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SINGLE-PHASE CRYOGENIC FLOWS THROUGH MICROCHANNEL HEAT SINKS

机译:单相致冷剂通过微通道传热流动

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Cryogenic fluids are used widely in several thermal management applications such as in regenerative cooling of rocket engine combustor liners, missile warning receivers, satellite tracking systems and cryo-adsorbent hydrogen storage systems. Single phase laminar flow and heat transfer rate of liquid nitrogen in microchannels is studied experimentally in this paper. The performance of two distinct geometries of microchannel heat sinks are evaluated and compared for simultaneous developing laminar flow in the Reynolds number range from 180 to 610. The first geometry pertains to parallel microchannels while the second corresponds to a staggered microscale pin fin array. Two parallel microchannel geometries having identical widths of 140μm and identical laminar thermal resistances but with different aspect ratios of 4.7 and 7.6 are compared. The pin fin heat sink consisted of square pins of 395μm side and oriented at 45 degrees to the flow. All three heat sinks have identical heat source surface area. Results are presented in a non-dimensional form in terms of the friction factor, Nusselt, Reynolds numbers and compared with the predictions of existing correlations in the literature for parallel microchannels and micro pin fin heat sinks.
机译:低温流体被广泛用于多种热管理应用中,例如火箭发动机燃烧室衬套,导弹预警接收器,卫星跟踪系统和低温吸收氢存储系统的再生冷却。本文通过实验研究了微通道中液氮的单相层流和传热速率。评估并比较了两个不同几何形状的微通道散热器的性能,以研究同时发展的层流在雷诺数范围从180到610的情况。第一种几何形状属于平行微通道,而第二种几何形状则对应于交错的微尺度针翅阵列。比较了两个平行的微通道几何结构,它们具有相同的140μm宽度和相同的层状热阻,但具有4.7和7.6的不同长宽比。针翅散热片由395μm边的方形针组成,并与气流成45度角。三个散热器均具有相同的热源表面积。结果以摩擦因数,努塞尔(Nusselt),雷诺数(Reynolds number)的无量纲形式表示,并与文献中关于平行微通道和微针翅片散热器的现有相关性的预测进行了比较。

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