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contributor authorR. I. Crane
contributor authorG. Leoutsakos
contributor authorJ. Sabzvari
date accessioned2017-05-08T23:26:05Z
date available2017-05-08T23:26:05Z
date copyrightApril, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28583#296_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103252
description abstractLaminar-to-turbulent transition in the presence of Görtler vortices has been investigated experimentally, in the outer wall boundary layer of a curved water channel. Ratios of boundary layer thickness at the start of curvature to wall radius were around 0.05 and core flow turbulence intensities were between 1 and 3 percent. Measurements of intermittency factor were made by hot film probe and of mean and rms velocity by laser anemometer. At Reynolds numbers low enough to allow considerable nonlinear vortex amplification in the laminar region, transition was found to begin sooner and progress faster at a vortex upwash position than at a spanwise-adjacent downwash position. Measured Görtler numbers at transition onset bore little relationship to those often used as transition criteria in two-dimensional boundary layer prediction codes. Little spanwise variation in intermittency occurred at higher Reynolds numbers, where mean velocity profiles at upwash were much less inflected. Toward the end of curvature, favorable pressure gradients estimated to exceed the Launder relaminarization value corresponded with cases of incomplete transition.
publisherThe American Society of Mechanical Engineers (ASME)
titleTransition in Pressure-Surface Boundary Layers
typeJournal Paper
journal volume109
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262102
journal fristpage296
journal lastpage302
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 002
contenttypeFulltext


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