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    Simulation of Subsonic Flow Through a Generic Labyrinth Seal

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 004::page 674
    Author:
    D. L. Rhode
    ,
    S. R. Sobolik
    DOI: 10.1115/1.3239964
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new method for predicting the leakage through labyrinth seals has been developed and is shown to provide realistic results which agree with measurements. It utilizes a finite-difference computer code which was developed in order to compute the pressure drop across a single cavity of the seal. This quantity is obtained at several leakage flow Mach numbers to be used subsequently in predicting the leakage rate. The model is widely applicable and does not require an estimate of the kinetic energy carry-over coefficient, whose value is often uncertain for many untested configurations. Detailed cavity distributions of basic flowfield quantities are also presented and examined. Specifically, the predicted results of four seal leakage mass flow rates at given cavity inlet pressure and temperature are compared, and important variations are examined. Also, realistic approximations of flow variable distributions within a single cavity are made from the included figures to assist in the development of analytical methods.
    keyword(s): Pressure , Flow (Dynamics) , Mach number , Temperature , Measurement , Kinetic energy , Simulation , Analytical methods , Computers , Approximation , Cavities , Pressure drop , Subsonic flow , Leakage flows AND Leakage ,
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      Simulation of Subsonic Flow Through a Generic Labyrinth Seal

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101087
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorD. L. Rhode
    contributor authorS. R. Sobolik
    date accessioned2017-05-08T23:22:22Z
    date available2017-05-08T23:22:22Z
    date copyrightOctober, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26639#674_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101087
    description abstractA new method for predicting the leakage through labyrinth seals has been developed and is shown to provide realistic results which agree with measurements. It utilizes a finite-difference computer code which was developed in order to compute the pressure drop across a single cavity of the seal. This quantity is obtained at several leakage flow Mach numbers to be used subsequently in predicting the leakage rate. The model is widely applicable and does not require an estimate of the kinetic energy carry-over coefficient, whose value is often uncertain for many untested configurations. Detailed cavity distributions of basic flowfield quantities are also presented and examined. Specifically, the predicted results of four seal leakage mass flow rates at given cavity inlet pressure and temperature are compared, and important variations are examined. Also, realistic approximations of flow variable distributions within a single cavity are made from the included figures to assist in the development of analytical methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulation of Subsonic Flow Through a Generic Labyrinth Seal
    typeJournal Paper
    journal volume108
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239964
    journal fristpage674
    journal lastpage680
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsTemperature
    keywordsMeasurement
    keywordsKinetic energy
    keywordsSimulation
    keywordsAnalytical methods
    keywordsComputers
    keywordsApproximation
    keywordsCavities
    keywordsPressure drop
    keywordsSubsonic flow
    keywordsLeakage flows AND Leakage
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 004
    contenttypeFulltext
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