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Heat transportation performance and entropy generation analysis of Iron (II, III) oxide microparticles on Taylor Couette flow over a slit wall

Authors
Sun, S.-L.Liu, D.Wang, Y.-Z.Qi, Y.-L.Kim, H.-B.
Issue Date
Dec-2022
Publisher
Pergamon Press Ltd.
Keywords
Entropy generation analysis; Eulerian-Lagrangian method; Heat transfer; Suspension; Taylor-Couette flow
Citation
International Communications in Heat and Mass Transfer, v.139
Indexed
SCIE
SCOPUS
Journal Title
International Communications in Heat and Mass Transfer
Volume
139
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/29926
DOI
10.1016/j.icheatmasstransfer.2022.106479
ISSN
0735-1933
1879-0178
Abstract
Despite the significance of Taylor Couette flow over a slit wall in industries, little is known about the impact of Iron (II, III) oxide (Fe3O4) microparticle on the dynamics and heat transfer properties of Taylor-Couette flow. This study aims to investigate the effect of solid particles on heat transfer performance of Taylor-Couette flow over a slit wall. The trajectory of particles in the flow field is described utilizing Eulerian-Lagrangian method in this report. The Fe3O4-water suspension with particle size dp = 1μm, 5μm and particle volume fraction φ = 0.5 %, 1.0 %, 1.5% are considered. Results reveal that the heat transfer performance of Taylor vortex is remarkable enhanced by adding the solid particles inside the annular gap compared to pure water. Solid particles in the annular gap show the movement of migration from inner to outer cylinders due to the interaction with fluid, which causes more disordered flow field around the inner cylinder. The addition of particles could significantly thin the velocity and temperature boundary layers. Frictional and thermal entropy generation display a reverse tendency with increasing particle volume fraction and size. Thermal entropy generation appears obviously higher than frictional entropy generation. Suspension with φ = 1.5% and dp = 1μm makes optimal performance of Taylor vortex because of the minimum entropy generation and boundary layers. © 2022 Elsevier Ltd
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대학원 (기계항공우주공학부)
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