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    Evaluation of Aerodynamic Instability Mechanisms for Centrifugal Compressors—Part I: Current Theory

    Source: Journal of Vibration and Acoustics:;1988:;volume( 110 ):;issue: 002::page 201
    Author:
    R. G. Kirk
    DOI: 10.1115/1.3269499
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Current theories of calculating levels of aerodynamic excitation are reviewed and methods of applying these results to actual compressor designs are discussed in detail. Comparison of compressor stability for approximate modal aerodynamic excitation influence to published equations for static labyrinth seal cross-coupled stiffness is made to illustrate the influence of system damping on compressor stability. The results of analysis for six operating machines are presented to give further justification for the selection of the aerodynamic excitation model.
    keyword(s): Compressors , Mechanisms , Stability , Machinery , Damping , Equations AND Stiffness ,
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      Evaluation of Aerodynamic Instability Mechanisms for Centrifugal Compressors—Part I: Current Theory

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    http://yetl.yabesh.ir/yetl1/handle/yetl/104784
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    contributor authorR. G. Kirk
    date accessioned2017-05-08T23:28:52Z
    date available2017-05-08T23:28:52Z
    date copyrightApril, 1988
    date issued1988
    identifier issn1048-9002
    identifier otherJVACEK-28977#201_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104784
    description abstractCurrent theories of calculating levels of aerodynamic excitation are reviewed and methods of applying these results to actual compressor designs are discussed in detail. Comparison of compressor stability for approximate modal aerodynamic excitation influence to published equations for static labyrinth seal cross-coupled stiffness is made to illustrate the influence of system damping on compressor stability. The results of analysis for six operating machines are presented to give further justification for the selection of the aerodynamic excitation model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEvaluation of Aerodynamic Instability Mechanisms for Centrifugal Compressors—Part I: Current Theory
    typeJournal Paper
    journal volume110
    journal issue2
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.3269499
    journal fristpage201
    journal lastpage206
    identifier eissn1528-8927
    keywordsCompressors
    keywordsMechanisms
    keywordsStability
    keywordsMachinery
    keywordsDamping
    keywordsEquations AND Stiffness
    treeJournal of Vibration and Acoustics:;1988:;volume( 110 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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