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凹槽孔槽深和动量比对气膜冷却特性的影响

王振伟 朱惠人 张宗卫 孟庆昆

王振伟, 朱惠人, 张宗卫, 孟庆昆. 凹槽孔槽深和动量比对气膜冷却特性的影响[J]. 航空动力学报, 2012, 27(11): 2455-2461.
引用本文: 王振伟, 朱惠人, 张宗卫, 孟庆昆. 凹槽孔槽深和动量比对气膜冷却特性的影响[J]. 航空动力学报, 2012, 27(11): 2455-2461.
WANG Zhen-wei, ZHU Hui-ren, ZHANG Zong-wei, MENG Qing-kun. Effect of trench hole depth and momentum flux ratio on film cooling characteristics[J]. Journal of Aerospace Power, 2012, 27(11): 2455-2461.
Citation: WANG Zhen-wei, ZHU Hui-ren, ZHANG Zong-wei, MENG Qing-kun. Effect of trench hole depth and momentum flux ratio on film cooling characteristics[J]. Journal of Aerospace Power, 2012, 27(11): 2455-2461.

凹槽孔槽深和动量比对气膜冷却特性的影响

基金项目: 国家重点基础研究发展计划(2007CB707701)

Effect of trench hole depth and momentum flux ratio on film cooling characteristics

  • 摘要: 采用瞬态液晶全表面测量技术测量了凹槽孔的气膜冷却特性,研究了动量比和槽深对冷却效率的影响,并和圆柱形孔的测量结果实施了比较.结果表明:冷气在凹槽内横向传播,凹槽抑制了冷气射流分离,凹槽孔比圆柱形孔提供更多的二维气膜.槽深孔径比为0.75是最佳的.随着动量比的增加,冷却效率值逐渐趋于稳定,冷却效率仅有轻微增加.

     

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出版历程
  • 收稿日期:  2011-10-31
  • 刊出日期:  2012-11-28

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