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    On Predicting the Resonant Response of Bladed Disk Assemblies

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001::page 45
    Author:
    J. H. Griffin
    DOI: 10.1115/1.3240085
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The vibratory responses of blades in gas turbine engines vary because of mistuning. An approach is developed for calculating the statistical distribution of peak resonant stresses in engine blading. It is used to predict the vibratory response of an un-shrouded fan stage. The results of the calculation compare favorably with test data for the lower frequency modes. The procedure can be used to predict fleet durability and offers a practical engineering approach for dealing with stage mistuning.
    keyword(s): Engines , Stress , Durability , Gas turbines , Disks , Blades AND Statistical distributions ,
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      On Predicting the Resonant Response of Bladed Disk Assemblies

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103915
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    contributor authorJ. H. Griffin
    date accessioned2017-05-08T23:27:10Z
    date available2017-05-08T23:27:10Z
    date copyrightJanuary, 1988
    date issued1988
    identifier issn1528-8919
    identifier otherJETPEZ-26651#45_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103915
    description abstractThe vibratory responses of blades in gas turbine engines vary because of mistuning. An approach is developed for calculating the statistical distribution of peak resonant stresses in engine blading. It is used to predict the vibratory response of an un-shrouded fan stage. The results of the calculation compare favorably with test data for the lower frequency modes. The procedure can be used to predict fleet durability and offers a practical engineering approach for dealing with stage mistuning.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn Predicting the Resonant Response of Bladed Disk Assemblies
    typeJournal Paper
    journal volume110
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240085
    journal fristpage45
    journal lastpage50
    identifier eissn0742-4795
    keywordsEngines
    keywordsStress
    keywordsDurability
    keywordsGas turbines
    keywordsDisks
    keywordsBlades AND Statistical distributions
    treeJournal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001
    contenttypeFulltext
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