首页> 外文会议>International Mechanical Engineering Congress and Exposition 2007 >EXPERIMENTS ON THE FLOW AND HEAT TRANSFER IN FINE PITCH PARALLEL PLATE HEAT SINKS WITH TOP INLET SIDE EXIT FLOW
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EXPERIMENTS ON THE FLOW AND HEAT TRANSFER IN FINE PITCH PARALLEL PLATE HEAT SINKS WITH TOP INLET SIDE EXIT FLOW

机译:顶部入口侧面出水细间距平行板热沉的流动与传热实验

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Detailed temperature and pressure measurements in high aspect ratio parallel plate fin heat sinks were made in a Top Inlet Side Exit (TISE) experiment configuration without top bypass flow. Air flow was supplied to the top of the heat sink using a rectangular jet nozzle with three different jet nozzle widths, Wj. The study covered five jet velocities and three different jet nozzle width to heat sink length ratios. Static pressure measurements were made along the spanwise centerline inside the heat sink and on the mounting plate outside the heat sink. The measurements were used to study the influence of the jet impinging on the top of the heat sink on the loss coefficient of the heat sink. It was found that the overall loss coefficient was dependent on Re, Wj, the fin spacing, b, and the jet nozzle width relative to the heat sink length, Wj/L. Temperature measurements were made to study the total thermal resistance with no base heat spreading. An ad hoc model was used to predict the total thermal resistance of the heat sink in this complicated flow. The model modifies the total cooled area of the fin as a function of jet width and heat sink geometry. Good agreement was found with the experimental data for the cases of Wj/L =1.0 and 0.5. The model does not work well in the case of Wj/L =0.25.
机译:在没有顶部旁路流量的顶部入口侧出口(TISE)实验配置中,对高纵横比平行板翅片散热器进行了详细的温度和压力测量。使用具有三个不同喷嘴宽度Wj的矩形喷嘴将空气流供应到散热器的顶部。该研究涵盖了五种射流速度和三种不同的射流喷嘴宽度与散热片长度之比。沿散热器内部的翼展方向中心线和散热器外部的安装板上进行静压力测量。这些测量值用于研究射流撞击散热器顶部对散热器的损耗系数的影响。发现总损耗系数取决于Re,Wj,散热片间距b和相对于散热器长度Wj / L的喷嘴宽度。进行温度测量以研究在没有基础热扩散的情况下的总热阻。在这种复杂的流动中,使用了一个ad hoc模型来预测散热器的总热阻。该模型根据射流宽度和散热器几何形状修改散热片的总冷却面积。在Wj / L = 1.0和0.5的情况下,与实验数据发现了很好的一致性。在Wj / L = 0.25的情况下,该模型不能很好地工作。

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