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    The Prediction and Measurement of Incompressible Flow in a Labyrinth Seal

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 004::page 697
    Author:
    J. A. Demko
    ,
    G. L. Morrison
    ,
    D. L. Rhode
    DOI: 10.1115/1.3240315
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Predictions and measurements were obtained for incompressible flow in a labyrinth seal for Taylor numbers of 0, 7,600, and 19,000 at an axial Reynolds number near 50,000. A hot-film anemometer with computer data acquisition was used in obtaining the measurements. The computations were made using a turbulent flow Navier-Stokes finite difference code. The QUICK differencing scheme was utilized in order to diminish false diffusion. Comparison between experiments and predictions are given for the axial and swirl velocity components and turbulent kinetic energy. Also, the substantial effect of the Taylor number on the pressure distribution is presented.
    keyword(s): Flow (Dynamics) , Measurement , Turbulence , Kinetic energy , Reynolds number , Computers , Computation , Data acquisition , Diffusion (Physics) AND Pressure ,
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      The Prediction and Measurement of Incompressible Flow in a Labyrinth Seal

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/105347
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. A. Demko
    contributor authorG. L. Morrison
    contributor authorD. L. Rhode
    date accessioned2017-05-08T23:29:52Z
    date available2017-05-08T23:29:52Z
    date copyrightOctober, 1989
    date issued1989
    identifier issn1528-8919
    identifier otherJETPEZ-26672#697_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105347
    description abstractPredictions and measurements were obtained for incompressible flow in a labyrinth seal for Taylor numbers of 0, 7,600, and 19,000 at an axial Reynolds number near 50,000. A hot-film anemometer with computer data acquisition was used in obtaining the measurements. The computations were made using a turbulent flow Navier-Stokes finite difference code. The QUICK differencing scheme was utilized in order to diminish false diffusion. Comparison between experiments and predictions are given for the axial and swirl velocity components and turbulent kinetic energy. Also, the substantial effect of the Taylor number on the pressure distribution is presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Prediction and Measurement of Incompressible Flow in a Labyrinth Seal
    typeJournal Paper
    journal volume111
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240315
    journal fristpage697
    journal lastpage702
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsMeasurement
    keywordsTurbulence
    keywordsKinetic energy
    keywordsReynolds number
    keywordsComputers
    keywordsComputation
    keywordsData acquisition
    keywordsDiffusion (Physics) AND Pressure
    treeJournal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 004
    contenttypeFulltext
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