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Impingement thermal performance of perforated circular pin-fin heat sinks

机译:穿孔圆形针翅式散热器的冲击热性能

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摘要

Abstract The study presents the experimental information on heat transfer performance of jet impingement cooling on circular pin- fin heat sinks with/without a hollow perforated base plate. Smoke flow visualization is also used to investigate the behavior of the complicated flow phenomena of the present heat sinks for this impingement cooling. The effects of flow Reynolds numbers (3458≤Re≤11,526), fin height, the geometry of the heat sinks (with/without a hollow perforated base plate), and jet-to-test heat sink placement (1 ≤ H / d ≤16) are examined. In addition, empirical correlation to estimate the heat transfer coefficient was also developed.
机译:摘要研究提供了带有或不带有空心穿孔基板的圆形针翅式散热器上射流冲击冷却传热性能的实验信息。烟流可视化还用于调查这种冲击冷却中当前散热器的复杂流现象的行为。雷诺流动数(3458≤Re≤11,526),散热片高度,散热器的几何形状(带/不带空心穿孔基板)和喷射测试散热器放置(1≤H / d≤)的影响16)被检查。此外,还建立了经验相关性来估算传热系数。

著录项

  • 来源
    《Heat and mass transfer》 |2018年第4期|1009-1020|共12页
  • 作者

    Mao-Yu Wen; Cheng-Hsiung Yeh;

  • 作者单位

    Department of Mechanical Engineering, Cheng Shiu University;

    Department of Mechanical Engineering, Cheng Shiu University;

  • 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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