Modeling of the thermal and hydraulic performance of plate fin, strip fin, and pin fin heat sinks-influence of flow bypass

H. Jonsson, B. Moshfegh
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引用次数: 147

Abstract

Tests have been conducted in a wind tunnel with seven types of heat sinks including plate fin, strip fill, and pin fin heat sinks. In the case of strip fin, and pin fin heat sinks, both inline and staggered arrays have been studied. The pin fin heat sinks had circular and square cross-sections. For each type, tests were run with fin heights (H) of 10, 15, and 20 mm while the heat sink width (B) was kept constant and equal to 52.8 mm. In total, 42 different heat sinks were tested. The width of the wind tunnel duct (CB) was varied in such a way that results were obtained for B/CB=0.84, 0.53, and 0.33. The wind tunnel height (CH) was varied similarly, and data were recorded for H/CH=1, 0.67, and 0.33 while the duct Reynolds number was varied between 2000 through 14000. An empirical bypass correlation has been developed for the different fin designs. The correlation predicts the Nusselt number and the dimensionless pressure drop and takes into account the influence of duct height, duct width, fin height, fin thickness, and fin-to-fin distance. The correlation parameters are individual for each fin design. Further, a physical bypass model for plate fin heat sinks has been developed to describe the bypass effect.
板翅片、条形片和针翅片散热器的热工性能建模——流动旁通的影响
在风洞中进行了包括板翅片、条填充片和针翅片在内的7种散热器的试验。在带状翅片和针翅片散热器的情况下,已经研究了直列和交错阵列。针翅式散热器有圆形和方形的横截面。对于每种型号,分别在翅片高度(H)为10、15和20 mm时进行试验,而散热器宽度(B)保持不变,等于52.8 mm。总共测试了42种不同的散热器。风洞风管宽度(CB)的变化使得B/CB=0.84, 0.53和0.33的结果得到。风洞高度(CH)也发生了类似的变化,当风洞雷诺数在2000 ~ 14000之间变化时,记录了H/CH=1、0.67和0.33的数据。针对不同的翅片设计,建立了经验涵道关联。相关性预测了努塞尔数和无量纲压降,并考虑了风管高度、风管宽度、翅片高度、翅片厚度和翅片间距的影响。每个翅片设计的相关参数都是独立的。此外,还建立了板翅式散热器的物理旁路模型来描述旁路效应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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