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    Relaxation of the Turbulent Boundary Layer After an Abrupt Change From Rough to Smooth Wall (Data Bank Contribution)

    Source: Journal of Fluids Engineering:;1993:;volume( 115 ):;issue: 003::page 379
    Author:
    R. P. Taylor
    ,
    M. H. Hosni
    ,
    H. W. Coleman
    ,
    J. K. Taylor
    DOI: 10.1115/1.2910149
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements of velocity and turbulence intensity profiles and skin friction coefficient are presented for turbulent flat-plate boundary layer flow over a test surface with a rough-to-smooth step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27 mm diameter hemispheres spaced 2 base diameters apart in a uniform staggered array, and the remaining 1.5 m length is smooth. The profiles are compared with previous data for all-rough cases under closely matched conditions in the same facility. The skin friction data are compared with previous data for both all-rough and all-smooth cases.
    keyword(s): Surface roughness , Relaxation (Physics) , Boundary layer turbulence , Skin friction (Fluid dynamics) , Turbulence , Boundary layers , Flat plates , Flow (Dynamics) AND Measurement ,
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      Relaxation of the Turbulent Boundary Layer After an Abrupt Change From Rough to Smooth Wall (Data Bank Contribution)

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112107
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    • Journal of Fluids Engineering

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    contributor authorR. P. Taylor
    contributor authorM. H. Hosni
    contributor authorH. W. Coleman
    contributor authorJ. K. Taylor
    date accessioned2017-05-08T23:41:39Z
    date available2017-05-08T23:41:39Z
    date copyrightSeptember, 1993
    date issued1993
    identifier issn0098-2202
    identifier otherJFEGA4-27077#379_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112107
    description abstractMeasurements of velocity and turbulence intensity profiles and skin friction coefficient are presented for turbulent flat-plate boundary layer flow over a test surface with a rough-to-smooth step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27 mm diameter hemispheres spaced 2 base diameters apart in a uniform staggered array, and the remaining 1.5 m length is smooth. The profiles are compared with previous data for all-rough cases under closely matched conditions in the same facility. The skin friction data are compared with previous data for both all-rough and all-smooth cases.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRelaxation of the Turbulent Boundary Layer After an Abrupt Change From Rough to Smooth Wall (Data Bank Contribution)
    typeJournal Paper
    journal volume115
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2910149
    journal fristpage379
    journal lastpage382
    identifier eissn1528-901X
    keywordsSurface roughness
    keywordsRelaxation (Physics)
    keywordsBoundary layer turbulence
    keywordsSkin friction (Fluid dynamics)
    keywordsTurbulence
    keywordsBoundary layers
    keywordsFlat plates
    keywordsFlow (Dynamics) AND Measurement
    treeJournal of Fluids Engineering:;1993:;volume( 115 ):;issue: 003
    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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