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    Heat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004::page 788
    Author:
    R. P. Taylor
    ,
    H. H. Hosni
    ,
    H. W. Coleman
    ,
    J. K. Taylor
    DOI: 10.1115/1.2928032
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements of Stanton numbers, velocity profiles, temperature profiles, and turbulence intensity profiles are reported for turbulent flat plate boundary layer flows with a step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27-mm-dia hemispheres spaced 2 base diameters apart in a staggered array. The remaining 1.5 m length is smooth. The experiments show that the step change from a rough to a smooth surface has a dramatic effect on the convective heat transfer. In many cases, the Stanton number drops below the smooth-wall correlation immediately downstream of the change in roughness. The Stanton number measurements are compared with predictions using the discrete element method with excellent results.
    keyword(s): Surface roughness , Boundary layer turbulence , Heat transfer , Measurement , Turbulence , Flow (Dynamics) , Discrete element methods , Flat plates , Temperature profiles , Drops , Boundary layers AND Convection ,
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      Heat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111042
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    • Journal of Turbomachinery

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    contributor authorR. P. Taylor
    contributor authorH. H. Hosni
    contributor authorH. W. Coleman
    contributor authorJ. K. Taylor
    date accessioned2017-05-08T23:39:49Z
    date available2017-05-08T23:39:49Z
    date copyrightOctober, 1992
    date issued1992
    identifier issn0889-504X
    identifier otherJOTUEI-28625#788_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111042
    description abstractMeasurements of Stanton numbers, velocity profiles, temperature profiles, and turbulence intensity profiles are reported for turbulent flat plate boundary layer flows with a step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27-mm-dia hemispheres spaced 2 base diameters apart in a staggered array. The remaining 1.5 m length is smooth. The experiments show that the step change from a rough to a smooth surface has a dramatic effect on the convective heat transfer. In many cases, the Stanton number drops below the smooth-wall correlation immediately downstream of the change in roughness. The Stanton number measurements are compared with predictions using the discrete element method with excellent results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness
    typeJournal Paper
    journal volume114
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2928032
    journal fristpage788
    journal lastpage794
    identifier eissn1528-8900
    keywordsSurface roughness
    keywordsBoundary layer turbulence
    keywordsHeat transfer
    keywordsMeasurement
    keywordsTurbulence
    keywordsFlow (Dynamics)
    keywordsDiscrete element methods
    keywordsFlat plates
    keywordsTemperature profiles
    keywordsDrops
    keywordsBoundary layers AND Convection
    treeJournal of Turbomachinery:;1992:;volume( 114 ):;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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