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    Experimental Demonstration of Maximum Mistuned Bladed Disk Forced Response

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 004::page 673
    Author:
    J. A. Kenyon
    ,
    J. H. Griffin
    DOI: 10.1115/1.1624847
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory was previously developed for predicting robust maximum forced response in mistuned bladed disks from distortion of a structural mode. This paper describes an experiment to demonstrate the theory. A bladed disk is designed to be sufficiently sensitive to mistuning to obtain maximum response. The maximum amplitude magnification from mistuning is predicted using the theory, 1.918. The bladed disk is intentionally mistuned to obtain the maximum response, and the response to an engine order traveling wave excitation is measured. The measured amplitude magnification is in close agreement with the theory. The robustness of the maximum response is demonstrated.
    keyword(s): Disks , Blades , Damping , Waves AND Frequency ,
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      Experimental Demonstration of Maximum Mistuned Bladed Disk Forced Response

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    https://yetl.yabesh.ir/yetl1/handle/yetl/129221
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    contributor authorJ. A. Kenyon
    contributor authorJ. H. Griffin
    date accessioned2017-05-09T00:11:37Z
    date available2017-05-09T00:11:37Z
    date copyrightOctober, 2003
    date issued2003
    identifier issn0889-504X
    identifier otherJOTUEI-28706#673_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129221
    description abstractA theory was previously developed for predicting robust maximum forced response in mistuned bladed disks from distortion of a structural mode. This paper describes an experiment to demonstrate the theory. A bladed disk is designed to be sufficiently sensitive to mistuning to obtain maximum response. The maximum amplitude magnification from mistuning is predicted using the theory, 1.918. The bladed disk is intentionally mistuned to obtain the maximum response, and the response to an engine order traveling wave excitation is measured. The measured amplitude magnification is in close agreement with the theory. The robustness of the maximum response is demonstrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Demonstration of Maximum Mistuned Bladed Disk Forced Response
    typeJournal Paper
    journal volume125
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1624847
    journal fristpage673
    journal lastpage681
    identifier eissn1528-8900
    keywordsDisks
    keywordsBlades
    keywordsDamping
    keywordsWaves AND Frequency
    treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 004
    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
    yabeshDSpacePersian