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contributor authorA. Yamamoto
date accessioned2017-05-08T23:31:20Z
date available2017-05-08T23:31:20Z
date copyrightJuly, 1989
date issued1989
identifier issn0889-504X
identifier otherJOTUEI-28596#264_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106161
description abstractThis paper discusses the mechanisms of three-dimensional flows and of the associated losses occurring near the tip endwall region of a linear turbine cascade with tip clearance. The clearance gap sizes and the cascade incidences were chosen as the most important variables affecting the mechanisms. Flows close to the endwall and inside the clearance were surveyed in great detail using a micro five-hole pitot tube of 0.6 mm head size. The results gave very detailed information on the mechanisms, such as leakage flow vectors and pressure distributions throughout the clearance. Interaction of leakage flow with the endwall flow and their associated separation lines, effects of gap size and inlet flow angle on loss generation, and skewness of the three-dimensional endwall flows are also discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleEndwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance
typeJournal Paper
journal volume111
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262265
journal fristpage264
journal lastpage275
identifier eissn1528-8900
keywordsCascades (Fluid dynamics)
keywordsClearances (Engineering)
keywordsTurbines
keywordsBlades
keywordsFlow (Dynamics)
keywordsMechanisms
keywordsLeakage flows
keywordsPressure
keywordsSeparation (Technology) AND Flowmeters
treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 003
contenttypeFulltext


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