Enhancement of the cooling performance of circular pin fin heat sinks under flow bypass conditions

H. Jonsson, B. Moshfegh
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引用次数: 12

Abstract

CFD models of circular pin fin heat sinks have been developed. The heat sinks are situated in bypass flow in a duct with constant dimensions. The air velocity was constant, the flow was turbulent, and for turbulence modeling the Chen-Kim k-/spl epsiv/ model was used. The influence of increasing fin height in the flow direction, and uneven distribution of the fins in the lengthwise and the spanwise direction are studied. In the case of increasing fin height, it was shown that an increase in the heat transfer coefficient can be achieved without an increase in pressure drop when compared at equal mean fin height. In the case of uneven distribution of the fins it was shown that the heat transfer coefficient could be increased by an uneven distribution of the fins in the lengthwise direction, using smaller fin spacing at the trailing edge of the heat sink. Results also showed that some cases of unevenly distributed fins in the spanwise direction could achieve an increase in the heat transfer coefficient. These cases had smaller fin spacing at the center of the heat sink, and the fin height was close to the duct height. The pressure drop was almost the same as for heat sinks with even distribution of the fins.
流动旁通条件下圆针翅片散热器冷却性能的提高
建立了圆针翅散热器的CFD模型。散热器位于一个尺寸恒定的管道的旁路流中。紊流模型采用Chen-Kim k-/spl epsiv/模型。研究了增加翅片高度对流动方向的影响,以及翅片在纵向和展向上的不均匀分布。在增加翅片高度的情况下,与等平均翅片高度相比,可以在不增加压降的情况下实现换热系数的增加。在翅片分布不均匀的情况下,在散热器后缘采用较小的翅片间距,使翅片在纵向上分布不均匀,可以提高换热系数。结果还表明,在某些情况下,翅片沿展向不均匀分布可以提高换热系数。在这种情况下,散热器中心的翅片间距较小,且翅片高度接近风管高度。压降几乎与翅片均匀分布的散热器相同。
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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