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    Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004::page 561
    Author:
    G. V. Hobson
    ,
    B. Lakshminarayana
    DOI: 10.1115/1.2929115
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fully elliptic, control volume solution of the two-dimensional incompressible Navier–Stokes equations for the prediction of cascade performance over a wide range is presented in this paper. The numerical technique is based on a new pressure substitution method. A Poisson equation is derived from the pressure-weighted substitution of the full momentum equations into the continuity equation. The analysis of a double circular arc compressor cascade is presented, and the results are compared with the available experimental data at various incidence angles. Good agreement is obtained for the blade pressure distribution, boundary layer and wake profiles, skin friction coefficient, losses and outlet angles. Turbulence effects are simulated by the low-Reynolds-number version of the k–ε turbulence model.
    keyword(s): Cascades (Fluid dynamics) , Pressure , Turbulence , Equations , Poisson equation , Compressors , Momentum , Skin friction (Fluid dynamics) , Wakes , Navier-Stokes equations , Boundary layers AND Blades ,
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      Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/109349
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    contributor authorG. V. Hobson
    contributor authorB. Lakshminarayana
    date accessioned2017-05-08T23:36:53Z
    date available2017-05-08T23:36:53Z
    date copyrightOctober, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28615#561_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109349
    description abstractA fully elliptic, control volume solution of the two-dimensional incompressible Navier–Stokes equations for the prediction of cascade performance over a wide range is presented in this paper. The numerical technique is based on a new pressure substitution method. A Poisson equation is derived from the pressure-weighted substitution of the full momentum equations into the continuity equation. The analysis of a double circular arc compressor cascade is presented, and the results are compared with the available experimental data at various incidence angles. Good agreement is obtained for the blade pressure distribution, boundary layer and wake profiles, skin friction coefficient, losses and outlet angles. Turbulence effects are simulated by the low-Reynolds-number version of the k–ε turbulence model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePrediction of Cascade Performance Using an Incompressible Navier–Stokes Technique
    typeJournal Paper
    journal volume113
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929115
    journal fristpage561
    journal lastpage571
    identifier eissn1528-8900
    keywordsCascades (Fluid dynamics)
    keywordsPressure
    keywordsTurbulence
    keywordsEquations
    keywordsPoisson equation
    keywordsCompressors
    keywordsMomentum
    keywordsSkin friction (Fluid dynamics)
    keywordsWakes
    keywordsNavier-Stokes equations
    keywordsBoundary layers AND Blades
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;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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