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contributor authorZ. Wang
contributor authorP. T. Ireland
contributor authorT. V. Jones
date accessioned2017-05-08T23:48:38Z
date available2017-05-08T23:48:38Z
date copyrightApril, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28643#290_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116160
description abstractThe heat transfer coefficient over the surface of a pedestal with fillet radii has been measured using thermochromic liquid crystals and the transient heat transfer method. The tests were performed at engine representative Reynolds numbers for a geometry typical of those used in turbine blade cooling systems. The heat conduction process that occurs in the engine was subsequently modeled numerically with a finite element discretization of the solid pedestal. The measured heat transfer coefficients were used to derive the exact boundary conditions applicable to the engine. The temperature field within the pedestal, calculated using the correct heat transfer coefficient distribution, is compared to that calculated using an area-averaged heat transfer coefficient. Metal temperature differences of 90 K are predicted across the blade wall.
publisherThe American Society of Mechanical Engineers (ASME)
titleDetailed Heat Transfer Coefficient Measurements and Thermal Analysis at Engine Conditions of a Pedestal With Fillet Radii
typeJournal Paper
journal volume117
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2835658
journal fristpage290
journal lastpage297
identifier eissn1528-8900
keywordsMeasurement
keywordsEngines
keywordsThermal analysis
keywordsHeat transfer coefficients
keywordsTemperature
keywordsLiquid crystals
keywordsMetals
keywordsCooling systems
keywordsTransient heat
keywordsReynolds number
keywordsHeat conduction
keywordsTurbine blades
keywordsFinite element analysis
keywordsBlades
keywordsBoundary-value problems AND Geometry
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 002
contenttypeFulltext


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