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

    The Application of Actuator Disks to Calculations of the Flow in Turbofan Installations

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004::page 733
    Author:
    W. G. Joo
    ,
    T. P. Hynes
    DOI: 10.1115/1.2841183
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the application of an actuator disk model to the problem of calculating the asymmetric performance of a turbofan operating behind a nonaxisymmetric intake and due to the presence of the engine pylon. Good agreement between predictions and experimental results is demonstrated. Further validation of the model is obtained by comparison with the results of a three-dimensional calculation of an isolated fan operating with a nonaxisymmetric inlet. Some justification of the neglect of unsteady aspects of the flow in the fan is presented. The quantitative features of the interaction of the pylon and fan flow fields are discussed.
    keyword(s): Flow (Dynamics) , Actuators , Disks , Turbofans AND Engines ,
    • Download: (1.293Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      The Application of Actuator Disks to Calculations of the Flow in Turbofan Installations

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119568
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorW. G. Joo
    contributor authorT. P. Hynes
    date accessioned2017-05-08T23:55:02Z
    date available2017-05-08T23:55:02Z
    date copyrightOctober, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28663#733_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119568
    description abstractThis paper discusses the application of an actuator disk model to the problem of calculating the asymmetric performance of a turbofan operating behind a nonaxisymmetric intake and due to the presence of the engine pylon. Good agreement between predictions and experimental results is demonstrated. Further validation of the model is obtained by comparison with the results of a three-dimensional calculation of an isolated fan operating with a nonaxisymmetric inlet. Some justification of the neglect of unsteady aspects of the flow in the fan is presented. The quantitative features of the interaction of the pylon and fan flow fields are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Application of Actuator Disks to Calculations of the Flow in Turbofan Installations
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841183
    journal fristpage733
    journal lastpage741
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsActuators
    keywordsDisks
    keywordsTurbofans AND Engines
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 004
    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