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

    An Experiment With Aspect Ratio as a Means of Extending the Useful Range of a Transonic Inlet Stage of an Axial Flow Compressor

    Source: Journal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 003::page 243
    Author:
    W. C. Swan
    DOI: 10.1115/1.3677586
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experiment in unstalled range of a transonic axial flow compressor stage is discussed. Two rotors of identical design, but of differing aspect ratio, are compared. The study suggests that some criteria other than blade chord Reynolds number be used to define chord lengths of transonic stages.
    keyword(s): Axial flow , Chords (Trusses) , Design , Rotors , Blades AND Reynolds number ,
    • Download: (1.412Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      An Experiment With Aspect Ratio as a Means of Extending the Useful Range of a Transonic Inlet Stage of an Axial Flow Compressor

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/99513
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorW. C. Swan
    date accessioned2017-05-08T23:19:41Z
    date available2017-05-08T23:19:41Z
    date copyrightJuly, 1964
    date issued1964
    identifier issn1528-8919
    identifier otherJETPEZ-26635#243_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99513
    description abstractAn experiment in unstalled range of a transonic axial flow compressor stage is discussed. Two rotors of identical design, but of differing aspect ratio, are compared. The study suggests that some criteria other than blade chord Reynolds number be used to define chord lengths of transonic stages.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experiment With Aspect Ratio as a Means of Extending the Useful Range of a Transonic Inlet Stage of an Axial Flow Compressor
    typeJournal Paper
    journal volume86
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3677586
    journal fristpage243
    journal lastpage246
    identifier eissn0742-4795
    keywordsAxial flow
    keywordsChords (Trusses)
    keywordsDesign
    keywordsRotors
    keywordsBlades AND Reynolds number
    treeJournal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 003
    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