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    Modeling Transition in Separated and Attached Boundary Layers

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002::page 402
    Author:
    Stephen K. Roberts
    ,
    Metin I. Yaras
    DOI: 10.1115/1.1860570
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a mathematical model for predicting the rate of turbulent spot production. In this model, attached- and separated-flow transition are treated in a unified manner, and the boundary layer shape factor is identified as the parameter with which the spot production rate correlates. The model is supplemented by several correlations to allow for its practical use in the prediction of the length of the transition zone. Second, the paper presents a model for the prediction of the location of transition inception in separation bubbles. The model improves on the accuracy of existing alternatives, and is the first to account for the effects of surface roughness.
    keyword(s): Flow (Dynamics) , Separation (Technology) , Turbulence , Surface roughness , Boundary layers , Modeling , Bubbles AND Pressure gradient ,
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      Modeling Transition in Separated and Attached Boundary Layers

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    https://yetl.yabesh.ir/yetl1/handle/yetl/132811
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    contributor authorStephen K. Roberts
    contributor authorMetin I. Yaras
    date accessioned2017-05-09T00:18:11Z
    date available2017-05-09T00:18:11Z
    date copyrightApril, 2005
    date issued2005
    identifier issn0889-504X
    identifier otherJOTUEI-28719#402_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132811
    description abstractThis paper presents a mathematical model for predicting the rate of turbulent spot production. In this model, attached- and separated-flow transition are treated in a unified manner, and the boundary layer shape factor is identified as the parameter with which the spot production rate correlates. The model is supplemented by several correlations to allow for its practical use in the prediction of the length of the transition zone. Second, the paper presents a model for the prediction of the location of transition inception in separation bubbles. The model improves on the accuracy of existing alternatives, and is the first to account for the effects of surface roughness.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleModeling Transition in Separated and Attached Boundary Layers
    typeJournal Paper
    journal volume127
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1860570
    journal fristpage402
    journal lastpage411
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsTurbulence
    keywordsSurface roughness
    keywordsBoundary layers
    keywordsModeling
    keywordsBubbles AND Pressure gradient
    treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 002
    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
    yabeshDSpacePersian