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    The Effect of a Turbulent Wake on the Stagnation Point: Part II—Heat Transfer Results

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001::page 46
    Author:
    A. J. Hanford
    ,
    D. E. Wilson
    DOI: 10.1115/1.2928277
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A phenomenological model is proposed that relates the effect of free-stream turbulence to the increase in stagnation point heat transfer. The model requires both turbulence intensity and energy spectra as inputs to the unsteady velocity at the edge of the boundary layer. The form of the edge velocity contains both a pulsation of the incoming flow and an oscillation of the streamlines. The incompressible unsteady and time-averaged boundary layer response is determined by solving the momentum and energy equations. The model allows for arbitrary two-dimensional geometry; however, results are given only for a circular cylinder. The time-averaged Nusselt number is determined theoretically and compared to existing experimental data.
    keyword(s): Wake turbulence , Heat transfer , Turbulence , Boundary layers , Circular cylinders , Equations , Geometry , Oscillations , Momentum , Flow (Dynamics) AND Spectra (Spectroscopy) ,
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      The Effect of a Turbulent Wake on the Stagnation Point: Part II—Heat Transfer Results

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/114585
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    contributor authorA. J. Hanford
    contributor authorD. E. Wilson
    date accessioned2017-05-08T23:45:53Z
    date available2017-05-08T23:45:53Z
    date copyrightJanuary, 1994
    date issued1994
    identifier issn0889-504X
    identifier otherJOTUEI-28634#46_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114585
    description abstractA phenomenological model is proposed that relates the effect of free-stream turbulence to the increase in stagnation point heat transfer. The model requires both turbulence intensity and energy spectra as inputs to the unsteady velocity at the edge of the boundary layer. The form of the edge velocity contains both a pulsation of the incoming flow and an oscillation of the streamlines. The incompressible unsteady and time-averaged boundary layer response is determined by solving the momentum and energy equations. The model allows for arbitrary two-dimensional geometry; however, results are given only for a circular cylinder. The time-averaged Nusselt number is determined theoretically and compared to existing experimental data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of a Turbulent Wake on the Stagnation Point: Part II—Heat Transfer Results
    typeJournal Paper
    journal volume116
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2928277
    journal fristpage46
    journal lastpage56
    identifier eissn1528-8900
    keywordsWake turbulence
    keywordsHeat transfer
    keywordsTurbulence
    keywordsBoundary layers
    keywordsCircular cylinders
    keywordsEquations
    keywordsGeometry
    keywordsOscillations
    keywordsMomentum
    keywordsFlow (Dynamics) AND Spectra (Spectroscopy)
    treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 001
    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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