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    Local/Global Effects of Mistuning on the Forced Response of Bladed Disks

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001::page 131
    Author:
    A. J. Rivas-Guerra
    ,
    M. P. Mignolet
    DOI: 10.1115/1.1581898
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The focus of the present investigation is on the assessment and modeling of the local (spanning only a few blades) and global (encompassing the entire disk) effects of mistuning on the forced response of bladed disks. To this end, the concept of localization is first revisited and a new measure of this effect is introduced in terms of the number of blades the mistuning of which actually affects the forced response of a central blade. Using this new metric, it is demonstrated that high responding blades typically exhibit a high level of localization and that the reverse is not necessarily true. Thus, localization is not only disk dependent but also varies from blade-to-blade on the same disk. This observation is then used to validate a partial mistuning approach to the determination of the maximum amplitude of response over the entire population of disks. The results of this study indicate that the largest amplification due to the mistuning occurs at very strong blade-to-blade coupling levels, at the contrary of a general perception, but is associated with large mistuning levels. Finally, the above phenomenological observations are used to devise a modeling technique of both local and global components of mistuning. An example of application is presented that demonstrates the high accuracy of this approach through the entire blade-to-blade coupling domain.
    keyword(s): Disks , Blades , Approximation AND Modeling ,
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      Local/Global Effects of Mistuning on the Forced Response of Bladed Disks

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    http://yetl.yabesh.ir/yetl1/handle/yetl/130075
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    contributor authorA. J. Rivas-Guerra
    contributor authorM. P. Mignolet
    date accessioned2017-05-09T00:13:05Z
    date available2017-05-09T00:13:05Z
    date copyrightJanuary, 2004
    date issued2004
    identifier issn1528-8919
    identifier otherJETPEZ-26825#131_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130075
    description abstractThe focus of the present investigation is on the assessment and modeling of the local (spanning only a few blades) and global (encompassing the entire disk) effects of mistuning on the forced response of bladed disks. To this end, the concept of localization is first revisited and a new measure of this effect is introduced in terms of the number of blades the mistuning of which actually affects the forced response of a central blade. Using this new metric, it is demonstrated that high responding blades typically exhibit a high level of localization and that the reverse is not necessarily true. Thus, localization is not only disk dependent but also varies from blade-to-blade on the same disk. This observation is then used to validate a partial mistuning approach to the determination of the maximum amplitude of response over the entire population of disks. The results of this study indicate that the largest amplification due to the mistuning occurs at very strong blade-to-blade coupling levels, at the contrary of a general perception, but is associated with large mistuning levels. Finally, the above phenomenological observations are used to devise a modeling technique of both local and global components of mistuning. An example of application is presented that demonstrates the high accuracy of this approach through the entire blade-to-blade coupling domain.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLocal/Global Effects of Mistuning on the Forced Response of Bladed Disks
    typeJournal Paper
    journal volume126
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1581898
    journal fristpage131
    journal lastpage141
    identifier eissn0742-4795
    keywordsDisks
    keywordsBlades
    keywordsApproximation AND Modeling
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001
    contenttypeFulltext
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