YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Secondary Flows in Compressor Bladings

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002::page 211
    Author:
    K. Papailiou
    ,
    R. Flot
    ,
    J. Mathieu
    DOI: 10.1115/1.3446274
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Present-day theories for the calculation of the development of end-wall shear layers in compressors demand detailed experimental information for their modeling. Experimental results obtained from compressor and turbine cascades and from single and multistage compressors were used in order to perform a critical examination of the underlying hypotheses of the available calculation methods.
    keyword(s): Flow (Dynamics) , Compressors , Shear (Mechanics) , Modeling AND Turbines ,
    • Download: (1.285Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Secondary Flows in Compressor Bladings

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/89822
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorK. Papailiou
    contributor authorR. Flot
    contributor authorJ. Mathieu
    date accessioned2017-05-08T23:02:48Z
    date available2017-05-08T23:02:48Z
    date copyrightApril, 1977
    date issued1977
    identifier issn1528-8919
    identifier otherJETPEZ-26732#211_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/89822
    description abstractPresent-day theories for the calculation of the development of end-wall shear layers in compressors demand detailed experimental information for their modeling. Experimental results obtained from compressor and turbine cascades and from single and multistage compressors were used in order to perform a critical examination of the underlying hypotheses of the available calculation methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSecondary Flows in Compressor Bladings
    typeJournal Paper
    journal volume99
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446274
    journal fristpage211
    journal lastpage224
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsShear (Mechanics)
    keywordsModeling AND Turbines
    treeJournal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian