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contributor authorD. M. Feiner
contributor authorJ. H. Griffin
date accessioned2017-05-09T00:14:43Z
date available2017-05-09T00:14:43Z
date copyrightJanuary, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28708#150_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131013
description abstractThis paper is the first in a two-part study of identifying mistuning in bladed disks. It develops a new method of mistuning identification based on measurements of the vibratory response of the system as a whole. As a system-based method, this approach is particularly suited to integrally bladed rotors, whose blades cannot be removed for individual measurements. The method is based on a recently developed reduced order model of mistuning called the fundamental mistuning model (FMM) and is applicable to isolated families of modes. Two versions of FMM system identification are presented: a basic version that requires some prior knowledge of the system’s properties, and a somewhat more complex version that determines the mistuning completely from experimental data.
publisherThe American Society of Mechanical Engineers (ASME)
titleMistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory
typeJournal Paper
journal volume126
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1643913
journal fristpage150
journal lastpage158
identifier eissn1528-8900
keywordsRotors
keywordsDisks
keywordsBlades
keywordsFrequency
keywordsEquations AND Measurement
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 001
contenttypeFulltext


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