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改变结构参数对旋流喷嘴内外两相流场的影响

史卫东 张良 陈亮 何海燕 刘江海

史卫东, 张良, 陈亮, 何海燕, 刘江海. 改变结构参数对旋流喷嘴内外两相流场的影响[J]. 航空动力学报, 2013, 28(1): 158-163.
引用本文: 史卫东, 张良, 陈亮, 何海燕, 刘江海. 改变结构参数对旋流喷嘴内外两相流场的影响[J]. 航空动力学报, 2013, 28(1): 158-163.
SHI Wei-dong, ZHANG Liang, CHEN Liang, HE Hai-yan, LIU Jiang-hai. Effect of structural changes of swirl nozzle on two phase flow[J]. Journal of Aerospace Power, 2013, 28(1): 158-163.
Citation: SHI Wei-dong, ZHANG Liang, CHEN Liang, HE Hai-yan, LIU Jiang-hai. Effect of structural changes of swirl nozzle on two phase flow[J]. Journal of Aerospace Power, 2013, 28(1): 158-163.

改变结构参数对旋流喷嘴内外两相流场的影响

Effect of structural changes of swirl nozzle on two phase flow

  • 摘要: 针对一种超细粉体旋流分散喷嘴,在不同进气角度和出口锥角的条件下,采用雷诺应力湍流模型(RSM)并考虑气体的可压缩性,对喷嘴内部及出口附近的强旋、跨声速流场进行了模拟,同时结合离散相模型研究了1~10μm粒子的运动轨迹和质量浓度分布规律.结果显示:改变旋流喷嘴的进气角度对旋流强度和湍流强度影响不大,而出口锥角改变时,喷嘴内的旋流强度有明显变化;随着颗粒密度或出口锥角增大,或进气角度减小,旋流喷嘴内粒子的临界逃逸粒径相应减小;在喷嘴后方,颗粒相达到较好的扩散均匀性所需的掺混距离约为20倍喷嘴出口直径.

     

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出版历程
  • 收稿日期:  2012-04-14
  • 刊出日期:  2013-01-28

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