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contributor authorS. C. Arora
contributor authorW. Abdel-Messeh
date accessioned2017-05-08T23:34:07Z
date available2017-05-08T23:34:07Z
date copyrightJuly, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28604#559_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107748
description abstractPin fins are commonly used as heat transfer augmentors for internal cooling of turbine airfoils. These pins may extend from one wall to the other or may be segmented to meet specific requirements of removing the airfoil’s varying heat load. Three configurations of the partial pins were tested in a channel with aspect ratio 25:1 and the results are compared with those for the full pins. The array average heat transfer rate decreases linearly with increasing gap and is bounded by the value for full pins at one end and that for the smooth channel at the other. However, the local distribution of the Nusselt number and the average for each of the two walls depends on the configuration of the partial pins. The friction factor was lower for partial pins than for the full pins and also decreased with increasing gap. For the configuration with all partial pins on one wall, the friction factor was found to be the lowest, with no change in the corresponding heat transfer rate from a wall with pins.
publisherThe American Society of Mechanical Engineers (ASME)
titleCharacteristics of Partial Length Circular Pin Fins As Heat Transfer Augmentors for Airfoil Internal Cooling Passages
typeJournal Paper
journal volume112
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927694
journal fristpage559
journal lastpage565
identifier eissn1528-8900
keywordsHeat transfer
keywordsCooling
keywordsFins
keywordsAirfoils
keywordsPins (Engineering)
keywordsFriction
keywordsChannels (Hydraulic engineering)
keywordsStress
keywordsHeat AND Turbines
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
contenttypeFulltext


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