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    Heat Transfer Committee and Turbomachinery Committee Best Paper of 1996 Award: The Path to Predicting Bypass Transition

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003::page 405
    Author:
    R. E. Mayle
    ,
    A. Schulz
    DOI: 10.1115/1.2841138
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory is presented for calculating the fluctuations in a laminar boundary layer when the free stream is turbulent. The kinetic energy equation for these fluctuations is derived and a new mechanism is revealed for their production. A methodology is presented for solving the equation using standard boundary layer computer codes. Solutions of the equation show that the fluctuations grow at first almost linearly with distance and then more slowly as viscous dissipation becomes important. Comparisons of calculated growth rates and kinetic energy profiles with data show good agreement. In addition, a hypothesis is advanced for the effective forcing frequency and free-stream turbulence level that produce these fluctuations. Finally, a method to calculate the onset of transition is examined and the results compared to data.
    keyword(s): Heat transfer , Turbulence , Kinetic energy , Energy dissipation , Fluctuations (Physics) , Boundary layers , Computers , Equations , Turbomachinery AND Mechanisms ,
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      Heat Transfer Committee and Turbomachinery Committee Best Paper of 1996 Award: The Path to Predicting Bypass Transition

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119587
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    • Journal of Turbomachinery

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    contributor authorR. E. Mayle
    contributor authorA. Schulz
    date accessioned2017-05-08T23:55:04Z
    date available2017-05-08T23:55:04Z
    date copyrightJuly, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28661#405_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119587
    description abstractA theory is presented for calculating the fluctuations in a laminar boundary layer when the free stream is turbulent. The kinetic energy equation for these fluctuations is derived and a new mechanism is revealed for their production. A methodology is presented for solving the equation using standard boundary layer computer codes. Solutions of the equation show that the fluctuations grow at first almost linearly with distance and then more slowly as viscous dissipation becomes important. Comparisons of calculated growth rates and kinetic energy profiles with data show good agreement. In addition, a hypothesis is advanced for the effective forcing frequency and free-stream turbulence level that produce these fluctuations. Finally, a method to calculate the onset of transition is examined and the results compared to data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Committee and Turbomachinery Committee Best Paper of 1996 Award: The Path to Predicting Bypass Transition
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841138
    journal fristpage405
    journal lastpage411
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsTurbulence
    keywordsKinetic energy
    keywordsEnergy dissipation
    keywordsFluctuations (Physics)
    keywordsBoundary layers
    keywordsComputers
    keywordsEquations
    keywordsTurbomachinery AND Mechanisms
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;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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