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    Analysis of Variable Fluid Properties, Turbulent Annular Seals

    Source: Journal of Tribology:;1991:;volume( 113 ):;issue: 004::page 694
    Author:
    Luis A. San Andres
    DOI: 10.1115/1.2920681
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computational analysis for calculation of the dynamic force response in turbulent flow annular pressure seals of arbitrary nonuniform clearance is presented. Cryogenic liquids are considered as barotropic. The fluid motion is described by a bulk flow model and Moody’s friction factor is introduced to accomodate surface roughness effects. The numerical solution scheme is computationally efficient and accurate for seal operation at arbitrary eccentricity ratios. Numerical predictions show good agreement with available experimental results. The effects of eccentricity and liquid properties on the performance of the Space Shuttle Main Engine High Pressure Fuel Turbopump interstage seal at full power level are discussed as a reference case.
    keyword(s): Turbulence , Fluids , Motion , Fuels , Engines , Surface roughness , High pressure (Physics) , Clearances (Engineering) , Force , Pressure , Flow (Dynamics) AND Friction ,
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      Analysis of Variable Fluid Properties, Turbulent Annular Seals

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109161
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    contributor authorLuis A. San Andres
    date accessioned2017-05-08T23:36:33Z
    date available2017-05-08T23:36:33Z
    date copyrightOctober, 1991
    date issued1991
    identifier issn0742-4787
    identifier otherJOTRE9-28492#694_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109161
    description abstractA computational analysis for calculation of the dynamic force response in turbulent flow annular pressure seals of arbitrary nonuniform clearance is presented. Cryogenic liquids are considered as barotropic. The fluid motion is described by a bulk flow model and Moody’s friction factor is introduced to accomodate surface roughness effects. The numerical solution scheme is computationally efficient and accurate for seal operation at arbitrary eccentricity ratios. Numerical predictions show good agreement with available experimental results. The effects of eccentricity and liquid properties on the performance of the Space Shuttle Main Engine High Pressure Fuel Turbopump interstage seal at full power level are discussed as a reference case.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Variable Fluid Properties, Turbulent Annular Seals
    typeJournal Paper
    journal volume113
    journal issue4
    journal titleJournal of Tribology
    identifier doi10.1115/1.2920681
    journal fristpage694
    journal lastpage702
    identifier eissn1528-8897
    keywordsTurbulence
    keywordsFluids
    keywordsMotion
    keywordsFuels
    keywordsEngines
    keywordsSurface roughness
    keywordsHigh pressure (Physics)
    keywordsClearances (Engineering)
    keywordsForce
    keywordsPressure
    keywordsFlow (Dynamics) AND Friction
    treeJournal of Tribology:;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
    yabeshDSpacePersian