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    An Approach for Inclusion of a Nonlocal Transition Model in a Parallel Unstructured Computational Fluid Dynamics Code

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 003::page 31008
    Author:
    Dragan Kožulović
    ,
    B. Leigh Lapworth
    DOI: 10.1115/1.2987238
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The implementation of an integral transition model in a parallel unstructured computational fluid dynamics code is described. In particular, an algorithm for gathering the nonlocal boundary layer values (momentum thickness and shape factor) from parallel distributed computational domains is presented. Transition modeling results are presented for a flat plate and for a low pressure turbine, covering a large variation of Reynolds numbers, Mach numbers, turbulence intensities, and incidence angles. Contrary to fully turbulent simulations, transitional predictions are in very good agreement with measurements. Furthermore, the computational overhead of transitional simulations is only 7% for one multigrid cycle.
    keyword(s): Pressure , Boundary layers , Computational fluid dynamics , Engineering simulation , Modeling , Turbulence , Reynolds number , Flow (Dynamics) , Mach number , Turbines , Algorithms , Measurement , Separation (Technology) , Momentum , Cycles , Thickness AND Flat plates ,
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      An Approach for Inclusion of a Nonlocal Transition Model in a Parallel Unstructured Computational Fluid Dynamics Code

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142162
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    • Journal of Turbomachinery

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    contributor authorDragan Kožulović
    contributor authorB. Leigh Lapworth
    date accessioned2017-05-09T00:35:48Z
    date available2017-05-09T00:35:48Z
    date copyrightJuly, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28755#031008_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142162
    description abstractThe implementation of an integral transition model in a parallel unstructured computational fluid dynamics code is described. In particular, an algorithm for gathering the nonlocal boundary layer values (momentum thickness and shape factor) from parallel distributed computational domains is presented. Transition modeling results are presented for a flat plate and for a low pressure turbine, covering a large variation of Reynolds numbers, Mach numbers, turbulence intensities, and incidence angles. Contrary to fully turbulent simulations, transitional predictions are in very good agreement with measurements. Furthermore, the computational overhead of transitional simulations is only 7% for one multigrid cycle.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Approach for Inclusion of a Nonlocal Transition Model in a Parallel Unstructured Computational Fluid Dynamics Code
    typeJournal Paper
    journal volume131
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2987238
    journal fristpage31008
    identifier eissn1528-8900
    keywordsPressure
    keywordsBoundary layers
    keywordsComputational fluid dynamics
    keywordsEngineering simulation
    keywordsModeling
    keywordsTurbulence
    keywordsReynolds number
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsTurbines
    keywordsAlgorithms
    keywordsMeasurement
    keywordsSeparation (Technology)
    keywordsMomentum
    keywordsCycles
    keywordsThickness AND Flat plates
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;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
    yabeshDSpacePersian