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    Numerical Comparative Study of Compressor Rotor and Stator Blade Deposition Rates

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 003::page 608
    Author:
    D. Bouris
    ,
    R. Kubo
    ,
    H. Hirata
    ,
    Y. Nakata
    DOI: 10.1115/1.1454113
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressor fouling is generally accepted to be an important factor when monitoring the efficiency of an engine’s operation. However, there are not many studies related to the local fouling behavior of the individual components of the compressor. In the present paper, the CFD-ACE software package is used for the flow field calculation and the results are utilized to calculate the deposition rates on the blade surfaces of a conventional compressor stator and rotor. The deposition model takes into account the particle and surface material properties and the energy balance at the point of impact. A discussion is presented regarding the various mechanisms that produce the final deposition rate distribution and how the flow field and blade geometry affect it.
    keyword(s): Flow (Dynamics) , Particulate matter , Compressors , Rotors , Blades , Stators , Mechanisms , Pressure AND Materials properties ,
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      Numerical Comparative Study of Compressor Rotor and Stator Blade Deposition Rates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/126750
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorD. Bouris
    contributor authorR. Kubo
    contributor authorH. Hirata
    contributor authorY. Nakata
    date accessioned2017-05-09T00:07:27Z
    date available2017-05-09T00:07:27Z
    date copyrightJuly, 2002
    date issued2002
    identifier issn1528-8919
    identifier otherJETPEZ-26814#608_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126750
    description abstractCompressor fouling is generally accepted to be an important factor when monitoring the efficiency of an engine’s operation. However, there are not many studies related to the local fouling behavior of the individual components of the compressor. In the present paper, the CFD-ACE software package is used for the flow field calculation and the results are utilized to calculate the deposition rates on the blade surfaces of a conventional compressor stator and rotor. The deposition model takes into account the particle and surface material properties and the energy balance at the point of impact. A discussion is presented regarding the various mechanisms that produce the final deposition rate distribution and how the flow field and blade geometry affect it.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Comparative Study of Compressor Rotor and Stator Blade Deposition Rates
    typeJournal Paper
    journal volume124
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1454113
    journal fristpage608
    journal lastpage616
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsParticulate matter
    keywordsCompressors
    keywordsRotors
    keywordsBlades
    keywordsStators
    keywordsMechanisms
    keywordsPressure AND Materials properties
    treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 003
    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