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dc.contributor.authorA. Muszyńska
dc.contributor.authorD. I. G. Jones
dc.date.accessioned2017-05-08T23:16:45Z
dc.date.available2017-05-08T23:16:45Z
dc.date.copyrightOctober, 1983
dc.date.issued1983
dc.identifier.issn1048-9002
dc.identifier.otherJVACEK-28959#434_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/97803
dc.description.abstractA model consisting of n five-degree-of-freedom subsystems has been developed to characterize some of the mechanical response features of a bladed disk system, including four modes of each blade, n bending modes of the disk, blade-to-blade and blade-to-ground Coulomb friction, structural damping, blade-to-blade mistuning, and various types of excitation. The equations of motion and method of solution are described, and numerical results illustrate some of the interesting effects of various levels of frictional damping on tuned and mistuned systems, which may shed light on some aspects of damped system design and performance.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleA Parametric Study of Dynamic Response of a Discrete Model of Turbomachinery Bladed Disk
dc.typeJournal Paper
dc.journal.volume105
dc.journal.issue4
dc.journal.titleJournal of Vibration and Acoustics
dc.identifier.doi10.1115/1.3269125
dc.journal.fristpage434
dc.journal.lastpage443
dc.identifier.eissn1528-8927
dc.keywordsDisks
dc.keywordsDynamic response
dc.keywordsTurbomachinery
dc.keywordsBlades
dc.keywordsDamping
dc.keywordsDesign
dc.keywordsFriction
dc.keywordsCoulombs AND Equations of motion
dc.treeJournal of Vibration and Acoustics:;1983:;volume( 105 ):;issue: 004
dc.contenttypeFulltext


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