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    Reynolds Number Effects in Axial Compressors

    Source: Journal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 002::page 149
    Author:
    A. B. Wassell
    DOI: 10.1115/1.3609154
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of variations in flow Reynolds number on the performance of axial compressors has been studied (changes in Reynolds number being, for the most part, achieved by changes in the inlet total pressure at or near the design speed). The measured results, so achieved, have been correlated to show how the main compressor performance parameters vary with Reynolds number. Reference has been made to cascade data to assist in choosing the form of the correlation, which is essentially empirical. A good correlation of the measured performance changes on component tests has been obtained. The method described, therefore, appears to be satisfactory for predicting trends for project assessments and avoids considering the detailed flow changes that occur within the machine as the Reynolds number is varied.
    keyword(s): Compressors , Reynolds number , Flow (Dynamics) , Machinery , Pressure , Cascades (Fluid dynamics) AND Design ,
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      Reynolds Number Effects in Axial Compressors

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/126034
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. B. Wassell
    date accessioned2017-05-09T00:06:16Z
    date available2017-05-09T00:06:16Z
    date copyrightApril, 1968
    date issued1968
    identifier issn1528-8919
    identifier otherJETPEZ-26668#149_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126034
    description abstractThe influence of variations in flow Reynolds number on the performance of axial compressors has been studied (changes in Reynolds number being, for the most part, achieved by changes in the inlet total pressure at or near the design speed). The measured results, so achieved, have been correlated to show how the main compressor performance parameters vary with Reynolds number. Reference has been made to cascade data to assist in choosing the form of the correlation, which is essentially empirical. A good correlation of the measured performance changes on component tests has been obtained. The method described, therefore, appears to be satisfactory for predicting trends for project assessments and avoids considering the detailed flow changes that occur within the machine as the Reynolds number is varied.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleReynolds Number Effects in Axial Compressors
    typeJournal Paper
    journal volume90
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3609154
    journal fristpage149
    journal lastpage156
    identifier eissn0742-4795
    keywordsCompressors
    keywordsReynolds number
    keywordsFlow (Dynamics)
    keywordsMachinery
    keywordsPressure
    keywordsCascades (Fluid dynamics) AND Design
    treeJournal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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