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    An Unsteady Velocity Formulation for the Edge of the Near-Wall Region

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002::page 351
    Author:
    D. E. Wilson
    ,
    A. J. Hanford
    DOI: 10.1115/1.2841413
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A phenomenological model is presented that relates free-stream turbulence to the augmentation of stagnation-point surface flux quantities. The model requires the turbulence intensity, the longitudinal scale of the turbulence, and the energy spectra as inputs for the unsteady velocity at the edge of the near-wall viscous region. The form of the edge velocity contains both pulsations of the incoming flow and oscillations of the streamline. Incompressible results using a single fluctuating component are presented within the stagnation region of a two-dimensional cylinder. The time-averaged Froessling number is determined from the computations. These predictions are compared to existing incompressible experimental data. Additionally, the variations in the surface flux quantities with the longitudinal scale of the incoming free-stream turbulence, the Reynolds number, and the free-stream turbulence intensity are considered.
    keyword(s): Oscillations , Flow (Dynamics) , Spectra (Spectroscopy) , Turbulence , Reynolds number , Computation AND Cylinders ,
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      An Unsteady Velocity Formulation for the Edge of the Near-Wall Region

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    https://yetl.yabesh.ir/yetl1/handle/yetl/121338
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    contributor authorD. E. Wilson
    contributor authorA. J. Hanford
    date accessioned2017-05-08T23:58:13Z
    date available2017-05-08T23:58:13Z
    date copyrightApril, 1998
    date issued1998
    identifier issn0889-504X
    identifier otherJOTUEI-28665#351_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121338
    description abstractA phenomenological model is presented that relates free-stream turbulence to the augmentation of stagnation-point surface flux quantities. The model requires the turbulence intensity, the longitudinal scale of the turbulence, and the energy spectra as inputs for the unsteady velocity at the edge of the near-wall viscous region. The form of the edge velocity contains both pulsations of the incoming flow and oscillations of the streamline. Incompressible results using a single fluctuating component are presented within the stagnation region of a two-dimensional cylinder. The time-averaged Froessling number is determined from the computations. These predictions are compared to existing incompressible experimental data. Additionally, the variations in the surface flux quantities with the longitudinal scale of the incoming free-stream turbulence, the Reynolds number, and the free-stream turbulence intensity are considered.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Unsteady Velocity Formulation for the Edge of the Near-Wall Region
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841413
    journal fristpage351
    journal lastpage361
    identifier eissn1528-8900
    keywordsOscillations
    keywordsFlow (Dynamics)
    keywordsSpectra (Spectroscopy)
    keywordsTurbulence
    keywordsReynolds number
    keywordsComputation AND Cylinders
    treeJournal of Turbomachinery:;1998:;volume( 120 ):;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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