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    Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 006::page 61001-1
    Author:
    Pelz, Peter F.
    ,
    Saul, Sebastian
    ,
    Brötz, Johannes
    DOI: 10.1115/1.4053172
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The efficiency, pressure ratio, and shaft power of a fan depends on type, size, working medium, and operating condition. For acceptance tests, a dissimilarity in Reynolds number, Mach number, relative roughness, and relative blade tip clearance of the scaled model and prototype is unavoidable. Hence, the efficiency differs between model and prototype. This difference is quantified by scaling methods. This article presents a validated and physics based, i.e., reliable scaling method for the efficiency, pressure ratio, and shaft power of axial and centrifugal fans operating at subsonic conditions. The method is validated using test results gained on standardized test rigs for different fan types, sizes, and operating conditions. For all scenarios, the presented scaling method provides a much reduced scaling uncertainty compared to the reference method described in ISO 13348.
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      Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4284520
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    contributor authorPelz, Peter F.
    contributor authorSaul, Sebastian
    contributor authorBrötz, Johannes
    date accessioned2022-05-08T08:55:44Z
    date available2022-05-08T08:55:44Z
    date copyright1/28/2022 12:00:00 AM
    date issued2022
    identifier issn0889-504X
    identifier otherturbo_144_6_061001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284520
    description abstractThe efficiency, pressure ratio, and shaft power of a fan depends on type, size, working medium, and operating condition. For acceptance tests, a dissimilarity in Reynolds number, Mach number, relative roughness, and relative blade tip clearance of the scaled model and prototype is unavoidable. Hence, the efficiency differs between model and prototype. This difference is quantified by scaling methods. This article presents a validated and physics based, i.e., reliable scaling method for the efficiency, pressure ratio, and shaft power of axial and centrifugal fans operating at subsonic conditions. The method is validated using test results gained on standardized test rigs for different fan types, sizes, and operating conditions. For all scenarios, the presented scaling method provides a much reduced scaling uncertainty compared to the reference method described in ISO 13348.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEfficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance
    typeJournal Paper
    journal volume144
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4053172
    journal fristpage61001-1
    journal lastpage61001-12
    page12
    treeJournal of Turbomachinery:;2022:;volume( 144 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian