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    Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004::page 660
    Author:
    H. D. Joslyn
    ,
    J. J. Brasz
    ,
    R. P. Dring
    DOI: 10.1115/1.2929132
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The ability to acquire blade loadings (surface pressure distributions) and surface flow visualization on an unshrouded centrifugal compressor impeller is demonstrated. Circumferential and streamwise static pressure distributions acquired on the stationary shroud are also presented. Data were acquired in a new facility designed for centrifugal compressor aerodynamic research. Blade loadings calculated with a blade-to-blade potential flow analysis are compared with the measured results. Surface flow visualization reveals some complex aspects of the flow on the surface of the impeller blading and hub.
    keyword(s): Aerodynamics , Compressor impellers , Blades , Flow visualization , Pressure , Flow (Dynamics) , Compressors AND Impellers ,
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      Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109361
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    • Journal of Turbomachinery

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    contributor authorH. D. Joslyn
    contributor authorJ. J. Brasz
    contributor authorR. P. Dring
    date accessioned2017-05-08T23:36:54Z
    date available2017-05-08T23:36:54Z
    date copyrightOctober, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28615#660_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109361
    description abstractThe ability to acquire blade loadings (surface pressure distributions) and surface flow visualization on an unshrouded centrifugal compressor impeller is demonstrated. Circumferential and streamwise static pressure distributions acquired on the stationary shroud are also presented. Data were acquired in a new facility designed for centrifugal compressor aerodynamic research. Blade loadings calculated with a blade-to-blade potential flow analysis are compared with the measured results. Surface flow visualization reveals some complex aspects of the flow on the surface of the impeller blading and hub.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCentrifugal Compressor Impeller Aerodynamics: An Experimental Investigation
    typeJournal Paper
    journal volume113
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929132
    journal fristpage660
    journal lastpage669
    identifier eissn1528-8900
    keywordsAerodynamics
    keywordsCompressor impellers
    keywordsBlades
    keywordsFlow visualization
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsCompressors AND Impellers
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;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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