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    Rotor-Stator Interaction Analysis Using the Navier–Stokes Equations and a Multigrid Method

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004::page 679
    Author:
    A. Arnone
    ,
    R. Pacciani
    DOI: 10.1115/1.2840923
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A recently developed, time-accurate multigrid viscous 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. By means of a dual time-stepping approach, 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. The accelerating strategies include local time stepping, residual smoothing, and multigrid. Two-dimensional viscous calculations of unsteady rotor–stator interaction in the first stage of a modern gas turbine are presented. The stage analysis is based on the introduction of several blade passages to approximate the stator:rotor count ratio. Particular attention is dedicated to grid dependency in space and time as well as to the influence of the number of blades included in the calculations.
    keyword(s): Navier-Stokes equations , Rotors , Stators , Blades , Steady state , Gas turbines , Stability AND Spacetime ,
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      Rotor-Stator Interaction Analysis Using the Navier–Stokes Equations and a Multigrid Method

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/117796
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    • Journal of Turbomachinery

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    contributor authorA. Arnone
    contributor authorR. Pacciani
    date accessioned2017-05-08T23:51:50Z
    date available2017-05-08T23:51:50Z
    date copyrightOctober, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28655#679_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117796
    description abstractA recently developed, time-accurate multigrid viscous 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. By means of a dual time-stepping approach, 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. The accelerating strategies include local time stepping, residual smoothing, and multigrid. Two-dimensional viscous calculations of unsteady rotor–stator interaction in the first stage of a modern gas turbine are presented. The stage analysis is based on the introduction of several blade passages to approximate the stator:rotor count ratio. Particular attention is dedicated to grid dependency in space and time as well as to the influence of the number of blades included in the calculations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRotor-Stator Interaction Analysis Using the Navier–Stokes Equations and a Multigrid Method
    typeJournal Paper
    journal volume118
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2840923
    journal fristpage679
    journal lastpage689
    identifier eissn1528-8900
    keywordsNavier-Stokes equations
    keywordsRotors
    keywordsStators
    keywordsBlades
    keywordsSteady state
    keywordsGas turbines
    keywordsStability AND Spacetime
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;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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