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不同形状喷嘴的旋流冲击射流压力损失和传热特性实验

徐亮 任德祖 马永浩 兰进 高建民

徐亮, 任德祖, 马永浩, 兰进, 高建民. 不同形状喷嘴的旋流冲击射流压力损失和传热特性实验[J]. 航空动力学报, 2018, 33(11): 2678-2686. doi: 10.13224/j.cnki.jasp.2018.11.014
引用本文: 徐亮, 任德祖, 马永浩, 兰进, 高建民. 不同形状喷嘴的旋流冲击射流压力损失和传热特性实验[J]. 航空动力学报, 2018, 33(11): 2678-2686. doi: 10.13224/j.cnki.jasp.2018.11.014
Pressure loss and heat transfer characteristics experiment of swirling impinging jet with different shape nozzles[J]. Journal of Aerospace Power, 2018, 33(11): 2678-2686. doi: 10.13224/j.cnki.jasp.2018.11.014
Citation: Pressure loss and heat transfer characteristics experiment of swirling impinging jet with different shape nozzles[J]. Journal of Aerospace Power, 2018, 33(11): 2678-2686. doi: 10.13224/j.cnki.jasp.2018.11.014

不同形状喷嘴的旋流冲击射流压力损失和传热特性实验

doi: 10.13224/j.cnki.jasp.2018.11.014
基金项目: 国家重点研发计划项目(2018YFB1106405); 陕西省自然科学基金(2015JQ5126); 中央高校基本科研业务专项基金(xjj2018044)

Pressure loss and heat transfer characteristics experiment of swirling impinging jet with different shape nozzles

  • 摘要: 提出了一种旋流喷嘴,即圆孔内径设有四条螺旋槽道的类螺纹孔喷嘴。实验对比研究了同一螺旋角下三类旋流喷嘴(插件、内置扭转带、导叶片)与螺纹孔喷嘴在雷诺数为6000、12000下靶面传热特性。分析了各喷嘴对应的气源室压力与流量系数。实验结果表明,螺纹孔喷嘴在靶面的中心区保持了高的传热效率,驻点努塞尔数比其他三种喷嘴高出29.7%~43.3%,当射流空间受限时(半封闭空间)所有喷嘴的努塞尔数下降了40%~60%,内置插件喷嘴下降幅度最大;另外,四种旋流喷嘴中,内置插件喷嘴的气源腔室压力最大,比最小的螺纹孔喷嘴高出一个数量级还多,压力损失系数的分析表明螺纹孔喷嘴的压力损失系数最小,仅是内置插件喷嘴的1/4左右,且雷诺数增大一倍,内置插件喷嘴的压力损失系数平均下降14%,下降幅度最大。

     

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出版历程
  • 收稿日期:  2017-07-21
  • 刊出日期:  2018-11-28

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