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    Rotating Waves as a Stall inception Indication in Axial Compressors

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002::page 290
    Author:
    V. H. Garnier
    ,
    A. H. Epstein
    ,
    E. M. Greitzer
    DOI: 10.1115/1.2929105
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stall inception has been studied in two low-speed compressors (a single-stage and a three-stage) and in a high-speed three-stage compressor, using temporally and spatially resolved measurements. In all three machines, rotating stall was preceded by a period in which small-amplitude waves were observed traveling around the circumference of the machine at a speed slightly less than the fully developed rotating stall cell speed. The waves evolved smoothly into rotating stall without sharp changes in phase or amplitude, implying that, in the machines tested, the prestall waves and the fully developed rotating stall are two stages of the same phenomenon. The growth rate of these disturbances was in accord with that predicted by current analytical models. The prestall waves were observed both with uniform and with distorted inflow, but were most readily discerned with uniform inflow. Engineering uses and limitations of these waves are discussed.
    keyword(s): Compressors , Waves , Stall inception , Machinery , Inflow , Measurement AND Travel ,
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      Rotating Waves as a Stall inception Indication in Axial Compressors

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109434
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    • Journal of Turbomachinery

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    contributor authorV. H. Garnier
    contributor authorA. H. Epstein
    contributor authorE. M. Greitzer
    date accessioned2017-05-08T23:37:00Z
    date available2017-05-08T23:37:00Z
    date copyrightApril, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28609#290_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109434
    description abstractStall inception has been studied in two low-speed compressors (a single-stage and a three-stage) and in a high-speed three-stage compressor, using temporally and spatially resolved measurements. In all three machines, rotating stall was preceded by a period in which small-amplitude waves were observed traveling around the circumference of the machine at a speed slightly less than the fully developed rotating stall cell speed. The waves evolved smoothly into rotating stall without sharp changes in phase or amplitude, implying that, in the machines tested, the prestall waves and the fully developed rotating stall are two stages of the same phenomenon. The growth rate of these disturbances was in accord with that predicted by current analytical models. The prestall waves were observed both with uniform and with distorted inflow, but were most readily discerned with uniform inflow. Engineering uses and limitations of these waves are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRotating Waves as a Stall inception Indication in Axial Compressors
    typeJournal Paper
    journal volume113
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929105
    journal fristpage290
    journal lastpage301
    identifier eissn1528-8900
    keywordsCompressors
    keywordsWaves
    keywordsStall inception
    keywordsMachinery
    keywordsInflow
    keywordsMeasurement AND Travel
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 002
    contenttypeFulltext
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