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contributor authorJ. T. Wagner
date accessioned2017-05-08T23:52:22Z
date available2017-05-08T23:52:22Z
date copyrightOctober, 1967
date issued1967
identifier issn1528-8919
identifier otherJETPEZ-26663#502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118079
description abstractThe forced vibration response of subsystems with different natural frequencies and damping, attached to a foundation with finite stiffness or mass, is calculated. Analytical models include simulations of turbomachine blading on a flexible disk or on a rotor with finite mass. Coupling through the disk or rotor explains variations in resonant frequencies and amplitudes that have been observed in blade-vibration tests. Effects on damping measurements are also determined.
publisherThe American Society of Mechanical Engineers (ASME)
titleCoupling of Turbomachine Blade Vibrations Through the Rotor
typeJournal Paper
journal volume89
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3616718
journal fristpage502
journal lastpage512
identifier eissn0742-4795
keywordsRotors
keywordsVibration
keywordsBlades
keywordsTurbomachinery
keywordsFrequency
keywordsDisks
keywordsDamping
keywordsEngineering simulation
keywordsStiffness AND Measurement
treeJournal of Engineering for Gas Turbines and Power:;1967:;volume( 089 ):;issue: 004
contenttypeFulltext


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