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contributor authorN. Hay
contributor authorD. Lampard
date accessioned2017-05-08T23:58:12Z
date available2017-05-08T23:58:12Z
date copyrightApril, 1998
date issued1998
identifier issn0889-504X
identifier otherJOTUEI-28665#314_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121332
description abstractPublished information on the discharge coefficient of film cooling holes is classified in terms of the hole geometry, the external flow conditions at inlet and outlet, and the method of evaluation. This may be either theoretical or experimental. The information is reviewed primarily in the context of its use for evaluating discharge coefficients for conditions not directly covered by published data. It is shown that potential flow analyses can give acceptable accuracy for simple geometries with crossflows, while more complex cases require the use of correlated data, which may be incorporated in a range of predictive schemes. Deficiencies and inconsistencies in the published information are highlighted, and future developments are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleDischarge Coefficient of Turbine Cooling Holes: A Review
typeJournal Paper
journal volume120
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841408
journal fristpage314
journal lastpage319
identifier eissn1528-8900
keywordsCooling
keywordsTurbines
keywordsDischarge coefficient
keywordsFlow (Dynamics)
keywordsEvaluation methods AND Geometry
treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
contenttypeFulltext


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