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contributor authorKirsch, Kathryn L.
contributor authorOstanek, Jason K.
contributor authorThole, Karen A.
date accessioned2017-05-09T01:13:20Z
date available2017-05-09T01:13:20Z
date issued2014
identifier issn0889-504X
identifier otherturbo_136_04_041015.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156539
description abstractPin fin arrays are most commonly used to promote convective cooling within the internal passages of gas turbine airfoils. Contributing to the heat transfer are the surfaces of the channel walls as well as the pin itself. Generally the pin fin cross section is circular; however, certain applications benefit from using other shapes such as oblong pin fins. The current study focuses on characterizing the heat transfer distribution on the surface of oblong pin fins with a particular focus on pin spacing effects. Comparisons were made with circular cylindrical pin fins, where both oblong and circular cylindrical pins had a heighttodiameter ratio of unity, with both streamwise and spanwise spacing varying between two and three diameters. To determine the effect of relative pin placement, measurements were taken in the first of a single row and in the third row of a multirow array. Results showed that areaaveraged heat transfer on the pin surface was between 30 and 35% lower for oblong pins in comparison to cylindrical. While heat transfer on the circular cylindrical pin experienced one minimum prior to boundary layer separation, heat transfer on the oblong pin fins experienced two minimums, where one is located before the boundary layer transitions to a turbulent boundary layer and the other prior to separation at the trailing edge.
publisherThe American Society of Mechanical Engineers (ASME)
titleComparison of Pin Surface Heat Transfer in Arrays of Oblong and Cylindrical Pin Fins
typeJournal Paper
journal volume136
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025213
journal fristpage41015
journal lastpage41015
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 004
contenttypeFulltext


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