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Experimental investigation of the twist angle effects on thermo-hydraulic performance of a square and hexagonal pin fin array in forced convection

机译:强制对流中正方形和六边形销鳍阵列热水性能的试验研究

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This research deals with an experimental investigation to manage the thermo-hydraulic performance of the heat sink with pin fin array under forced convection at various design factors and operating conditions. Experimentation tests were performed on two pin fin section shapes of a square and hexagonal with four various twist angles (0, 30, 60, and 90°) at constant heat flux with air Reynolds number (Re) ranging from 3182 to 9971. The enhancement in Nusselt number (Nu) and heat transfer coefficient increased with the increase of twisting angle for the whole tested range of Re. The hexagonal cross-section produced an increment of Nu more than a square shape. The hexagonal fins with θ = 90° have higher Nu than other values of twisting angle. The enhancement in heat transfer and heat dissipation performed by square fin was more than hexagonal fins for all values of twisting angle. A decrease in the thermal resistance was recorded with the increase of Re, also, the twisted fins have lower thermal resistance than that of non-twisted pins. The friction factor and pressure drop reduces with an increase of twisting angle. The twisted fins have lower efficiency compared to no twisted fins. The HTPF of the hexagonal pin has the maximum value at twisting angle (θ) = 90° and the lowest value for the square pin at twisting angle (θ) = 30°. Dimensionless empirical general correlations were extracted from the experimental results of the current investigation with maximum deviations about ±8.9%, ±6.3%, and ± 10.6% for Nusselt number, fin efficiency, and friction factor, respectively.
机译:该研究涉及实验研究,以管理在各种设计因子和操作条件下用销钉阵列进行磁性水槽的热水力性能。在两根销鳍片部分的正方形和六边形的两个销翅片段形状上进行实验测试,其中四个各种扭曲角度(0,30,60和90°),在恒定的热量通量下,空气雷诺数(RE)从3182到9971的范围内。增强在露珠数(nu)和传热系数随着扭曲角度的扭曲角度的增加而增加。六边形横截面产生的腹部增量超过正方形。具有θ= 90°的六边形鳍具有比扭曲角度的其他值更高。由方形翅片进行的热传递和散热的增强超过六边形翅片,用于扭曲角度的所有值。随着RE的增加,记录了热阻的减小,也是扭曲的翅片具有比非扭曲引脚的热阻较低。随着扭曲角度的增加,摩擦因子和压降减少。与无扭曲翅片相比,扭转翅片具有较低的效率。六边形引脚的HTPF具有扭曲角度(θ)= 90°的最大值,并且在扭曲角度(θ)= 30°以平方销的最低值。从目前调查的实验结果中提取无量纲的经验一般相关性,其最大偏差分别具有较大的偏差约为±8.9%,±6.3%和±10.6%,分别进行营养号,鳍效率和摩擦因子。

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