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

    A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 004::page 893
    Author:
    M.-T. Yang
    ,
    J. H. Griffin
    DOI: 10.1115/1.1385197
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Reduced-order models have been reported in the literature that can be used to predict the harmonic response of mistuned bladed disks. It has been shown that in many cases they exhibit structural fidelity comparable to a finite element analysis of the full bladed disk system while offering a significant improvement in computational efficiency. In these models the blades and disk are treated as distinct substructures. This paper presents a new, simpler approach for developing reduced-order models in which the modes of the mistuned system are represented in terms of a subset of nominal system modes. It has the following attributes: the input requirements are relatively easy to generate; it accurately predicts mistuning effects in regions where frequency veering occurs; as the number of degrees-of-freedom increases it converges to the exact solution; it accurately predicts stresses as well as displacements; and it accurately models the deformation and stresses at the blades’ bases.
    keyword(s): Degrees of freedom , Disks , Blades , Frequency , Finite element analysis , Shapes , Stiffness , Errors AND Force ,
    • Download: (151.7Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/125151
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorM.-T. Yang
    contributor authorJ. H. Griffin
    date accessioned2017-05-09T00:04:44Z
    date available2017-05-09T00:04:44Z
    date copyrightOctober, 2001
    date issued2001
    identifier issn1528-8919
    identifier otherJETPEZ-26807#893_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125151
    description abstractReduced-order models have been reported in the literature that can be used to predict the harmonic response of mistuned bladed disks. It has been shown that in many cases they exhibit structural fidelity comparable to a finite element analysis of the full bladed disk system while offering a significant improvement in computational efficiency. In these models the blades and disk are treated as distinct substructures. This paper presents a new, simpler approach for developing reduced-order models in which the modes of the mistuned system are represented in terms of a subset of nominal system modes. It has the following attributes: the input requirements are relatively easy to generate; it accurately predicts mistuning effects in regions where frequency veering occurs; as the number of degrees-of-freedom increases it converges to the exact solution; it accurately predicts stresses as well as displacements; and it accurately models the deformation and stresses at the blades’ bases.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes
    typeJournal Paper
    journal volume123
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1385197
    journal fristpage893
    journal lastpage900
    identifier eissn0742-4795
    keywordsDegrees of freedom
    keywordsDisks
    keywordsBlades
    keywordsFrequency
    keywordsFinite element analysis
    keywordsShapes
    keywordsStiffness
    keywordsErrors AND Force
    treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;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