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    Low-Reynolds-Number Turbulent Boundary Layers

    Source: Journal of Fluids Engineering:;1981:;volume( 103 ):;issue: 004::page 624
    Author:
    B. R. White
    DOI: 10.1115/1.3241782
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents experimental wind-tunnel data that show the universal logarithmic velocity profile for zero-pressure-gradient turbulent boundary layer flows is valid for values of momentum-deficit Reynolds numbers Rθ as low as 600. However, for values of Rθ between 425 and 600, the von Kármán and additive constants vary and are shown to be functions of Rθ and shape factor H. Furthermore, the viscous sublayer in the range 425<Rθ <600 can no longer maintain its characteristically small size. It is forced to grow, due to viscous effects, into a super sublayer (6-9 percent of the boundary layer height) that greatly exceeds conventional predictions of sublayer heights.
    keyword(s): Boundary layer turbulence , Functions , Gradients , Shapes , Wind tunnels , Pressure , Momentum , Flow (Dynamics) , Reynolds number AND Boundary layers ,
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      Low-Reynolds-Number Turbulent Boundary Layers

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    https://yetl.yabesh.ir/yetl1/handle/yetl/94677
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    contributor authorB. R. White
    date accessioned2017-05-08T23:11:19Z
    date available2017-05-08T23:11:19Z
    date copyrightDecember, 1981
    date issued1981
    identifier issn0098-2202
    identifier otherJFEGA4-26977#624_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94677
    description abstractThis paper presents experimental wind-tunnel data that show the universal logarithmic velocity profile for zero-pressure-gradient turbulent boundary layer flows is valid for values of momentum-deficit Reynolds numbers Rθ as low as 600. However, for values of Rθ between 425 and 600, the von Kármán and additive constants vary and are shown to be functions of Rθ and shape factor H. Furthermore, the viscous sublayer in the range 425<Rθ <600 can no longer maintain its characteristically small size. It is forced to grow, due to viscous effects, into a super sublayer (6-9 percent of the boundary layer height) that greatly exceeds conventional predictions of sublayer heights.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLow-Reynolds-Number Turbulent Boundary Layers
    typeJournal Paper
    journal volume103
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3241782
    journal fristpage624
    journal lastpage630
    identifier eissn1528-901X
    keywordsBoundary layer turbulence
    keywordsFunctions
    keywordsGradients
    keywordsShapes
    keywordsWind tunnels
    keywordsPressure
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsReynolds number AND Boundary layers
    treeJournal of Fluids Engineering:;1981:;volume( 103 ):;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
    yabeshDSpacePersian