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contributor authorA. Muszyńska
contributor authorD. I. G. Jones
date accessioned2017-05-08T23:16:45Z
date available2017-05-08T23:16:45Z
date copyrightOctober, 1983
date issued1983
identifier issn1048-9002
identifier otherJVACEK-28959#434_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97803
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.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Parametric Study of Dynamic Response of a Discrete Model of Turbomachinery Bladed Disk
typeJournal Paper
journal volume105
journal issue4
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.3269125
journal fristpage434
journal lastpage443
identifier eissn1528-8927
keywordsDisks
keywordsDynamic response
keywordsTurbomachinery
keywordsBlades
keywordsDamping
keywordsDesign
keywordsFriction
keywordsCoulombs AND Equations of motion
treeJournal of Vibration and Acoustics:;1983:;volume( 105 ):;issue: 004
contenttypeFulltext


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