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Cited 11 time in webofscience Cited 13 time in scopus
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Slit Wall and Heat Transfer Effect on the Taylor Vortex Flowopen access

Authors
Liu, DongWang, Ying-ZeShi, Wei-DongKim, Hyoung-BumTang, Ai-Kun
Issue Date
Mar-2015
Publisher
MDPI
Keywords
Heat transfer; Numerical simulation; Particle image velocimetry (PIV); Slit number; Taylor vortex flow
Citation
ENERGIES, v.8, no.3, pp 1958 - 1974
Pages
17
Indexed
SCIE
SCOPUS
Journal Title
ENERGIES
Volume
8
Number
3
Start Page
1958
End Page
1974
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/17391
DOI
10.3390/en8031958
ISSN
1996-1073
1996-1073
Abstract
The Taylor vortex flow in the plain model with a constant temperature gradient effect was studied by experimental measurement, and the preliminary features of Taylor vortex flow affected by heat transfer process were obtained. This flow field in the plain model was also studied by numerical simulation. The reliability of numerical simulation was verified by comparing the numerical results with the experimental ones. To study the slit wall effect on this flow regime under the same temperature gradient conditions, another three models with different slit numbers (6, 9 and 12) were considered. The vortex pairs were found to have a motion along the axial direction. Because of the existence of the temperature gradient, the axial flow in the annulus gap was enhanced, but the radial velocity near the inner cylinder was found to be weakened. The heat flux generated by the inner cylinder was also compared among different models, and it was found that the heat flux generated by the 6-slit model was increased by 4.5% compared to that of the plain model, and the 12-slit model generated the maximum heat flux, which has the best heat transfer ability.
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공학계열 > 기계항공우주공학부 > Journal Articles

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Kim, Hyoung Bum
대학원 (기계항공우주공학부)
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