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    A Novel Limit Distribution for the Analysis of Randomly Mistuned Bladed Disks1

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 002::page 388
    Author:
    M. P. Mignolet
    ,
    C.-C. Lin
    ,
    B. H. LaBorde
    DOI: 10.1115/1.1339001
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A recently introduced perturbation technique is employed to derive a novel closed form model for the probability density function of the resonant and near-resonant, steady state amplitude of blade response in randomly mistuned disks. In its most general form, this model is shown to involve six parameters but, in the important practical case of a pure stiffness (or frequency) mistuning, only three parameters are usually sufficient to completely specify this distribution. A series of numerical examples are presented that demonstrate the reliability of this three-parameter model in accurately predicting the entire probability density function of the amplitude of response, and in particular the large amplitude tail of this distribution, which is the most critical effect of mistuning.
    keyword(s): Disks , Blades , Probability , Density , Stiffness , Steady state , Damping AND Reliability ,
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      A Novel Limit Distribution for the Analysis of Randomly Mistuned Bladed Disks1

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/125216
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. P. Mignolet
    contributor authorC.-C. Lin
    contributor authorB. H. LaBorde
    date accessioned2017-05-09T00:04:52Z
    date available2017-05-09T00:04:52Z
    date copyrightApril, 2001
    date issued2001
    identifier issn1528-8919
    identifier otherJETPEZ-26803#388_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125216
    description abstractA recently introduced perturbation technique is employed to derive a novel closed form model for the probability density function of the resonant and near-resonant, steady state amplitude of blade response in randomly mistuned disks. In its most general form, this model is shown to involve six parameters but, in the important practical case of a pure stiffness (or frequency) mistuning, only three parameters are usually sufficient to completely specify this distribution. A series of numerical examples are presented that demonstrate the reliability of this three-parameter model in accurately predicting the entire probability density function of the amplitude of response, and in particular the large amplitude tail of this distribution, which is the most critical effect of mistuning.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Novel Limit Distribution for the Analysis of Randomly Mistuned Bladed Disks1
    typeJournal Paper
    journal volume123
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1339001
    journal fristpage388
    journal lastpage394
    identifier eissn0742-4795
    keywordsDisks
    keywordsBlades
    keywordsProbability
    keywordsDensity
    keywordsStiffness
    keywordsSteady state
    keywordsDamping AND Reliability
    treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;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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