPA(phase Doppler particle analyzer)及单反相机测得的喷嘴出口速度和雾化锥角一致性较高.清晰地捕获了中心空气涡结构及喷嘴内部的回流区,展现了切向孔与旋流室的交互影响,并着重分析了液膜厚度演变特性及喷嘴内外速度场发展规律.随着喷注压降的增加,破碎长度降低,打开长度及喷雾角增加.揭示了敞口式离心喷嘴独特的流动机制,为喷嘴雾化性能预测及结构优化提供依据.

     

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出版历程
  • 收稿日期:  2016-03-29
  • 刊出日期:  2016-12-28

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