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旋转条件下半封闭空间内多孔冲击平均换热特性实验

杨敏 常海萍 吴培光

杨敏, 常海萍, 吴培光. 旋转条件下半封闭空间内多孔冲击平均换热特性实验[J]. 航空动力学报, 2006, 21(6): 984-988.
引用本文: 杨敏, 常海萍, 吴培光. 旋转条件下半封闭空间内多孔冲击平均换热特性实验[J]. 航空动力学报, 2006, 21(6): 984-988.
YANG Min, CHANG Hai-ping, WU Pei-guang. Experimental investigation of the rotating multiple jets impingement heat transfer chracteristic in semi-limited space[J]. Journal of Aerospace Power, 2006, 21(6): 984-988.
Citation: YANG Min, CHANG Hai-ping, WU Pei-guang. Experimental investigation of the rotating multiple jets impingement heat transfer chracteristic in semi-limited space[J]. Journal of Aerospace Power, 2006, 21(6): 984-988.

旋转条件下半封闭空间内多孔冲击平均换热特性实验

基金项目: 国家自然科学基金资助项目(50276027);国防基础科研资助项目(J1400D001)

Experimental investigation of the rotating multiple jets impingement heat transfer chracteristic in semi-limited space

  • 摘要: 通过实验研究了冲击雷诺数Rej、旋转雷诺数Reω、以及冲击孔的排列方式、冲击孔到靶板之间的距离等参数,对旋转条件下半封闭空间内多孔冲击平均换热特性的影响。实验结果表明:随着冲击雷诺数的增大,多孔冲击的平均Nu数显著提高;随着旋转雷诺数的增大,平均Nu数稍有提高,但变化幅度不大;冲击孔的排列方式对平均换热效果也有一定的影响,叉排式稍优于顺排式;并且实验得出,冲击孔到靶板之间的距离为4倍冲击孔直径时多孔冲击平均换热效果最佳。

     

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出版历程
  • 收稿日期:  2005-12-12
  • 修回日期:  2006-06-21
  • 刊出日期:  2006-12-28

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