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带斜孔肋大宽高比矩形通道的强化传热特性

朱强华 崔苗 高效伟

朱强华, 崔苗, 高效伟. 带斜孔肋大宽高比矩形通道的强化传热特性[J]. 航空动力学报, 2016, 31(4): 780-787. doi: 10.13224/j.cnki.jasp.2016.04.003
引用本文: 朱强华, 崔苗, 高效伟. 带斜孔肋大宽高比矩形通道的强化传热特性[J]. 航空动力学报, 2016, 31(4): 780-787. doi: 10.13224/j.cnki.jasp.2016.04.003
ZHU Qiang-hua, CUI Miao, GAO Xiao-wei. Enhanced heat transfer characteristics in a large aspect ratio rectangular channel with inclined perforated rib[J]. Journal of Aerospace Power, 2016, 31(4): 780-787. doi: 10.13224/j.cnki.jasp.2016.04.003
Citation: ZHU Qiang-hua, CUI Miao, GAO Xiao-wei. Enhanced heat transfer characteristics in a large aspect ratio rectangular channel with inclined perforated rib[J]. Journal of Aerospace Power, 2016, 31(4): 780-787. doi: 10.13224/j.cnki.jasp.2016.04.003

带斜孔肋大宽高比矩形通道的强化传热特性

doi: 10.13224/j.cnki.jasp.2016.04.003
基金项目: 

国家自然科学基金(51206014)

中央高校基本科研业务费专项资助(DUT2014040)

详细信息
    作者简介:

    朱强华(1980-),男,江西南昌人,讲师,博士,研究方向为叶轮机气动热力学.

  • 中图分类号: V231.1

Enhanced heat transfer characteristics in a large aspect ratio rectangular channel with inclined perforated rib

  • 摘要: 为了获得带斜孔肋大宽高比矩形通道的强化传热特性,并寻求最佳的孔排倾斜角度,调节孔排倾斜角度和通道雷诺数,使其分别在0°~30°和3×104~9×104范围内变化,通过数值计算系统分析了通道摩擦因数和带肋壁努塞尔数等参数的变化规律.研究发现:相比于常规肋片,新型斜孔肋有效改善了肋片后方紧邻肋片的局部区域的壁面换热,并降低通道的摩擦因数,但传热增强因子有所减小;随着孔排倾斜角度的增大,通道的相对摩擦因子单调升高,传热增强因子则呈现出先升高后降低的变化过程,因此存在着最优孔排倾斜角度为15°,此时斜孔肋的强化传热综合指标达到最大值;随着通道雷诺数的增大,斜孔肋通道的摩擦因数小幅减小,换热则逐渐增强.

     

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出版历程
  • 收稿日期:  2014-08-25
  • 刊出日期:  2016-04-28

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