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contributor authorJ. A. Kenyon
contributor authorJ. H. Griffin
date accessioned2017-05-09T00:11:37Z
date available2017-05-09T00:11:37Z
date copyrightOctober, 2003
date issued2003
identifier issn0889-504X
identifier otherJOTUEI-28706#673_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129221
description abstractA theory was previously developed for predicting robust maximum forced response in mistuned bladed disks from distortion of a structural mode. This paper describes an experiment to demonstrate the theory. A bladed disk is designed to be sufficiently sensitive to mistuning to obtain maximum response. The maximum amplitude magnification from mistuning is predicted using the theory, 1.918. The bladed disk is intentionally mistuned to obtain the maximum response, and the response to an engine order traveling wave excitation is measured. The measured amplitude magnification is in close agreement with the theory. The robustness of the maximum response is demonstrated.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Demonstration of Maximum Mistuned Bladed Disk Forced Response
typeJournal Paper
journal volume125
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1624847
journal fristpage673
journal lastpage681
identifier eissn1528-8900
keywordsDisks
keywordsBlades
keywordsDamping
keywordsWaves AND Frequency
treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 004
contenttypeFulltext


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