Heat Transfer Enhancement for Finned-Tube Heat Exchangers With Winglets

J. O'Brien, M. Sohal
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引用次数: 37

Abstract

This paper presents the results of an experimental study of forced convection heat transfer in a narrow rectangular duct fitted with a circular tube and/or a delta-winglet pair. The duct was designed to simulate a single passage in a fin-tube heat exchanger. Heat transfer measurements were obtained using a transient technique in which a heated airflow is suddenly introduced to the test section. High-resolution local fin-surface temperature distributions were obtained at several times after initiation of the transient using an imaging infrared camera. Corresponding local fin-surface heat transfer coefficient distributions were then calculated from a locally applied one-dimensional semi-infinite inverse heat conduction model. Heat transfer results were obtained over an airflow rate ranging from 1.51 × 10−3 to 14.0 × 10−3 kg/s. These flow rates correspond to a duct-height Reynolds number range of 670–6300 with a duct height of 1.106 cm and a duct width-to-height ratio, W/H, of 11.25. The test cylinder was sized such that the diameter-to-duct height ratio, D/H is 5. Results presented in this paper reveal visual and quantitative details of local fin-surface heat transfer distributions in the vicinity of a circular tube, a delta-winglet pair, and a combination of a circular tube and a delta-winglet pair. Comparisons of local and average heat transfer distributions for the circular tube with and without winglets are provided. Overall mean fin-surface Nusselt-number results indicate a significant level of heat transfer enhancement associated with the deployment of the winglets with the circular cylinder. At the lowest Reynolds numbers (which correspond to the laminar operating conditions of existing geothermal aircooled condensers), the enhancement level is nearly a factor of two. At higher Reynolds numbers, the enhancement level is close to 50%.
带小翼翅片管换热器的强化传热研究
本文介绍了在装有圆管和/或三角小翼对的窄矩形管道中强制对流换热的实验研究结果。该管道被设计成模拟翅片管换热器的单通道。传热测量是使用一种瞬态技术获得的,其中加热气流突然引入测试部分。利用红外成像相机获得了瞬态启动后几次高分辨率的局部鳍表面温度分布。然后根据局部应用的一维半无限逆热传导模型计算相应的翅片-表面局部传热系数分布。在1.51 × 10−3 ~ 14.0 × 10−3 kg/s的气流速率范围内,获得了传热结果。这些流量对应的风管高度雷诺数范围为670-6300,风管高度为1.106 cm,风管宽高比W/H为11.25。试验筒的尺寸使直径与管道高度比D/H为5。本文的结果揭示了在圆管、三角-小翼对以及圆管和三角-小翼对组合附近的翅片-表面局部传热分布的视觉和定量细节。比较了带小翼和不带小翼圆管的局部和平均传热分布。总体平均翅片表面努塞尔数结果表明,与小翼与圆柱体的展开相关的传热增强显著水平。在最低雷诺数下(对应于现有地热空冷冷凝器的层流运行条件),增强水平几乎是两倍。在较高的雷诺数下,增强水平接近50%。
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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