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    Modeling Tip Clearance Effects in Multistage Axial Compressors

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004::page 697
    Author:
    S. Baghdadi
    DOI: 10.1115/1.2840925
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A variety of techniques for simulating the effects of rotor tip clearances in multistage axial compressors is discussed. Proper recognition of stage coupling and rematching effects is shown to be key to successful modeling of the overall behavior of actual engine compression systems. The application of a relatively simple one-dimensional unsteady row-by-row systems analysis is presented and shown to compare well to test data from several engine compressors.
    keyword(s): Compressors , Clearances (Engineering) , Modeling , Engines , Systems analysis , Rotors AND Compression ,
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      Modeling Tip Clearance Effects in Multistage Axial Compressors

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    https://yetl.yabesh.ir/yetl1/handle/yetl/117798
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    contributor authorS. Baghdadi
    date accessioned2017-05-08T23:51:50Z
    date available2017-05-08T23:51:50Z
    date copyrightOctober, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28655#697_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117798
    description abstractA variety of techniques for simulating the effects of rotor tip clearances in multistage axial compressors is discussed. Proper recognition of stage coupling and rematching effects is shown to be key to successful modeling of the overall behavior of actual engine compression systems. The application of a relatively simple one-dimensional unsteady row-by-row systems analysis is presented and shown to compare well to test data from several engine compressors.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleModeling Tip Clearance Effects in Multistage Axial Compressors
    typeJournal Paper
    journal volume118
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2840925
    journal fristpage697
    journal lastpage705
    identifier eissn1528-8900
    keywordsCompressors
    keywordsClearances (Engineering)
    keywordsModeling
    keywordsEngines
    keywordsSystems analysis
    keywordsRotors AND Compression
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 004
    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
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