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射流、旋流、出流共同作用下矩形通道换热特性

张宗卫 朱惠人 赵曙 郭涛

张宗卫, 朱惠人, 赵曙, 郭涛. 射流、旋流、出流共同作用下矩形通道换热特性[J]. 航空动力学报, 2011, 26(6): 1321-1327.
引用本文: 张宗卫, 朱惠人, 赵曙, 郭涛. 射流、旋流、出流共同作用下矩形通道换热特性[J]. 航空动力学报, 2011, 26(6): 1321-1327.
ZHANG Zong-wei, ZHU Hui-ren, ZHAO Shu, GUO Tao. Heat transfer characteristics in an internal coolant passage with crossflow-induced swirl, impingement and film cooling holes[J]. Journal of Aerospace Power, 2011, 26(6): 1321-1327.
Citation: ZHANG Zong-wei, ZHU Hui-ren, ZHAO Shu, GUO Tao. Heat transfer characteristics in an internal coolant passage with crossflow-induced swirl, impingement and film cooling holes[J]. Journal of Aerospace Power, 2011, 26(6): 1321-1327.

射流、旋流、出流共同作用下矩形通道换热特性

基金项目: 国家重点基础研究发展计划(2007CB707701); 西北工业大学博士论文创新基金

Heat transfer characteristics in an internal coolant passage with crossflow-induced swirl, impingement and film cooling holes

  • 摘要: 在放大模型上详细研究了不同雷诺数和出流比下涡轮叶片内冷通道中冲击靶面、出流面和冲击侧面的换热特性.采用热色液晶瞬态测量技术测量通道内部各个面的传热系数,得到以下结论:靶面直接受到射流的第一次冲击,射流形成旋流对出流面进行第二次冲刷,对冲击侧面进行第三次冲刷;靶面受到冲击孔射流的直接冲击,因此换热最强;冲击侧面只受到旋流、横流影响,因此换热最弱;冲击和旋流是通道各个面换热强化的主要原因;换热随雷诺数的增大而增强.出流比对各个面的换热分布及大小也有一定影响.

     

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出版历程
  • 收稿日期:  2010-05-29
  • 修回日期:  2010-10-28
  • 刊出日期:  2011-06-28

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