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

    Inviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 2—Computational Results

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001::page 101
    Author:
    L. He
    ,
    J. D. Denton
    DOI: 10.1115/1.2929193
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A quasi-three-dimensional inviscid-viscous coupled approached has been developed for unsteady flows around oscillating blades, as described in Part 1. To validate this method, calculations for several steady and unsteady flow cases with strong inviscid-viscous interactions are performed, and the results are compared with the corresponding experiments. Calculated results for unsteady flows around a biconvex cascade and a fan tip section highlight the necessity of including viscous effects in predictions of turbomachinery blade flutter at transonic flow conditions.
    keyword(s): Blades , Unsteady flow , Transonic flow , Turbomachinery , Cascades (Fluid dynamics) AND Flutter (Aerodynamics) ,
    • Download: (1.159Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Inviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 2—Computational Results

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112853
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorL. He
    contributor authorJ. D. Denton
    date accessioned2017-05-08T23:42:56Z
    date available2017-05-08T23:42:56Z
    date copyrightJanuary, 1993
    date issued1993
    identifier issn0889-504X
    identifier otherJOTUEI-28627#101_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112853
    description abstractA quasi-three-dimensional inviscid-viscous coupled approached has been developed for unsteady flows around oscillating blades, as described in Part 1. To validate this method, calculations for several steady and unsteady flow cases with strong inviscid-viscous interactions are performed, and the results are compared with the corresponding experiments. Calculated results for unsteady flows around a biconvex cascade and a fan tip section highlight the necessity of including viscous effects in predictions of turbomachinery blade flutter at transonic flow conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 2—Computational Results
    typeJournal Paper
    journal volume115
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929193
    journal fristpage101
    journal lastpage109
    identifier eissn1528-8900
    keywordsBlades
    keywordsUnsteady flow
    keywordsTransonic flow
    keywordsTurbomachinery
    keywordsCascades (Fluid dynamics) AND Flutter (Aerodynamics)
    treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 001
    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