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    Transition in Pressure-Surface Boundary Layers

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002::page 296
    Author:
    R. I. Crane
    ,
    G. Leoutsakos
    ,
    J. Sabzvari
    DOI: 10.1115/1.3262102
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Laminar-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.
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      Transition in Pressure-Surface Boundary Layers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103252
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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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