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contributor authorHyung Hee Cho
contributor authorDong Ho Rhee
date accessioned2017-05-09T00:06:16Z
date available2017-05-09T00:06:16Z
date copyrightJuly, 2001
date issued2001
identifier issn0889-504X
identifier otherJOTUEI-28689#601_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126035
description abstractThe present study is conducted to investigate the local heat/mass transfer characteristics for flow through perforated plates. A naphthalene sublimation method is employed to determine the local heat/mass transfer coefficients on the effusion plate. Two parallel perforated plates are arranged in two different configurations: staggered and shifted in one direction. The experiments are conducted for hole pitch-to-diameter ratios of 6.0, for gap distance between the perforated plates of 0.33 to 10 hole diameters, and for Reynolds numbers of 5000 to 12,000. The result shows that the high transfer region is formed at stagnation region and at the midline of the adjacent impinging jets due to secondary vortices and flow acceleration to the effusion hole. For flows through the perforated plates, the mass transfer rates on the surface of the effusion plate are about six to ten times higher than for effusion cooling alone (single perforated plate). In general, higher heat/mass transfer is obtained with smaller gap distance between two perforated plates.
publisherThe American Society of Mechanical Engineers (ASME)
titleLocal Heat/Mass Transfer Measurement on the Effusion Plate in Impingement/Effusion Cooling Systems
typeJournal Paper
journal volume123
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1344904
journal fristpage601
journal lastpage608
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsHeat
keywordsMass transfer
keywordsJets
keywordsVortices
keywordsPlates (structures)
keywordsReynolds number
keywordsCooling AND Cooling systems
treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 003
contenttypeFulltext


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