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    Loss and Flow Path Studies on Centrifugal Compressors—Part I

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 275
    Author:
    O. E. Baljé
    DOI: 10.1115/1.3445352
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Relations are derived for the boundary layer momentum thickness growth in channels with adverse pressure gradients and for the maximum allowable momentum thickness to avoid flow separation. These data are obtained by integrating the Truckenbrodt equation stepwise and by extending the Gruschwitz-Schmidbauer separation criterion. Fair agreement between calculated data and test information is demonstrated.
    keyword(s): Momentum , Flow (Dynamics) , Separation (Technology) , Channels (Hydraulic engineering) , Compressors , Boundary layers , Equations , Flow separation , Pressure gradient AND Thickness ,
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      Loss and Flow Path Studies on Centrifugal Compressors—Part I

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142233
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorO. E. Baljé
    date accessioned2017-05-09T00:35:56Z
    date available2017-05-09T00:35:56Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#275_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142233
    description abstractRelations are derived for the boundary layer momentum thickness growth in channels with adverse pressure gradients and for the maximum allowable momentum thickness to avoid flow separation. These data are obtained by integrating the Truckenbrodt equation stepwise and by extending the Gruschwitz-Schmidbauer separation criterion. Fair agreement between calculated data and test information is demonstrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLoss and Flow Path Studies on Centrifugal Compressors—Part I
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445352
    journal fristpage275
    journal lastpage286
    identifier eissn0742-4795
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsChannels (Hydraulic engineering)
    keywordsCompressors
    keywordsBoundary layers
    keywordsEquations
    keywordsFlow separation
    keywordsPressure gradient AND Thickness
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    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
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