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A numerical study of entry region laminar mixed convection over shrouded vertical fin arrays

机译:笼罩式垂直翅片阵列入口区域层流混合对流的数值研究

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摘要

A computational study of laminar mixed convection over a shrouded vertical rectangular fin array attached to a vertical base has been performed. Maintaining the base-fin system above the surrounding temperature, a fan velocity is imposed to enhance the heat transfer through the mixed convection process. Present study finds the effects of clearance spacing, fin spacing, fin length, Reynolds number and Grashof number on the thermal performance of the base-fin system. Mixed convection inlet velocity is decoupled to forced and natural convection velocity components and the resulting pressure drop across the duct length arises purely due to the forced convection velocity component. Thus, Reynolds number is estimated based on forced convection velocity component as the inlet velocity does not vanish even in pure natural convection. Computed local Nusselt number shows sharp drop near the entrance and reaches a fully developed value after a certain streamwise distance from the entrance. Further, fully developed local Nusselt number shows a clear maximum at the clearance spacing of 0.075 and 0.15 for the inter-fin spacing of 0.3 and 0.5 respectively. Pressure drop across the duct, induced natural convection velocity and overall Nusselt number are well correlated with the governing parameters of the problem.
机译:已经进行了对附接到垂直基座上的垂直矩形翅片阵列的层流混合对流的计算研究。将基翅片系统维持在高于周围温度的温度下,施加风扇速度以提高通过混合对流过程的热传递。目前的研究发现间隙间距,散热片间距,散热片长度,雷诺数和格拉索夫数对基础散热片系统的热性能的影响。混合对流入口速度与强制对流速度和自然对流速度分量解耦,并且在管道长度方向上产生的压降纯粹是由于强制对流速度分量引起的。因此,雷诺数是基于强制对流速度分量估算的,因为即使在纯自然对流中入口速度也不会消失。计算得出的本地Nusselt数在入口附近急剧下降,并在距入口一定的沿河方向的距离后达到完全展开值。此外,充分发展的局部努塞尔数在翅片间距为0.3和0.5的间隙间距为0.075和0.15时显示出明显的最大值。管道上的压降,自然对流速度和总Nusselt数与问题的控制参数密切相关。

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