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contributor authorKirsch, Kathryn L.
contributor authorThole, Karen A.
date accessioned2017-05-09T01:24:37Z
date available2017-05-09T01:24:37Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_07_071004.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159940
description abstractPin fin arrays are employed as an effective means for heat transfer enhancement in the internal passages of a gas turbine blade, specifically in the blade's trailing edge. Various shapes of the pin itself have been used in such arrays. In this study, oblong pin fins are investigated whereby their long axis is perpendicular to the flow direction. Heat transfer measurements were taken at the pin midspan with unheated endwalls to isolate the pin heat transfer. Results show important differences in the heat transfer patterns between a pin in the first row and a pin in the third row. In the third row, wider spanwise spacing allows for two peaks in heat transfer over the pin surface. Additionally, closer streamwise spacing leads to consistently higher heat transfer for the same spanwise spacing. Due to the blunt orientation of the pins, the peak in heat transfer occurs off the stagnation point.
publisherThe American Society of Mechanical Engineers (ASME)
titleHeat Transfer Measurements of Oblong Pins
typeJournal Paper
journal volume137
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4029124
journal fristpage71004
journal lastpage71004
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 007
contenttypeFulltext


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