Effect of peak-to-peak amplitude at the base of crimped spiral fins on the air-side performance of crimped spiral fin-and-tube heat exchangers

IF 2.2 Q2 ENGINEERING, MULTIDISCIPLINARY
Thawatchai Keawkamrop, Somchai Wongwises
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Abstract

This experimental study investigates the effect of peak-to-peak amplitude (PTPA) at the base of a crimped spiral fin (CSF) on the air-side performance of a crimped spiral fin-and-tube heat exchanger (CSFTHX) within a 3000 to 14,000 Reynolds number range. Both plain spiral fins (PSFs) and CSFs are examined. The PTPA is the main geometric parameter of interest in this study. We investigated CSFTHXs with a 19.05 mm outer tube diameter, a fin density of 5 fins per inch (equivalent to a fin pitch of 5.08 mm). The selected peak-to-peak amplitude (PTPA) values—2.5 mm (low), 3.5 mm (medium), and 5.08 mm (high)—cover a representative range commonly used in industrial applications. The results indicate that variations in the PTPA have an insignificant effect on the Colburn factor, suggesting minimal influence on heat transfer performance. However, the PTPA has a significant effect on the friction factor, with higher PTPA values resulting in increased pressure drops. The fin factor, defined as the ratio between the percentage increase in the convective heat transfer coefficient and the corresponding percentage increase in pressure drop, is used for the investigation. For the air frontal velocities above 2 m/s, the fin factor of the CSF with a PTPA of 2.50 mm is higher than those with PTPA values of 3.50 mm and 5.08 mm. This indicates better overall performance in terms of a heat transfer-to-pressure drop trade-off at lower amplitudes.
卷曲螺旋翅片底部峰间振幅对卷曲螺旋翅片管换热器空气侧性能的影响
本实验研究了在3000 ~ 14000雷诺数范围内,卷曲螺旋翅片(CSF)底部的峰峰振幅(PTPA)对卷曲螺旋翅片管换热器(CSFTHX)空气侧性能的影响。对平面螺旋鳍和螺旋鳍进行了研究。PTPA是本研究的主要几何参数。我们研究的csfthx外管直径为19.05 mm,鳍密度为每英寸5个鳍(相当于鳍间距为5.08 mm)。所选的峰对峰振幅(PTPA)值- 2.5 mm(低),3.5 mm(中)和5.08 mm(高)-涵盖了工业应用中常用的代表性范围。结果表明,PTPA的变化对Colburn因子的影响不显著,表明对换热性能的影响很小。然而,PTPA对摩擦系数有显著影响,PTPA值越高,压降越大。翅片系数定义为对流换热系数增加百分比与相应的压降增加百分比之比,用于研究。在锋面速度大于2 m/s时,PTPA为2.50 mm时的尾翼系数高于PTPA为3.50 mm和5.08 mm时的尾翼系数。这表明在较低振幅下传热与压降权衡方面的整体性能更好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Applications in engineering science
Applications in engineering science Mechanical Engineering
CiteScore
3.60
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0.00%
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审稿时长
68 days
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