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    Investigations of Boundary Layer Transition in an Adverse Pressure Gradient

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 004::page 366
    Author:
    J. P. Gostelow
    ,
    A. R. Blunden
    DOI: 10.1115/1.3262281
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Boundary layer transition was measured on a flat plate for four different turbulence levels. A range of adverse pressure gradients was imposed for one of these. The zero pressure gradient results were in agreement with accepted data for transition inception, length, and turbulent spot formation rate. They were also well represented by Narasimha’s universal intermittency distribution. A surprisingly strong similarity was also exhibited by intermittency distributions under adverse pressure gradients. Dimensionless velocity profiles were reasonable for the zero pressure gradient cases but difficulties with skin-friction prediction were experienced under adverse pressure gradient conditions. For this moderate turbulence level the transition inception Reynolds number remained reasonably constant with pressure gradient. Transition lengths, however, were greatly reduced by the imposition of even a weak adverse pressure gradient. This was associated with a strong increase in turbulent spot formation rate.
    keyword(s): Boundary layers , Pressure gradient , Turbulence , Reynolds number , Skin friction (Fluid dynamics) AND Flat plates ,
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      Investigations of Boundary Layer Transition in an Adverse Pressure Gradient

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/106125
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    contributor authorJ. P. Gostelow
    contributor authorA. R. Blunden
    date accessioned2017-05-08T23:31:18Z
    date available2017-05-08T23:31:18Z
    date copyrightOctober, 1989
    date issued1989
    identifier issn0889-504X
    identifier otherJOTUEI-28598#366_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106125
    description abstractBoundary layer transition was measured on a flat plate for four different turbulence levels. A range of adverse pressure gradients was imposed for one of these. The zero pressure gradient results were in agreement with accepted data for transition inception, length, and turbulent spot formation rate. They were also well represented by Narasimha’s universal intermittency distribution. A surprisingly strong similarity was also exhibited by intermittency distributions under adverse pressure gradients. Dimensionless velocity profiles were reasonable for the zero pressure gradient cases but difficulties with skin-friction prediction were experienced under adverse pressure gradient conditions. For this moderate turbulence level the transition inception Reynolds number remained reasonably constant with pressure gradient. Transition lengths, however, were greatly reduced by the imposition of even a weak adverse pressure gradient. This was associated with a strong increase in turbulent spot formation rate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigations of Boundary Layer Transition in an Adverse Pressure Gradient
    typeJournal Paper
    journal volume111
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262281
    journal fristpage366
    journal lastpage374
    identifier eissn1528-8900
    keywordsBoundary layers
    keywordsPressure gradient
    keywordsTurbulence
    keywordsReynolds number
    keywordsSkin friction (Fluid dynamics) AND Flat plates
    treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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