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contributor authorLesley M. Wright
contributor authorWen-Lung Fu
contributor authorJe-Chin Han
date accessioned2017-05-09T00:14:39Z
date available2017-05-09T00:14:39Z
date copyrightOctober, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28715#604_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130962
description abstractAn experimental study was performed to measure the heat transfer distributions and frictional losses in rotating ribbed channels with an aspect ratio of 4:1. Angled, discrete angled, V-shaped, and discrete V-shaped ribs were investigated, as well as the newly proposed W-shaped and discrete W-shaped ribs. In all cases, the ribs are placed on both the leading and trailing surfaces of the channel, and they are oriented 45 deg to the mainstream flow. The rib height-to-hydraulic diameter ratio (e/D) is 0.078, and the rib pitch-to-height ratio (P/e) is 10. The channel orientation with respect to the direction of rotation is 135 deg. The range of flow parameters includes Reynolds number (Re=10,000–40,000), rotation number (Ro=0.0–0.15), and inlet coolant-to-wall density ratio (Δρ/ρ=0.12). Both heat transfer and pressure measurements were taken, so the overall performance of each rib configuration could be evaluated. It was determined that the W-shaped and discrete W-shaped ribs had the superior heat transfer performance in both nonrotating and rotating channels. However, these two configurations also incurred the greatest frictional losses while the discrete V-shaped and discrete angled ribs resulted in the lowest pressure drop. Based on the heat transfer enhancement and the pressure drop penalty, the discrete V-shaped ribs and the discrete W-shaped ribs exhibit the best overall thermal performance in both rotating and nonrotating channels. These configurations are followed closely by the W-shaped ribs. The angled rib configuration resulted in the worst performance of the six configurations of the present study.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR=4:1)
typeJournal Paper
journal volume126
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1791286
journal fristpage604
journal lastpage614
identifier eissn1528-8900
keywordsHeat transfer
keywordsChannels (Hydraulic engineering)
keywordsCooling AND Rotation
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 004
contenttypeFulltext


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