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    Calculation of Surface Roughness Effects on Air-Riding Seals

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001::page 75
    Author:
    C. Guardino
    ,
    N. J. Hills
    ,
    J. W. Chew
    DOI: 10.1115/1.1619426
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of surface roughness on air-riding seals are investigated here using the Rayleigh pad as an example. Both incompressible and compressible flows are considered using both CFD analysis and analytical/numerical solutions of the Reynolds equation for various two-dimensional or three-dimensional roughness patterns on the stationary wall. A “unit-based” approach for incompressible flows has also been employed and is shown to be computationally much less expensive than the full-geometry solution. Results are presented showing the effect of surface roughness on the net lift force. The effects of varying the Reynolds number are demonstrated, as well as comparative results for static stiffness.
    keyword(s): Flow (Dynamics) , Surface roughness , Equations , Pressure , Clearances (Engineering) , Computational fluid dynamics , Reynolds number AND Stiffness ,
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      Calculation of Surface Roughness Effects on Air-Riding Seals

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    https://yetl.yabesh.ir/yetl1/handle/yetl/130068
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorC. Guardino
    contributor authorN. J. Hills
    contributor authorJ. W. Chew
    date accessioned2017-05-09T00:13:04Z
    date available2017-05-09T00:13:04Z
    date copyrightJanuary, 2004
    date issued2004
    identifier issn1528-8919
    identifier otherJETPEZ-26825#75_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130068
    description abstractThe effects of surface roughness on air-riding seals are investigated here using the Rayleigh pad as an example. Both incompressible and compressible flows are considered using both CFD analysis and analytical/numerical solutions of the Reynolds equation for various two-dimensional or three-dimensional roughness patterns on the stationary wall. A “unit-based” approach for incompressible flows has also been employed and is shown to be computationally much less expensive than the full-geometry solution. Results are presented showing the effect of surface roughness on the net lift force. The effects of varying the Reynolds number are demonstrated, as well as comparative results for static stiffness.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCalculation of Surface Roughness Effects on Air-Riding Seals
    typeJournal Paper
    journal volume126
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1619426
    journal fristpage75
    journal lastpage82
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsSurface roughness
    keywordsEquations
    keywordsPressure
    keywordsClearances (Engineering)
    keywordsComputational fluid dynamics
    keywordsReynolds number AND Stiffness
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001
    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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