YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • 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

    Closure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002::page 255
    Author:
    W. C. Zierke
    ,
    S. Deutsch
    DOI: 10.1115/1.2927641
    Publisher: The American Society of Mechanical Engineers (ASME)
    keyword(s): Flow (Dynamics) , Compressors , Cascades (Fluid dynamics) , Boundary layers AND Blades ,
    • Download: (153.6Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Closure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107749
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorW. C. Zierke
    contributor authorS. Deutsch
    date accessioned2017-05-08T23:34:07Z
    date available2017-05-08T23:34:07Z
    date copyrightApril, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28601#255_2.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107749
    publisherThe American Society of Mechanical Engineers (ASME)
    titleClosure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)
    typeJournal Paper
    journal volume112
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927641
    journal fristpage255
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsCascades (Fluid dynamics)
    keywordsBoundary layers AND Blades
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;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