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contributor authorJ. R. Mondt
contributor authorD. C. Siegla
date accessioned2017-05-09T01:38:07Z
date available2017-05-09T01:38:07Z
date copyrightApril, 1974
date issued1974
identifier issn1528-8919
identifier otherJETPEZ-26710#81_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164755
description abstractHeat transfer and flow friction behavior have been measured for plain and perforated plate-fin and 10-deg herringbone surfaces. For the range of geometries and Reynolds numbers studied, the perforations produced no significant improvement in heat transfer for the same pressure drop. Heat transfer behavior was determined with the “single blow” transient technique. The “initial rise” evaluation procedure was used for low Ntu test packs. Entrance length effects on both heat transfer and friction behavior were correlated for L/4rh as low as 45.
publisherThe American Society of Mechanical Engineers (ASME)
titlePerformance of Perforated Heat Exchanger Surfaces
typeJournal Paper
journal volume96
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445766
journal fristpage81
journal lastpage86
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsFriction
keywordsHeat transfer
keywordsReynolds number
keywordsHeat exchangers AND Pressure drop
treeJournal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 002
contenttypeFulltext


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