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    Boundary Layer Calculation for Analysis and Design

    Source: Journal of Fluids Engineering:;1978:;volume( 100 ):;issue: 002::page 232
    Author:
    H. E. Weber
    DOI: 10.1115/1.3448637
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A simple, semiempirical method for calculating the laminar, transition, and turbulent boundary layer with arbitrary free stream pressure gradient is developed. Good correlation is obtained with data on general two dimensional turbulent flows, diffuser flows, and the cylinder in cross-flow. However only for the diffuser has the boundary layer flow been coupled with the potential core so that only the inlet conditions and geometry are required. In other cases the free stream velocity distribution must be known or calculable. Skin friction coefficient, momentum thickness Reynolds number, and free stream pressure gradient parameter correlation employs a simple lag theory. With the integral momentum equation the complete boundary layer parameters are obtained as functions of the distance along a surface.
    keyword(s): Boundary layers , Design , Momentum , Flow (Dynamics) , Pressure gradient , Diffusers , Thickness , Cross-flow , Turbulence , Reynolds number , Skin friction (Fluid dynamics) , Boundary layer turbulence , Cylinders , Equations , Functions AND Geometry ,
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      Boundary Layer Calculation for Analysis and Design

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    https://yetl.yabesh.ir/yetl1/handle/yetl/91197
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    contributor authorH. E. Weber
    date accessioned2017-05-08T23:05:06Z
    date available2017-05-08T23:05:06Z
    date copyrightJune, 1978
    date issued1978
    identifier issn0098-2202
    identifier otherJFEGA4-26933#232_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91197
    description abstractA simple, semiempirical method for calculating the laminar, transition, and turbulent boundary layer with arbitrary free stream pressure gradient is developed. Good correlation is obtained with data on general two dimensional turbulent flows, diffuser flows, and the cylinder in cross-flow. However only for the diffuser has the boundary layer flow been coupled with the potential core so that only the inlet conditions and geometry are required. In other cases the free stream velocity distribution must be known or calculable. Skin friction coefficient, momentum thickness Reynolds number, and free stream pressure gradient parameter correlation employs a simple lag theory. With the integral momentum equation the complete boundary layer parameters are obtained as functions of the distance along a surface.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBoundary Layer Calculation for Analysis and Design
    typeJournal Paper
    journal volume100
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448637
    journal fristpage232
    journal lastpage236
    identifier eissn1528-901X
    keywordsBoundary layers
    keywordsDesign
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsPressure gradient
    keywordsDiffusers
    keywordsThickness
    keywordsCross-flow
    keywordsTurbulence
    keywordsReynolds number
    keywordsSkin friction (Fluid dynamics)
    keywordsBoundary layer turbulence
    keywordsCylinders
    keywordsEquations
    keywordsFunctions AND Geometry
    treeJournal of Fluids Engineering:;1978:;volume( 100 ):;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
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