LAPSE:2023.8092
Published Article

LAPSE:2023.8092
Thermal Visualization and Performance Analysis in a Channel Installing Transverse Baffles with Square Wings
February 24, 2023
Abstract
The experimental examination of local heat transfer, thermal intensification, friction factors, and thermal performance factors (TPF) in a rectangular channel with square-winged transverse baffles (SW-TB) are presented in this paper. The purpose of this study is to modify the typical transverse baffles (TB) into square-winged transverse baffles (SW-TB) in order to improve the thermal performance and heat transfer rate of the channel. The effects of SW-TBs with various wing attack angles and Reynolds numbers on the heat transfer performance characteristics were examined using a thermochromic liquid crystal sheet. In the experiments, the SW-TBs were attached to the bottom wall of the channel, which had an aspect ratio (W:H) of 3.75:1. The SW-TBs had a width (w) of 150 mm, a square perforated cross-sectional area (a × b) of 8 × 8 mm2, and attack angles (θ) of 0° (solid transverse-baffle), 22.5°, 45°, 67.5°, and 90°. The bottom wall of the channel was evenly heated, while the other walls were insulated. The temperature contours on the heated surface were plotted using temperatures obtained through using the thermochromic liquid crystal (TLC) image-processing method. Experimental results revealed that the SW-TBs created multiple impinging jets, apart from the recirculation. At the proper attack angles (θ = 22.5° and 45°), the SW-TBs offered greater heat transfer rates and caused lower friction losses, resulting in higher TPFs than the solid transverse baffles. In the current work, channels where the SW-TBs display a θ = 45° presented the greatest TPF, as high as 1.26. The multiple impinging jets issuing by the SW-TBs suppressed the size of the recirculation flow and allowed better contact between the fluid flow and channel wall.
The experimental examination of local heat transfer, thermal intensification, friction factors, and thermal performance factors (TPF) in a rectangular channel with square-winged transverse baffles (SW-TB) are presented in this paper. The purpose of this study is to modify the typical transverse baffles (TB) into square-winged transverse baffles (SW-TB) in order to improve the thermal performance and heat transfer rate of the channel. The effects of SW-TBs with various wing attack angles and Reynolds numbers on the heat transfer performance characteristics were examined using a thermochromic liquid crystal sheet. In the experiments, the SW-TBs were attached to the bottom wall of the channel, which had an aspect ratio (W:H) of 3.75:1. The SW-TBs had a width (w) of 150 mm, a square perforated cross-sectional area (a × b) of 8 × 8 mm2, and attack angles (θ) of 0° (solid transverse-baffle), 22.5°, 45°, 67.5°, and 90°. The bottom wall of the channel was evenly heated, while the other walls were insulated. The temperature contours on the heated surface were plotted using temperatures obtained through using the thermochromic liquid crystal (TLC) image-processing method. Experimental results revealed that the SW-TBs created multiple impinging jets, apart from the recirculation. At the proper attack angles (θ = 22.5° and 45°), the SW-TBs offered greater heat transfer rates and caused lower friction losses, resulting in higher TPFs than the solid transverse baffles. In the current work, channels where the SW-TBs display a θ = 45° presented the greatest TPF, as high as 1.26. The multiple impinging jets issuing by the SW-TBs suppressed the size of the recirculation flow and allowed better contact between the fluid flow and channel wall.
Record ID
Keywords
channel, heat transfer, square-winged transverse baffles, thermal performance
Subject
Suggested Citation
Eiamsa-Ard S, Phila A, Wongcharee K, Chuwattanakul V, Pimsarn M, Maruyama N, Hirota M. Thermal Visualization and Performance Analysis in a Channel Installing Transverse Baffles with Square Wings. (2023). LAPSE:2023.8092
Author Affiliations
Eiamsa-Ard S: Division of System Engineering, Graduate School of Engineering, Mie University, Tsu 514-8507, Japan; Department of Mechanical Engineering, Mahanakorn University of Technology, Bangkok 10530, Thailand [ORCID]
Phila A: Department of Mechanical Engineering, Mahanakorn University of Technology, Bangkok 10530, Thailand
Wongcharee K: Department of Mechanical Engineering, Mahanakorn University of Technology, Bangkok 10530, Thailand
Chuwattanakul V: School of Engineering, King Mongkut’s Institute of Technology Ladkrabang, Bangkok 10520, Thailand
Pimsarn M: School of Engineering, King Mongkut’s Institute of Technology Ladkrabang, Bangkok 10520, Thailand [ORCID]
Maruyama N: Division of Mechanical Engineering, Graduate School of Engineering, Mie University, Tsu 514-8507, Japan; Engineering Innovation Unit, Graduate School of Regional Innovation Studies, Mie University, Tsu 514-8507, Japan
Hirota M: Division of Mechanical Engineering, Graduate School of Engineering, Mie University, Tsu 514-8507, Japan
Phila A: Department of Mechanical Engineering, Mahanakorn University of Technology, Bangkok 10530, Thailand
Wongcharee K: Department of Mechanical Engineering, Mahanakorn University of Technology, Bangkok 10530, Thailand
Chuwattanakul V: School of Engineering, King Mongkut’s Institute of Technology Ladkrabang, Bangkok 10520, Thailand
Pimsarn M: School of Engineering, King Mongkut’s Institute of Technology Ladkrabang, Bangkok 10520, Thailand [ORCID]
Maruyama N: Division of Mechanical Engineering, Graduate School of Engineering, Mie University, Tsu 514-8507, Japan; Engineering Innovation Unit, Graduate School of Regional Innovation Studies, Mie University, Tsu 514-8507, Japan
Hirota M: Division of Mechanical Engineering, Graduate School of Engineering, Mie University, Tsu 514-8507, Japan
Journal Name
Energies
Volume
15
Issue
22
First Page
8736
Year
2022
Publication Date
2022-11-20
ISSN
1996-1073
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Original Submission
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PII: en15228736, Publication Type: Journal Article
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LAPSE:2023.8092
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https://doi.org/10.3390/en15228736
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Feb 24, 2023
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