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Investigation of film cooling effectiveness and heat transfer coefficient for rectangular holes with two rows

机译:两排矩形孔的薄膜冷却效率和传热系数的研究

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摘要

When the figures are investigated the film cooling effectiveness are high value in low-blowing ratios (Figures 6-8 [Figure omitted. See Article Image.]). The best blowing ratio is 0.5 in the present blowing ratios as shown in Figures 6-8 [Figure omitted. See Article Image.]. When the differences between the injection temperature and main flow temperature are increased the cooling effectiveness increases for the same blowing ratios in mainstream direction. For example, in Figure 6 [Figure omitted.
机译:当研究数字时,薄膜的冷却效率在低吹气比时是很高的值(图6-8 [省略图。请参见文章图像]。)。如图6-8所示,在目前的吹风比中,最佳吹风比为0.5。参见文章图片。]。当喷射温度和主流温度之间的差异增大时,对于主流方向上相同的鼓风比,冷却效率会提高。例如,在图6中[省略了图。

著录项

  • 来源
    《Aircraft Engineering and Aerospace Technology》 |2009年第2期|p.1-13|共13页
  • 作者单位

    Ibrahim Koç, Department of Aeronautical Engineering, Turkish Air Force Academy, Istanbul, Turkey Yasar Islamoglu, Mechanical Engineering Department, Sakarya University, Adapazari, Turkey Ünal Akdag, Mechanical Engineering Department, Aksaray University, Aksaray, Turkey;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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