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    Mode Localization of a Cracked Blade Disk

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002::page 335
    Author:
    J. H. Kuang
    ,
    B. W. Huang
    DOI: 10.1115/1.2817125
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the effect of blade crack on the mode localization of a rotating blade disk is studied. Pretwisted taper beams are used to simulate blades of a blade disk. The crack on the blade can be regarded as a local disorder of this periodically coupled blades system. An application of Hamilton’s principle and Galerkin’s method is used to formulate the equations of motion of the mistuned system. Effects of pretwisted angle, rotating speed, and crack depth of the blade on the in-plane and off-plane mode localizations of a rotating system are investigated. Numerical results indicate that the increase of rotating speed, pretwisted angle, and crack depth could enhance the localization phenomenon significantly.
    keyword(s): Disks , Blades , Fracture (Materials) , Hamilton's principle , Rotating blades AND Equations of motion ,
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      Mode Localization of a Cracked Blade Disk

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/122161
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. H. Kuang
    contributor authorB. W. Huang
    date accessioned2017-05-08T23:59:38Z
    date available2017-05-08T23:59:38Z
    date copyrightApril, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26788#335_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122161
    description abstractIn this paper, the effect of blade crack on the mode localization of a rotating blade disk is studied. Pretwisted taper beams are used to simulate blades of a blade disk. The crack on the blade can be regarded as a local disorder of this periodically coupled blades system. An application of Hamilton’s principle and Galerkin’s method is used to formulate the equations of motion of the mistuned system. Effects of pretwisted angle, rotating speed, and crack depth of the blade on the in-plane and off-plane mode localizations of a rotating system are investigated. Numerical results indicate that the increase of rotating speed, pretwisted angle, and crack depth could enhance the localization phenomenon significantly.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMode Localization of a Cracked Blade Disk
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2817125
    journal fristpage335
    journal lastpage341
    identifier eissn0742-4795
    keywordsDisks
    keywordsBlades
    keywordsFracture (Materials)
    keywordsHamilton's principle
    keywordsRotating blades AND Equations of motion
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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