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contributor authorF. Victor
contributor authorF. Ellyin
date accessioned2017-05-08T23:10:26Z
date available2017-05-08T23:10:26Z
date copyrightJune, 1981
date issued1981
identifier issn0021-8936
identifier otherJAMCAV-26177#419_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94182
description abstractThe dynamic response of a simple beam excited at its midspan by the action of a turbomachine secured to it, is investigated in detail. The forcing function includes transients at startup or shutdown. Effects of the shear deformation, rotatory inertia, and the internal viscous damping, which may depend on the frequency, are considered individually as well as in combined forms. The results indicate that the maximum amplitude of vibration is highly dependent on the acceleration rate through the critical frequency. There is also an apparent shift in its position as compared to the classical resonance frequency. Influences of shear deformation and rotatory inertia are significant when the supporting structure (or foundation) is relatively massive.
publisherThe American Society of Mechanical Engineers (ASME)
titleAcceleration of Unbalanced Rotor Through the Resonance of Supporting Structure
typeJournal Paper
journal volume48
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3157632
journal fristpage419
journal lastpage424
identifier eissn1528-9036
keywordsResonance
keywordsRotors
keywordsShear deformation
keywordsInertia (Mechanics)
keywordsTurbomachinery
keywordsVibration
keywordsDynamic response AND Damping
treeJournal of Applied Mechanics:;1981:;volume( 048 ):;issue: 002
contenttypeFulltext


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