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    Turbulence Intensity and Length Scale Measurements in Multistage Compressors

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001::page 38
    Author:
    T. R. Camp
    ,
    H.-W. Shin
    DOI: 10.1115/1.2835642
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the measurement and processing of turbulence data from multistage low-speed compressors. Measurements were made at the same relative positions in three four-stage compressors, each having different levels of the design stage loading coefficient. A new method of data processing to calculate turbulence intensities and integral length scales is outlined. Using this method, integral length scales have been measured in turbomachinery flows for the first time. It is shown how the turbulence intensity and integral length scale vary with position in the blade passage, with changing flow coefficient and with the value of the design stage loading coefficient. The results have been used to specify representative inlet conditions for experimental rigs and to improve the application of CFD turbulence models to turbomachinery modeling.
    keyword(s): Measurement , Turbulence , Compressors , Design , Flow (Dynamics) , Turbomachinery , Modeling , Blades AND Computational fluid dynamics ,
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      Turbulence Intensity and Length Scale Measurements in Multistage Compressors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116170
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    contributor authorT. R. Camp
    contributor authorH.-W. Shin
    date accessioned2017-05-08T23:48:39Z
    date available2017-05-08T23:48:39Z
    date copyrightJanuary, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28642#38_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116170
    description abstractThis paper describes the measurement and processing of turbulence data from multistage low-speed compressors. Measurements were made at the same relative positions in three four-stage compressors, each having different levels of the design stage loading coefficient. A new method of data processing to calculate turbulence intensities and integral length scales is outlined. Using this method, integral length scales have been measured in turbomachinery flows for the first time. It is shown how the turbulence intensity and integral length scale vary with position in the blade passage, with changing flow coefficient and with the value of the design stage loading coefficient. The results have been used to specify representative inlet conditions for experimental rigs and to improve the application of CFD turbulence models to turbomachinery modeling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTurbulence Intensity and Length Scale Measurements in Multistage Compressors
    typeJournal Paper
    journal volume117
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2835642
    journal fristpage38
    journal lastpage46
    identifier eissn1528-8900
    keywordsMeasurement
    keywordsTurbulence
    keywordsCompressors
    keywordsDesign
    keywordsFlow (Dynamics)
    keywordsTurbomachinery
    keywordsModeling
    keywordsBlades AND Computational fluid dynamics
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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