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Heat Transfer Coefficient of Film Cooling with Ellipse-Shaped Tab

机译:椭圆形凸片冷却薄膜的传热系数

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摘要

The enhanced cooling performance caused by ellipse-shaped tabs located at the outlet of the film cooling holes is conducted.Three covering ratios of ellipse-shaped tabs on film holes and four blowing ratios are studied.The results show that:(1)The heat transfer coefficient ratio is higher than that without tab,indicating that the mixing of mainstream and coolant jet provides a better coverage film on the cooling wall,but increases the local turbulence production which enhances the heat transfer coefficient;(2)When the ellipse-shaped tabs are located at the film hole outlet,there is a larger pressure drop with the ellipse tab relative to the no-tab case.Thus,the discharge coefficient with ellipse tab is lower than that without tab.

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2016年第2期|155-165|共11页
  • 作者

    Zheng Xianwu; Yang Weihua;

  • 作者单位

    China Aviation Powerplant Research Institute, Zhuzhou 412002, P.R.China;

    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 热力学、传热;
  • 关键词

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