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Numerical estimation of pressure drop and heat transfer characteristics in annular-finned channel heat exchangers with different channel configurations

机译:不同通道结构的环形翅片通道换热器中压降和传热特性的数值估算

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In this numerical investigation, three-dimensional analysis has been used to study the effect of finned channels configuration of (circular, square, and triangular shape) and fin spacing with four rows in staggered arrangements. The finite volume method with k-ω turbulent model is applied to estimate the heat transfer and flow characteristics. The results illustrate that the development of the boundary layer between the fins surfaces is credited to the finned channels configuration, fin spacing, and Reynolds number. Moreover, the results of pressure drop and heat transfer with various channel configuration and different fin spacings (1.6, 2, and 4 mm) are presented and validated with the available correlations. The triangular-finned channel with 1.6 mm fin spacing offered higher heat transfer enhancement followed by square- and circular-finned channels. A considerable agreement was observed when the current findings and the existing correlations were compared, with a maximum deviation of 15% for all the cases.
机译:在此数值研究中,已使用三维分析来研究翅片通道结构(圆形,正方形和三角形)和四排交错排列的翅片间距的影响。采用k-ω湍流模型的有限体积方法来估计传热和流动特性。结果表明,翅片表面之间的边界层的发展归因于翅片通道结构,翅片间距和雷诺数。此外,还介绍了具有各种通道配置和不同翅片间距(1.6、2和4 mm)的压降和传热结果,并通过可用的相关性进行了验证。翅片间距为1.6 mm的三角形翅片通道可提供更高的传热效果,其次是方形翅片和圆形翅片通道。当比较当前发现和现有相关性时,观察到了相当大的共识,在所有情况下最大偏差为15%。

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