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Detailed Heat Transfer Measurements of Curved Fin Channels

机译:弯曲翅片通道的详细传热测量

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Detailed Nusselt number (Nu) distributions over six fin surfaces are presented for two sets of curved fin channels with twin- and single-flow exits that simulate flow passages in a cylindrical fin array for cooling of electronic chipsets. Each set of curved fin channels shares an identical cross-sectional shape with three different fin length (L)-to-hydraulic diameter (D) ratios of 22.5, 16.2 and 9.8. Influences of LID ratio and exit condition on local Nu distributions over curve fin surfaces at Reynolds numbers (Re) of 500, 1,000, 1,200, 2,000, 4,000, 6,000, and 8,000 are examined. Spatially averaged Nusselt numbers (Nu) for two sets of tested channels are analyzed and compared that unravel the interactive impacts of LID ratio and Re on heat transfer. In the present Re range, relative Nu ratios between test channels with twin and single exits fall in the ranges of 0.97-1.08, 1.1-1.2, and 1.25-1.3 for LID ratios of 22.5, 16.2, and 9.8, respectively. Heat transfer correlations for Nu are generated using Re and LID ratio as determining variables. A set of criteria for determining the optimal LID ratio that provides the maximum cooling power available from a curve fin surface for the specified cross-sectional shape of curved fin channel are derived to assist the design activities for such cylindrical fin array.
机译:为两组弯曲的翅片通道提供了六个翅片表面的详细Nusselt数(Nu)分布,该翅片通道具有双流和单流出口,可模拟圆柱形翅片阵列中的流动通道以冷却电子芯片组。每组弯曲的翅片通道共享相同的横截面形状,并且翅片长度(L)与液压直径(D)的比率为32.5,即22.5、16.2和9.8。研究了LID比率和出口条件对雷诺数(Re)为500、1,000、1,200、2,000、4,000、6,000和8,000的曲线鳍表面上局部Nu分布的影响。分析并比较了两组测试通道的空间平均努塞尔数(Nu),以揭示LID比和Re对传热的交互影响。在当前的Re范围内,对于LID比率为22.5、16.2和9.8,具有双出口和单出口的测试通道之间的相对Nu比率分别落在0.97-1.08、1.1-1.2和1.25-1.3的范围内。使用Re和LID比作为确定变量来生成Nu的传热相关性。得出了一组确定最佳LID比率的标准,该标准为弯曲翅片通道的指定横截面形状提供了可从弯曲翅片表面获得的最大冷却功率,以帮助进行此类圆柱形翅片阵列的设计活动。

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