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    Measurement of the Three-Dimensional Flow Field Behind an Axial Compressor Stage

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002::page 168
    Author:
    Ch. Hirsch
    ,
    P. Kool
    DOI: 10.1115/1.3446263
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Hot wire instrumentation and a periodic sampling and averaging technique have been used in order to measure the three-dimensional flow field behind a rotor of an axial compressor stage. A single slanted rotating wire allows the determination of the three components of the blade-to-blade velocity distribution together with informations on the turbulence level. A description is given of the measurement technique, and typical experimental results are presented.
    keyword(s): Compressors , Flow (Dynamics) , Blades , Wire , Sampling (Acoustical engineering) , Instrumentation , Rotors AND Turbulence ,
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      Measurement of the Three-Dimensional Flow Field Behind an Axial Compressor Stage

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    http://yetl.yabesh.ir/yetl1/handle/yetl/89817
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    contributor authorCh. Hirsch
    contributor authorP. Kool
    date accessioned2017-05-08T23:02:48Z
    date available2017-05-08T23:02:48Z
    date copyrightApril, 1977
    date issued1977
    identifier issn1528-8919
    identifier otherJETPEZ-26732#168_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/89817
    description abstractHot wire instrumentation and a periodic sampling and averaging technique have been used in order to measure the three-dimensional flow field behind a rotor of an axial compressor stage. A single slanted rotating wire allows the determination of the three components of the blade-to-blade velocity distribution together with informations on the turbulence level. A description is given of the measurement technique, and typical experimental results are presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of the Three-Dimensional Flow Field Behind an Axial Compressor Stage
    typeJournal Paper
    journal volume99
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446263
    journal fristpage168
    journal lastpage179
    identifier eissn0742-4795
    keywordsCompressors
    keywordsFlow (Dynamics)
    keywordsBlades
    keywordsWire
    keywordsSampling (Acoustical engineering)
    keywordsInstrumentation
    keywordsRotors AND Turbulence
    treeJournal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002
    contenttypeFulltext
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