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    A Finite Difference Solution of the Two and Three-Dimensional Incompressible Turbulent Boundary Layer Equations

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 003::page 445
    Author:
    W. F. Klinksiek
    ,
    F. J. Pierce
    DOI: 10.1115/1.3447049
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A modified Crank-Nicholson implicit finite difference formulation is presented for two and three-dimensional turbulent boundary layers. The turbulent stresses are treated after Prandtl’s early mixing length model. “Boundary layer like” assumptions result in only the streamwise and transverse stresses remaining. The specific empirical input is the Maise and McDonald mixing length model. Excellent agreement with two independent experiments is obtained for mean velocity field data. Both experiments included a plane of symmetry to provide a transverse coordinate initial condition.
    keyword(s): Boundary layer turbulence , Equations , Stress , Boundary layers AND Turbulence ,
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      A Finite Difference Solution of the Two and Three-Dimensional Incompressible Turbulent Boundary Layer Equations

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    https://yetl.yabesh.ir/yetl1/handle/yetl/163882
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    contributor authorW. F. Klinksiek
    contributor authorF. J. Pierce
    date accessioned2017-05-09T01:36:34Z
    date available2017-05-09T01:36:34Z
    date copyrightSeptember, 1973
    date issued1973
    identifier issn0098-2202
    identifier otherJFEGA4-26849#445_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163882
    description abstractA modified Crank-Nicholson implicit finite difference formulation is presented for two and three-dimensional turbulent boundary layers. The turbulent stresses are treated after Prandtl’s early mixing length model. “Boundary layer like” assumptions result in only the streamwise and transverse stresses remaining. The specific empirical input is the Maise and McDonald mixing length model. Excellent agreement with two independent experiments is obtained for mean velocity field data. Both experiments included a plane of symmetry to provide a transverse coordinate initial condition.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Finite Difference Solution of the Two and Three-Dimensional Incompressible Turbulent Boundary Layer Equations
    typeJournal Paper
    journal volume95
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447049
    journal fristpage445
    journal lastpage458
    identifier eissn1528-901X
    keywordsBoundary layer turbulence
    keywordsEquations
    keywordsStress
    keywordsBoundary layers AND Turbulence
    treeJournal of Fluids Engineering:;1973:;volume( 095 ):;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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