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    Simulating Boundary Layer Transition With Low-Reynolds-Number k–ε Turbulence Models: Part 1—An Evaluation of Prediction Characteristics

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001::page 10
    Author:
    R. C. Schmidt
    ,
    S. V. Patankar
    DOI: 10.1115/1.2927728
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis and evaluation of the capability of k –ε low-Reynolds-number turbulence models to predict transition in external boundary-layer flows subject to free-stream turbulence is presented. The similarities between the near-wall cross-stream regions in a fully turbulent boundary layer and the progressive stages through which developing boundary layers pass in the streamwise direction are used to describe the mechanisms by which the models simulate the transition process. Two representative models (Jones and Launder, 1972; Lam and Bremhorst, 1981) are employed in a series of computational tests designed to answer some specific practical questions about the ability of these models to yield accurate, reliable answers over a range of free-stream turbulence conditions.
    keyword(s): Turbulence , Boundary layers , Boundary layer turbulence , Mechanisms AND Flow (Dynamics) ,
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      Simulating Boundary Layer Transition With Low-Reynolds-Number k–ε Turbulence Models: Part 1—An Evaluation of Prediction Characteristics

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109439
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    • Journal of Turbomachinery

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    contributor authorR. C. Schmidt
    contributor authorS. V. Patankar
    date accessioned2017-05-08T23:37:01Z
    date available2017-05-08T23:37:01Z
    date copyrightJanuary, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28608#10_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109439
    description abstractAn analysis and evaluation of the capability of k –ε low-Reynolds-number turbulence models to predict transition in external boundary-layer flows subject to free-stream turbulence is presented. The similarities between the near-wall cross-stream regions in a fully turbulent boundary layer and the progressive stages through which developing boundary layers pass in the streamwise direction are used to describe the mechanisms by which the models simulate the transition process. Two representative models (Jones and Launder, 1972; Lam and Bremhorst, 1981) are employed in a series of computational tests designed to answer some specific practical questions about the ability of these models to yield accurate, reliable answers over a range of free-stream turbulence conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulating Boundary Layer Transition With Low-Reynolds-Number k–ε Turbulence Models: Part 1—An Evaluation of Prediction Characteristics
    typeJournal Paper
    journal volume113
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927728
    journal fristpage10
    journal lastpage17
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsBoundary layers
    keywordsBoundary layer turbulence
    keywordsMechanisms AND Flow (Dynamics)
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;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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