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    Off-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004::page 602
    Author:
    A. Pinarbasi
    ,
    M. W. Johnson
    DOI: 10.1115/1.2836574
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements have been taken of the three-dimensional velocity field within the vaneless diffuser of a backswept low speed centrifugal compressor using hot-wire anemometry. A 16 percent below and an 11 percent above design flow rate were used in the present study. Results at both flow rates show how the blade wake mixes out more rapidly than the passage wake. Strong secondary flows inherited from the impeller at the higher flow rate delay the mixing out of the circumferential velocity variations, but at both flow rates these circumferential variations are negligible at the last measurement station. The measured tangential/radial flow angle is used to recommend optimum values for the vaneless space and vane angle for design of a vaned diffuser.
    keyword(s): Compressors , Design , Flow measurement , Vaneless diffusers , Flow (Dynamics) , Wakes , Diffusers , Blades , Delays , Measurement , Wire , Impellers AND Radial flow ,
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      Off-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116116
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    • Journal of Turbomachinery

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    contributor authorA. Pinarbasi
    contributor authorM. W. Johnson
    date accessioned2017-05-08T23:48:34Z
    date available2017-05-08T23:48:34Z
    date copyrightOctober, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28646#602_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116116
    description abstractDetailed measurements have been taken of the three-dimensional velocity field within the vaneless diffuser of a backswept low speed centrifugal compressor using hot-wire anemometry. A 16 percent below and an 11 percent above design flow rate were used in the present study. Results at both flow rates show how the blade wake mixes out more rapidly than the passage wake. Strong secondary flows inherited from the impeller at the higher flow rate delay the mixing out of the circumferential velocity variations, but at both flow rates these circumferential variations are negligible at the last measurement station. The measured tangential/radial flow angle is used to recommend optimum values for the vaneless space and vane angle for design of a vaned diffuser.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOff-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser
    typeJournal Paper
    journal volume117
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836574
    journal fristpage602
    journal lastpage608
    identifier eissn1528-8900
    keywordsCompressors
    keywordsDesign
    keywordsFlow measurement
    keywordsVaneless diffusers
    keywordsFlow (Dynamics)
    keywordsWakes
    keywordsDiffusers
    keywordsBlades
    keywordsDelays
    keywordsMeasurement
    keywordsWire
    keywordsImpellers AND Radial flow
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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