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    Multigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations

    Source: Journal of Fluids Engineering:;1995:;volume( 117 ):;issue: 004::page 647
    Author:
    A. Arnone
    ,
    R. Pacciani
    ,
    A. Sestini
    DOI: 10.1115/1.2817317
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Navier-Stokes time-accurate solver has been extended to the analysis of unsteady rotor-stator interaction. In the proposed method, a fully-implicit time discretization is used to remove stability limitations. A four-stage Runge-Kutta scheme is used in conjunction with several accelerating techniques typical of steady-state solvers, instead of traditional time-expensive factorizations. Those accelerating strategies include local time stepping, residual smoothing, and multigrid. Direct interpolation of the conservative variables is used to handle the interfaces between blade rows. Two-dimensional viscous calculations of unsteady rotor-stator interaction in a modern gas turbine stage are presented to check for the capability of the procedure.
    keyword(s): Navier-Stokes equations , Rotors , Computation , Stators , Steady state , Interpolation , Blades , Gas turbines AND Stability ,
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      Multigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/115461
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    • Journal of Fluids Engineering

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    contributor authorA. Arnone
    contributor authorR. Pacciani
    contributor authorA. Sestini
    date accessioned2017-05-08T23:47:27Z
    date available2017-05-08T23:47:27Z
    date copyrightDecember, 1995
    date issued1995
    identifier issn0098-2202
    identifier otherJFEGA4-27099#647_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115461
    description abstractA Navier-Stokes time-accurate solver has been extended to the analysis of unsteady rotor-stator interaction. In the proposed method, a fully-implicit time discretization is used to remove stability limitations. A four-stage Runge-Kutta scheme is used in conjunction with several accelerating techniques typical of steady-state solvers, instead of traditional time-expensive factorizations. Those accelerating strategies include local time stepping, residual smoothing, and multigrid. Direct interpolation of the conservative variables is used to handle the interfaces between blade rows. Two-dimensional viscous calculations of unsteady rotor-stator interaction in a modern gas turbine stage are presented to check for the capability of the procedure.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMultigrid Computations of Unsteady Rotor-Stator Interaction Using the Navier-Stokes Equations
    typeJournal Paper
    journal volume117
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2817317
    journal fristpage647
    journal lastpage652
    identifier eissn1528-901X
    keywordsNavier-Stokes equations
    keywordsRotors
    keywordsComputation
    keywordsStators
    keywordsSteady state
    keywordsInterpolation
    keywordsBlades
    keywordsGas turbines AND Stability
    treeJournal of Fluids Engineering:;1995:;volume( 117 ):;issue: 004
    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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