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首页> 外文期刊>International journal of mechanical and production engineering research and development >EXPERIMENTAL STUDY OF HIGH HEAT REMOVAL BY ALUMINUM PIN FIN HEAT SINK USING MULTI-JET AIR IMPINGEMENT
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EXPERIMENTAL STUDY OF HIGH HEAT REMOVAL BY ALUMINUM PIN FIN HEAT SINK USING MULTI-JET AIR IMPINGEMENT

机译:多喷流空气撞击铝销翅片散热片去除高热量的实验研究

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摘要

This Experimental Study utilizes the multi-jet impingement technique to investigate the thermal performance of pin fin heat sink under unconfined and semi confined conditions. In the present Experimental investigates the effect of Aluminum Heat sink, nozzle jet exit Velocity, the jet to jet spacing and the nozzle plate to Flat plate heat sink or pin fin base plate Separation distance(Z/D) in a 3×3Square Multi-jet impinging array on average Nusselts number. Thermal Performance of Pin fin heat sink of 60×60×6mm for the Reynolds numbers range 6000 to 12000 is studied. The thermal performance of 4×4array circular Pin fin heat sink is studied with the thermal Parameters like Average Nusselts number, total thermal resistance, Average base temperature, Reynolds numbers.
机译:该实验研究利用多喷流撞击技术研究了无限制和半限制条件下针翅式散热器的热性能。在本实验中,我们研究了3×3平方英寸多方孔距中铝散热片,喷嘴射流出口速度,喷嘴与射流间距以及喷嘴板与平板散热器或针状翅片基板之间的距离的影响。平均努塞尔特数的喷气撞击阵列。研究了雷诺数为6000至12000的60×60×6mm翅片散热片的热性能。利用平均努塞尔数,总热阻,平均基准温度,雷诺数等热参数研究了4×4阵列圆形Pin翅片散热器的热性能。

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