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    A Correlation-Based Transition Model Using Local Variables—Part I: Model Formulation

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003::page 413
    Author:
    S. R. Likki
    ,
    Y. B. Suzen
    ,
    P. G. Huang
    ,
    S. Völker
    ,
    F. R. Menter
    ,
    R. B. Langtry
    DOI: 10.1115/1.2184352
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new correlation-based transition model has been developed, which is based strictly on local variables. As a result, the transition model is compatible with modern computational fluid dynamics (CFD) approaches, such as unstructured grids and massive parallel execution. The model is based on two transport equations, one for intermittency and one for the transition onset criteria in terms of momentum thickness Reynolds number. The proposed transport equations do not attempt to model the physics of the transition process (unlike, e.g., turbulence models) but form a framework for the implementation of correlation-based models into general-purpose CFD methods. Part I (this part) of this paper gives a detailed description of the mathematical formulation of the model and some of the basic test cases used for model validation, including a two-dimensional turbine blade. Part II (, , , , , and , 2006, ASME J. Turbomach., 128(3), pp. 423–434) of the paper details a significant number of test cases that have been used to validate the transition model for turbomachinery and aerodynamic applications. The authors believe that the current formulation is a significant step forward in engineering transition modeling, as it allows the combination of correlation-based transition models with general purpose CFD codes.
    keyword(s): Momentum , Turbulence , Reynolds number , Boundary layers , Equations , Thickness , Flow (Dynamics) , Computational fluid dynamics AND Turbine blades ,
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      A Correlation-Based Transition Model Using Local Variables—Part I: Model Formulation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/134816
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    contributor authorS. R. Likki
    contributor authorY. B. Suzen
    contributor authorP. G. Huang
    contributor authorS. Völker
    contributor authorF. R. Menter
    contributor authorR. B. Langtry
    date accessioned2017-05-09T00:21:55Z
    date available2017-05-09T00:21:55Z
    date copyrightJuly, 2006
    date issued2006
    identifier issn0889-504X
    identifier otherJOTUEI-28730#413_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134816
    description abstractA new correlation-based transition model has been developed, which is based strictly on local variables. As a result, the transition model is compatible with modern computational fluid dynamics (CFD) approaches, such as unstructured grids and massive parallel execution. The model is based on two transport equations, one for intermittency and one for the transition onset criteria in terms of momentum thickness Reynolds number. The proposed transport equations do not attempt to model the physics of the transition process (unlike, e.g., turbulence models) but form a framework for the implementation of correlation-based models into general-purpose CFD methods. Part I (this part) of this paper gives a detailed description of the mathematical formulation of the model and some of the basic test cases used for model validation, including a two-dimensional turbine blade. Part II (, , , , , and , 2006, ASME J. Turbomach., 128(3), pp. 423–434) of the paper details a significant number of test cases that have been used to validate the transition model for turbomachinery and aerodynamic applications. The authors believe that the current formulation is a significant step forward in engineering transition modeling, as it allows the combination of correlation-based transition models with general purpose CFD codes.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Correlation-Based Transition Model Using Local Variables—Part I: Model Formulation
    typeJournal Paper
    journal volume128
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2184352
    journal fristpage413
    journal lastpage422
    identifier eissn1528-8900
    keywordsMomentum
    keywordsTurbulence
    keywordsReynolds number
    keywordsBoundary layers
    keywordsEquations
    keywordsThickness
    keywordsFlow (Dynamics)
    keywordsComputational fluid dynamics AND Turbine blades
    treeJournal of Turbomachinery:;2006:;volume( 128 ):;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