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    Rotating Blade Vibration Analysis Using Shells

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002::page 296
    Author:
    A. W. Leissa
    ,
    J. K. Lee
    ,
    A. J. Wang
    DOI: 10.1115/1.3227279
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Shallow shell theory and Ritz method are employed to determine the frequencies and mode shapes of turbomachinery blades having both camber and twist, rotating with non-zero angles of attack. Frequencies obtained for different degrees of shallowness and thickness are compared with results available in the literature, obtained from finite element analyses of nonrotating blades. Frequencies are also determined for a rotating blade, showing the effects of changing the (1) angular velocity of rotation (2) disk radius and (3) angle of attack, as well as the significance of the most important body force terms.
    keyword(s): Shells , Rotating blades , Vibration analysis , Frequency , Blades , Shapes , Thickness , Turbomachinery , Force , Rotation , Finite element analysis AND Disks ,
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      Rotating Blade Vibration Analysis Using Shells

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/95790
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. W. Leissa
    contributor authorJ. K. Lee
    contributor authorA. J. Wang
    date accessioned2017-05-08T23:13:15Z
    date available2017-05-08T23:13:15Z
    date copyrightApril, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26772#296_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95790
    description abstractShallow shell theory and Ritz method are employed to determine the frequencies and mode shapes of turbomachinery blades having both camber and twist, rotating with non-zero angles of attack. Frequencies obtained for different degrees of shallowness and thickness are compared with results available in the literature, obtained from finite element analyses of nonrotating blades. Frequencies are also determined for a rotating blade, showing the effects of changing the (1) angular velocity of rotation (2) disk radius and (3) angle of attack, as well as the significance of the most important body force terms.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRotating Blade Vibration Analysis Using Shells
    typeJournal Paper
    journal volume104
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227279
    journal fristpage296
    journal lastpage302
    identifier eissn0742-4795
    keywordsShells
    keywordsRotating blades
    keywordsVibration analysis
    keywordsFrequency
    keywordsBlades
    keywordsShapes
    keywordsThickness
    keywordsTurbomachinery
    keywordsForce
    keywordsRotation
    keywordsFinite element analysis AND Disks
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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