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    Performance of Axial Compressor With Nonuniform Exit Static Pressure

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001::page 76
    Author:
    H. Kodama
    DOI: 10.1115/1.3262027
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical model has been developed to predict the performance of axial compressors with an exit static pressure perturbation. The model uses a two-dimensional compressible semi-actuator disk model. This method can be applied to the compressor with known circumferential variation in exit static pressure which is measured or predicted by an analytical method. The analytical results are found to be in good agreement with experiments carried out on two transonic fans.
    keyword(s): Pressure , Compressors , Actuators , Fans AND Disks ,
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      Performance of Axial Compressor With Nonuniform Exit Static Pressure

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    http://yetl.yabesh.ir/yetl1/handle/yetl/101856
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    contributor authorH. Kodama
    date accessioned2017-05-08T23:23:43Z
    date available2017-05-08T23:23:43Z
    date copyrightJuly, 1986
    date issued1986
    identifier issn0889-504X
    identifier otherJOTUEI-28577#76_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101856
    description abstractAn analytical model has been developed to predict the performance of axial compressors with an exit static pressure perturbation. The model uses a two-dimensional compressible semi-actuator disk model. This method can be applied to the compressor with known circumferential variation in exit static pressure which is measured or predicted by an analytical method. The analytical results are found to be in good agreement with experiments carried out on two transonic fans.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance of Axial Compressor With Nonuniform Exit Static Pressure
    typeJournal Paper
    journal volume108
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262027
    journal fristpage76
    journal lastpage81
    identifier eissn1528-8900
    keywordsPressure
    keywordsCompressors
    keywordsActuators
    keywordsFans AND Disks
    treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 001
    contenttypeFulltext
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