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contributor authorJ. E. Doorly
date accessioned2017-05-08T23:28:37Z
date available2017-05-08T23:28:37Z
date copyrightApril, 1988
date issued1988
identifier issn0889-504X
identifier otherJOTUEI-28589#242_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104671
description abstractThe paper describes how thin film surface heat flux gages may be used to measure surface heat transfer rate to enamel-coated metal turbine blades. Flexible methods, which are also computationally efficient, for obtaining the heat transfer rate are described. Experimental results, using the new coated metal turbine blades and processing techniques, in a stationary transient cascade facility are given, and are shown to agree well with results using the existing method for gages on single-layer substrate blades. The application of the gages for measuring highly unsteady heat transfer is also discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleProcedures for Determining Surface Heat Flux Using Thin Film Gages on a Coated Metal Model in a Transient Test Facility
typeJournal Paper
journal volume110
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262187
journal fristpage242
journal lastpage250
identifier eissn1528-8900
treeJournal of Turbomachinery:;1988:;volume( 110 ):;issue: 002
contenttypeFulltext


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