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可增材制造的偏置条形翅片传热结构不可逆熵产生的数值计算

Numerical Calculation of the Irreversible Entropy Production of Additively Manufacturable Off-Set Strip Fin Heat-Transferring Structures.

作者信息

Fuchs Marco, Lubos Nico, Kabelac Stephan

机构信息

Institute of Thermodynamics, Leibniz University Hannover, An der Universität 1, 30823 Garbsen, Germany.

出版信息

Entropy (Basel). 2023 Jan 13;25(1):162. doi: 10.3390/e25010162.

DOI:10.3390/e25010162
PMID:36673306
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC9857494/
Abstract

In this manuscript, off-set strip fin structures are presented which are adapted to the possibilities of additive manufacturing. For this purpose, the geometric parameters, including fin height, fin spacing, fin length, and fin longitudinal displacement, are varied, and the Colburn j-factor and the Fanning friction factor are numerically calculated in the Reynolds number range of 80-920. The structures are classified with respect to their entropy production number according to Bejan. This method is compared with the results from partial differential equations for the calculation of the irreversible entropy production rate due to shear stresses and heat conduction. This study reveals that the chosen temperature difference leads to deviation in terms of entropy production due to heat conduction, whereas the dissipation by shear stresses shows only small deviations of less than 2%. It is further shown that the variation in fin height and fin spacing has only a small influence on heat transfer and pressure drop, while a variation in fin length and fin longitudinal displacement shows a larger influence. With respect to the entropy production number, short and long fins, as well as large fin spacing and fin longitudinal displacement, are shown to be beneficial. A detailed examination of a single structure shows that the entropy production rate due to heat conduction is dominated by the entropy production rate in the wall, while the fluid has only a minor influence.

摘要

在本手稿中,提出了适用于增材制造可能性的偏移条形翅片结构。为此,改变了包括翅片高度、翅片间距、翅片长度和翅片纵向位移在内的几何参数,并在80 - 920的雷诺数范围内对科尔伯恩j因子和范宁摩擦因子进行了数值计算。根据贝扬的方法,这些结构按照其熵产生数进行分类。将该方法与用于计算由于剪切应力和热传导导致的不可逆熵产生率的偏微分方程的结果进行了比较。该研究表明,所选择的温差会导致由于热传导引起的熵产生出现偏差,而由剪切应力引起的耗散仅显示出小于2%的小偏差。进一步表明,翅片高度和翅片间距的变化对传热和压降的影响很小,而翅片长度和翅片纵向位移的变化则显示出较大影响。就熵产生数而言,短翅片和长翅片以及大的翅片间距和翅片纵向位移是有益的。对单个结构的详细研究表明,由于热传导引起的熵产生率主要由壁中的熵产生率主导,而流体的影响较小。

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本文引用的文献

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Entropy (Basel). 2020 Feb 14;22(2):215. doi: 10.3390/e22020215.