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    Stability of Flow Through Multistage Axial Compressors

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001::page 126
    Author:
    J. P. Longley
    ,
    T. P. Hynes
    DOI: 10.1115/1.2927409
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes measurements of the performance of a research stage operating in isolation and as part of a multistage compressor. It is shown that the stall point and the stalled performance of the stage are properties of the system in which it operates rather than a property of the stage itself. The consequences of this for the estimation of the stall point for compressors and compression systems are discussed. The support that the measurements give to assumptions made by mathematical models which use the concept of an “underlying axisymmetric” characteristic, are highlighted.
    keyword(s): Stability , Flow (Dynamics) , Compressors , Measurement AND Compression ,
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      Stability of Flow Through Multistage Axial Compressors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/107795
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    contributor authorJ. P. Longley
    contributor authorT. P. Hynes
    date accessioned2017-05-08T23:34:11Z
    date available2017-05-08T23:34:11Z
    date copyrightJanuary, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28600#126_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107795
    description abstractThis paper describes measurements of the performance of a research stage operating in isolation and as part of a multistage compressor. It is shown that the stall point and the stalled performance of the stage are properties of the system in which it operates rather than a property of the stage itself. The consequences of this for the estimation of the stall point for compressors and compression systems are discussed. The support that the measurements give to assumptions made by mathematical models which use the concept of an “underlying axisymmetric” characteristic, are highlighted.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStability of Flow Through Multistage Axial Compressors
    typeJournal Paper
    journal volume112
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927409
    journal fristpage126
    journal lastpage132
    identifier eissn1528-8900
    keywordsStability
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsMeasurement AND Compression
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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