This study examines the airside fin-and-tube heat exchangers having a larger diameter tube Dc = 16.59 mm) with the tube row ranging from 1 to 16. It is found that the effect of tube row on the heat transfer performance is quite significant, and the heat transfer performance deteriorates with the rise of tube row. The performance deteriorates with the rise of tube row. The performance drop is especially pronounced at the low Reynolds number region. Actually more than 85% drop of heat transfer performance is seen for Fp ∼ 1.7 mm as the row number is increased from 1 to 16. Upon the influence of tube row on the frictional performance, an unexpected row dependence of the friction factor is encountered. The effect of fin pitch on the airside performance is comparatively small for N = 1 or N = 2. However, a notable drop of heat transfer performance is seen when the number of tube row is increased, and normally higher heat transfer and frictional performance is associated with that of the larger fin pitch.
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2010 14th International Heat Transfer Conference
August 8–13, 2010
Washington, DC, USA
Conference Sponsors:
- Heat Transfer Division
ISBN:
978-0-7918-4939-2
PROCEEDINGS PAPER
Airside Performance of Wavy Fin-and-Tube Heat Exchangers: Data With Larger Diameter Tube
Huau Pao Lo,
Huau Pao Lo
National Chiao Tung University, Hsinchu, Taiwan
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Chinghua Hung,
Chinghua Hung
National Chiao Tung University, Hsinchu, Taiwan
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Chi-Chuan Wang
Chi-Chuan Wang
National Chiao Tung University, Hsinchu, Taiwan
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Huau Pao Lo
National Chiao Tung University, Hsinchu, Taiwan
Chinghua Hung
National Chiao Tung University, Hsinchu, Taiwan
Chi-Chuan Wang
National Chiao Tung University, Hsinchu, Taiwan
Paper No:
IHTC14-22409, pp. 423-428; 6 pages
Published Online:
March 1, 2011
Citation
Lo, HP, Hung, C, & Wang, C. "Airside Performance of Wavy Fin-and-Tube Heat Exchangers: Data With Larger Diameter Tube." Proceedings of the 2010 14th International Heat Transfer Conference. 2010 14th International Heat Transfer Conference, Volume 4. Washington, DC, USA. August 8–13, 2010. pp. 423-428. ASME. https://doi.org/10.1115/IHTC14-22409
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