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contributor authorR. D. Stieger
contributor authorH. P. Hodson
date accessioned2017-05-09T00:14:38Z
date available2017-05-09T00:14:38Z
date copyrightOctober, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28715#536_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130953
description abstractA detailed experimental investigation was conducted into the interaction of a convected wake and a separation bubble on the rear suction surface of a highly loaded low-pressure (LP) turbine blade. Boundary layer measurements, made with 2D LDA, revealed a new transition mechanism resulting from this interaction. Prior to the arrival of the wake, the boundary layer profiles in the separation region are inflexional. The perturbation of the separated shear layer caused by the convecting wake causes an inviscid Kelvin-Helmholtz rollup of the shear layer. This results in the breakdown of the laminar shear layer and a rapid wake-induced transition in the separated shear layer.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Transition Mechanism of Highly Loaded Low-Pressure Turbine Blades
typeJournal Paper
journal volume126
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1773850
journal fristpage536
journal lastpage543
identifier eissn1528-8900
keywordsSeparation (Technology)
keywordsTurbine blades
keywordsWakes
keywordsBoundary layers
keywordsMechanisms
keywordsShear (Mechanics)
keywordsPressure
keywordsTurbulence
keywordsMeasurement
keywordsFlow (Dynamics) AND Blades
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 004
contenttypeFulltext


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