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    A Navier–Stokes Solver for Turbomachinery Applications

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002::page 305
    Author:
    A. Arnone
    ,
    R. C. Swanson
    DOI: 10.1115/1.2929236
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computer code for solving the Reynolds-averaged full Navier–Stokes equations has been developed and applied using H- and C-type grids. The Baldwin–Lomax eddy-viscosity model is used for turbulence closure. The integration in time is based on an explicit four-stage Runge–Kutta scheme. Local time stepping, variable coefficient implicit residual smoothing, and a full multigrid method have been implemented to accelerate steady-state calculations. A grid independence analysis is presented for a transonic rotor blade. Comparisons with experimental data show that the code is an accurate viscous solver and can give very good blade-to-blade predictions for engineering applications.
    keyword(s): Turbulence , Eddies (Fluid dynamics) , Viscosity , Navier-Stokes equations , Engineering systems and industry applications , Rotors , Computers , Blades , Steady state AND Turbomachinery ,
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      A Navier–Stokes Solver for Turbomachinery Applications

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112827
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    contributor authorA. Arnone
    contributor authorR. C. Swanson
    date accessioned2017-05-08T23:42:53Z
    date available2017-05-08T23:42:53Z
    date copyrightApril, 1993
    date issued1993
    identifier issn0889-504X
    identifier otherJOTUEI-28629#305_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112827
    description abstractA computer code for solving the Reynolds-averaged full Navier–Stokes equations has been developed and applied using H- and C-type grids. The Baldwin–Lomax eddy-viscosity model is used for turbulence closure. The integration in time is based on an explicit four-stage Runge–Kutta scheme. Local time stepping, variable coefficient implicit residual smoothing, and a full multigrid method have been implemented to accelerate steady-state calculations. A grid independence analysis is presented for a transonic rotor blade. Comparisons with experimental data show that the code is an accurate viscous solver and can give very good blade-to-blade predictions for engineering applications.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Navier–Stokes Solver for Turbomachinery Applications
    typeJournal Paper
    journal volume115
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929236
    journal fristpage305
    journal lastpage313
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsEddies (Fluid dynamics)
    keywordsViscosity
    keywordsNavier-Stokes equations
    keywordsEngineering systems and industry applications
    keywordsRotors
    keywordsComputers
    keywordsBlades
    keywordsSteady state AND Turbomachinery
    treeJournal of Turbomachinery:;1993:;volume( 115 ):;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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