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contributor authorL. S. Han
contributor authorW. R. Cox
date accessioned2017-05-08T23:15:36Z
date available2017-05-08T23:15:36Z
date copyrightJanuary, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26779#47_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97122
description abstractBoundary layer characteristics on the pressure-side of a turbine airfoil were investigated experimentally in a three-blade cascade tunnel. The blades had a chord length of 21 in. to facilitate flow visualization and high-speed photography. The investigation revealed the existence of the Gortler’s vortices appearing in spurts in regions of severe curvature. In the trailing edge region, Karman vortices were detected and found to interact strongly with the Gortler’s vortices convected thereto.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Visual Study of Turbine Blade Pressure-Side Boundary Layers
typeJournal Paper
journal volume105
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227397
journal fristpage47
journal lastpage52
identifier eissn0742-4795
keywordsPressure
keywordsTurbine blades
keywordsBoundary layers
keywordsVortices
keywordsBlades
keywordsTunnels
keywordsAirfoils
keywordsCascades (Fluid dynamics)
keywordsFlow visualization
keywordsChords (Trusses) AND Turbines
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001
contenttypeFulltext


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