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contributor authorN. Klompas
date accessioned2017-05-08T23:04:40Z
date available2017-05-08T23:04:40Z
date copyrightOctober, 1978
date issued1978
identifier issn1528-8919
identifier otherJETPEZ-26743#647_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90959
description abstractA new method of analyzing multishaft jet engine critical speeds and unbalance response is derived to account for flexible bladed disks, asymmetric mounting, and squeeze film bearing damping. The resulting elliptical shaft whirling drives traveling waves in disks at speeds equal to the sum and the difference of the rotating speed and the whirling speed. To illustrate a possible problem that cannot be predicted by current methods, a sample calculation shows a simplified model representing possible engine parameters tuned so that a critical speed associated with backward whirling is lowered into the operating range by reduction in disk stiffness. In contradiction to the current literature, the rotor is shown highly responsive to unbalance at this critical speed.
publisherThe American Society of Mechanical Engineers (ASME)
titleSignificance of Disk Flexing in Viscous-Damped Jet Engine Dynamics
typeJournal Paper
journal volume100
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446413
journal fristpage647
journal lastpage654
identifier eissn0742-4795
keywordsDynamics (Mechanics)
keywordsDisks
keywordsJet engines
keywordsWhirls
keywordsStiffness
keywordsTravel
keywordsEngines
keywordsWaves
keywordsBearings
keywordsDamping AND Rotors
treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004
contenttypeFulltext


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