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contributor authorLedezma, Gustavo A.
contributor authorBunker, Ronald S.
date accessioned2017-05-09T01:24:19Z
date available2017-05-09T01:24:19Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_01_011002.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159870
description abstractThis article presents a geometric optimization study to maximize the total heat transfer rate between an array of discrete pin fins and the surrounding serpentine cooling flow. The fins are installed on the tip cap underside of a highpressure turbine blade (HPTB) model. The study has three parts. In the first, the numerical model is validated against experimental data obtained with liquid crystal thermography. In the second part, the heat and fluid flow performance of the pin fin assembly is simulated numerically, using RANS turbulence models in the range 25,000 < Re < 100,000 and Pr ∼ 0.7. The effect of varying the spacing and the tip cap boundary condition is investigated. In the last part of the study, it is shown that the optimal spacing between the pin fins can be correlated following the same theoretical arguments derived in the previous investigations that used simpler geometries.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Optimal Distribution of Pin Fins for Blade Tip Cap Underside Cooling
typeJournal Paper
journal volume137
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4028290
journal fristpage11002
journal lastpage11002
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 001
contenttypeFulltext


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