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    Flowfield and Performance Measurements in a Vaned Radial Diffuser

    Source: Journal of Fluids Engineering:;1986:;volume( 108 ):;issue: 002::page 141
    Author:
    J. C. Dutton
    ,
    P. Piemsomboon
    ,
    P. E. Jenkins
    DOI: 10.1115/1.3242553
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow characteristics of a vaned diffuser typical of those currently used in centrifugal compressors have been determined experimentally by using a static diffuser test rig. The vortex test vehicle (VTV) portion of this rig was used to simulate the essential features of the flow leaving the impeller of an actual compressor. The mean flow phenomena at the diffuser entrance and the static pressure recovery along the diffuser passage have been determined. In addition, the flow angle and Mach number distributions at several key locations throughout the diffuser channel have been obtained. The most notable feature of the diffuser flowfield is the high degree of nonuniformity in the inlet/leading edge region.
    keyword(s): Measurement , Diffusers , Flow (Dynamics) , Compressors , Impellers , Mach number , Channels (Hydraulic engineering) , Vehicles , Vortices AND Pressure ,
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      Flowfield and Performance Measurements in a Vaned Radial Diffuser

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101306
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    • Journal of Fluids Engineering

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    contributor authorJ. C. Dutton
    contributor authorP. Piemsomboon
    contributor authorP. E. Jenkins
    date accessioned2017-05-08T23:22:47Z
    date available2017-05-08T23:22:47Z
    date copyrightJune, 1986
    date issued1986
    identifier issn0098-2202
    identifier otherJFEGA4-27020#141_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101306
    description abstractThe flow characteristics of a vaned diffuser typical of those currently used in centrifugal compressors have been determined experimentally by using a static diffuser test rig. The vortex test vehicle (VTV) portion of this rig was used to simulate the essential features of the flow leaving the impeller of an actual compressor. The mean flow phenomena at the diffuser entrance and the static pressure recovery along the diffuser passage have been determined. In addition, the flow angle and Mach number distributions at several key locations throughout the diffuser channel have been obtained. The most notable feature of the diffuser flowfield is the high degree of nonuniformity in the inlet/leading edge region.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFlowfield and Performance Measurements in a Vaned Radial Diffuser
    typeJournal Paper
    journal volume108
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3242553
    journal fristpage141
    journal lastpage147
    identifier eissn1528-901X
    keywordsMeasurement
    keywordsDiffusers
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsImpellers
    keywordsMach number
    keywordsChannels (Hydraulic engineering)
    keywordsVehicles
    keywordsVortices AND Pressure
    treeJournal of Fluids Engineering:;1986:;volume( 108 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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