插入v-下游小翼紊流器的方管换热器内空气的传热与流动特性

Q3 Agricultural and Biological Sciences Asia-Pacific Journal of Science and Technology Pub Date : 2015-12-18 DOI:10.14456/KKURJ.2015.33
et.al Suriya Chokphoemphun
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引用次数: 0

摘要

本文在恒定壁面热流密度条件下,在雷诺数(Re)为4000 ~ 26000的紊流状态下,对插入45o v下游小翼紊流器的方形管换热器进行了换热强化和热性能的实验研究。四种不同节距的影响;将P=22.5、33.75、45和90 mm (PR=P/H=0.5、0.75、1和2)和3个不同小翼高度e=6.75、9和11.25 mm (BR=e/H=0.15、0.2和0.25)对角插入,放置在核心流道内,观察以努塞尔数(Nu)表示的换热率、以摩擦系数(f)表示的压力损失和热性能(f)。结果表明,45o v下游小翼在不同工况下Nu和f分别比光滑表面高6.0 ~ 8.7倍和37 ~ 170倍,热性能约为1.50 ~ 2.06。在Re=4100, BR=0.2, PR=1.0条件下,采用45o v下游小翼紊流器的最大热性能为2.06。
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Heat transfer and fluid flow behavior of air in square duct heat exchanger inserted with v-downstream winglet turbulators
This work present the experimental investigation on heat transfer enhancement and thermal performance in a square-duct heat exchanger inserted with 45o V-downstream winglet turbulator is carried out by varying velocity of air in the turbulent regime for Reynolds numbers (Re) ranging from 4000 to 26,000 in the test section with a constant wall heat flux condition. Influents of four different pitch lengths; P=22.5, 33.75, 45 and 90 mm (PR=P/H=0.5, 0.75, 1 and 2) and three different winglet heights, e=6.75, 9 and 11.25 mm (BR=e/H=0.15, 0.2 and 0.25) were inserted diagonally and placed in the core flow area into the test duct on heat transfer rates in the term of Nusselt number (Nu), pressure loss in form of friction factor (f) and thermal performance (). It was found that the 45o V-downstream winglet is provided the Nu and f higher than the smooth surface around 6.0 to 8.7 times and 37 to 170 times, respectively depending upon operating conditions while the thermal performance are about 1.50–2.06. The maximum thermal performance for using 45o V-downstream winglet turbulator is 2.06 at Re=4100, BR=0.2 and PR=1.0 in this experiment.
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来源期刊
Asia-Pacific Journal of Science and Technology
Asia-Pacific Journal of Science and Technology Agricultural and Biological Sciences-Agricultural and Biological Sciences (all)
CiteScore
0.90
自引率
0.00%
发文量
0
审稿时长
8 weeks
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