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    Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 370
    Author:
    J. J. Adamczyk
    ,
    M. L. Celestina
    ,
    M. Barnett
    ,
    T. A. Beach
    DOI: 10.1115/1.2927669
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work outlines a procedure for simulating the flow field within multistage turbomachinery, which includes the effects of unsteadiness, compressibility, and viscosity. The associated modeling equations are the average passage equation system, which governs the time-averaged flow field within a typical passage of a blade row embedded within a multistage configuration. The results from a simulation of a low aspect ratio stage and one-half turbine will be presented and compared with experimental measurements. It will be shown that the secondary flow field generated by the rotor causes the aerodynamic performance of the downstream vane to be significantly different from that of an isolated blade row.
    keyword(s): Simulation , Viscous flow , Turbines , Flow (Dynamics) , Blades , Equations , Turbomachinery , Modeling , Rotors , Measurement , Viscosity AND Compressibility ,
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      Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107721
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    contributor authorJ. J. Adamczyk
    contributor authorM. L. Celestina
    contributor authorM. Barnett
    contributor authorT. A. Beach
    date accessioned2017-05-08T23:34:05Z
    date available2017-05-08T23:34:05Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#370_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107721
    description abstractThis work outlines a procedure for simulating the flow field within multistage turbomachinery, which includes the effects of unsteadiness, compressibility, and viscosity. The associated modeling equations are the average passage equation system, which governs the time-averaged flow field within a typical passage of a blade row embedded within a multistage configuration. The results from a simulation of a low aspect ratio stage and one-half turbine will be presented and compared with experimental measurements. It will be shown that the secondary flow field generated by the rotor causes the aerodynamic performance of the downstream vane to be significantly different from that of an isolated blade row.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927669
    journal fristpage370
    journal lastpage376
    identifier eissn1528-8900
    keywordsSimulation
    keywordsViscous flow
    keywordsTurbines
    keywordsFlow (Dynamics)
    keywordsBlades
    keywordsEquations
    keywordsTurbomachinery
    keywordsModeling
    keywordsRotors
    keywordsMeasurement
    keywordsViscosity AND Compressibility
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;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
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