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    An Experimental Study of Rotating Stall in a Multistage Axial-Flow Compressor

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003::page 542
    Author:
    D. K. Das
    ,
    H. K. Jiang
    DOI: 10.1115/1.3239605
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field and the distribution of the flow parameters in the rotating stall regime in a three stage axial flow compressor were obtained in detail using three-hole cylindrical probes containing fast response transducers in association with a digital data acquisition system and an ensemble averaging technique. An appreciable amount of experimental data are presented in this paper with a critical discussion on those.
    keyword(s): Compressors , Axial flow , Flow (Dynamics) , Probes , Data acquisition systems AND Transducers ,
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      An Experimental Study of Rotating Stall in a Multistage Axial-Flow Compressor

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    https://yetl.yabesh.ir/yetl1/handle/yetl/98394
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    contributor authorD. K. Das
    contributor authorH. K. Jiang
    date accessioned2017-05-08T23:17:44Z
    date available2017-05-08T23:17:44Z
    date copyrightJuly, 1984
    date issued1984
    identifier issn1528-8919
    identifier otherJETPEZ-26607#542_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98394
    description abstractThe flow field and the distribution of the flow parameters in the rotating stall regime in a three stage axial flow compressor were obtained in detail using three-hole cylindrical probes containing fast response transducers in association with a digital data acquisition system and an ensemble averaging technique. An appreciable amount of experimental data are presented in this paper with a critical discussion on those.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experimental Study of Rotating Stall in a Multistage Axial-Flow Compressor
    typeJournal Paper
    journal volume106
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239605
    journal fristpage542
    journal lastpage551
    identifier eissn0742-4795
    keywordsCompressors
    keywordsAxial flow
    keywordsFlow (Dynamics)
    keywordsProbes
    keywordsData acquisition systems AND Transducers
    treeJournal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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