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首页> 外文期刊>WSEAS Transactions on Heat and Mass Transfer >Effect of Fin Array Parameters on Variation in Heat Transfer Coefficient for Natural Convection in Fin
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Effect of Fin Array Parameters on Variation in Heat Transfer Coefficient for Natural Convection in Fin

机译:翅片阵列参数对翅片自然对流换热系数变化的影响

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摘要

Fins are usually analyzed by assuming uniform heat transfer coefficient model on its surface. However, studies by various investigators revealed that it is not constant but varies along the fin length. It is mainly because of non-uniform resistance experienced by the fluid flow in the inter fin region. Obviously, this variation is functions of fin array parameters such as inter fin spacing (S), fin height (Hf) & fin tip clearance (C) as they largely influence the resistance to the fluid flow. The objective of the present work is to establish experimental relationship between the variations in the heat transfer coefficient along the fin height (Length) with respect to the fin array parameters fin spacing (S), fin height (Hf) & fin tip clearance (C). Experiments were performed for five different values of inter fin spacing (S) and tip clearance (C) and best fit curve of the type h = ax{sup}n was obtained. The values of 'a' and 'n' were then correlated with the appropriate dimensionless fin array parameters thus variation in the heat transfer coefficient with respect to the fin array parameters is obtained It is found that average heat transfer coefficient varies hyperbolically (for constant clearance C= 6) with respect to S/Hf Also the value of n is fairly constant at 0.065 while value of a is decreasing as (S) inter-fin spacing is increasing indicating that the average value of 'h' also decreases with increase in 'S'. It is found that average heat transfer coefficient varies parabolically (for constant inert-fin spacing S= 5.5cm) with respect to C/S with minima occurring around C/S =0.55 Also the value of n is decreasing with increasing clearance and at C=6it again increases indicating rise in heat transfer coefficient
机译:通常通过假设散热片表面均匀的传热系数模型来分析散热片。然而,各种研究人员的研究表明,它不是恒定的,而是沿鳍片长度变化。这主要是由于翅片间区域中的流体流动所经历的阻力不均匀。显然,这种变化是鳍阵列参数的函数,例如鳍间间距(S),鳍高(Hf)和鳍尖端间隙(C),因为它们极大地影响了对流体流动的阻力。本工作的目的是建立相对于翅片阵列参数,翅片间距(S),翅片高度(Hf)和翅片尖端间隙(C)的沿翅片高度(Length)的传热系数变化之间的实验关系。 )。针对翅片间距(S)和尖端间隙(C)的五个不同值进行了实验,并获得了h = ax {sup} n类型的最佳拟合曲线。然后将'a'和'n'的值与适当的无量纲翅片阵列参数相关联,从而获得相对于翅片阵列参数的传热系数变化。发现平均传热系数双曲线变化(对于恒定间隙)相对于S / Hf,C = 6)n的值也相当恒定,为0.065,而随着(S)鳍间距的增加,a的值减小,这表明'h'的平均值也随着S / Hf的增加而减小。 'S'。发现平均传热系数相对于C / S呈抛物线变化(对于恒定的惰性散热片间距S = 5.5cm),并且在C / S = 0.55处出现最小值,并且随着间隙的增加和在C处n的值减小= 6它再次增加,表明传热系数增加

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