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Numerical and experimental methods for heat transfer enhancement for finned-tube heat exchangers with oval tubes

机译:具有椭圆管翅片管热交换器的传热增强的数值和实验方法

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This paper presents the results of an experimental and numerical study of forced convection heat transfer in a narrow rectangular duct fitted with an oval tube. The duct was designed to simulate a single passage in a fin-tube heat exchanger. The objective of this paper is to determine the suitability of numerical methods as a tool for predicting the effectiveness of oval tubes and winglets for heat transfer enhancement. Heat transfer measurements were obtained experimentally 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 was predicted numerically using a three-dimensional computational model of the test section that was developed to accurately predict fin-surface heat transfer coefficient distributions. Comparisons of numerical and experimental results are made at Reynolds numbers based on channel height, Re{sub}H, of 500 and 1240, the normal range of operation of air-cooled heat exchangers in geothermal applications. These Re{sub}H values correspond to an air frontal velocity of 1.0 m/s and 2.5 m/s respectively. The elliptical tube had a major axis to minor axis aspect ratio, a/b of 3:1 and a/H equal to 4.33. Results presented in this paper reveal visual and quantitative details of local fin-surface heat transfer distributions in the vicinity of an oval tube obtained both numerically and experimentally. Comparisons of numerical and experimental results show good agreement, however the numerical results are consistently higher in value. Several possible explanations for this difference are identified that will be investigated further.
机译:本文介绍了椭圆形管窄矩形管道中强制对流传热的实验和数值研究的结果。设计管道设计用于在翅片管热交换器中模拟单个通道。本文的目的是确定数值方法作为预测热传递增强的椭圆管和小翼效果的工具的适用性。实验使用其中加热的气流被突然引入到测试段的瞬时技术得到的热传递测量。使用成像红外相机在瞬态启动后几次获得高分辨率局部翅片表面温度分布。然后根据局部施加的一维半无限逆热传导模型计算相应的局部翅片表面传热系数分布。传热进行数值使用的开发是为了准确地预测翅片表面传热系数分布测试部分的三维计算模型预测。数值和实验结果的比较在基于通道高度,Re {Sub} H,500和1240的雷诺数,在地热应用中的风冷热交换器的正常操作范围。这些RE {sub} H值分别对应于1.0 m / s和2.5 m / s的空气额速度。椭圆管的主要轴为短轴纵横比,3:1的A / B和A / H等于4.33。本文提出的结果揭示了在数值和实验上获得的椭圆形管附近的局部翅片表面传热分布的视觉和定量细节。数值和实验结果的比较表现出良好的一致性,但数值结果始终如一的价值。鉴定了几种可能的解释该差异,将进一步调查。

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