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contributor authorCarlos Martel
contributor authorRoque Corral
date accessioned2017-05-09T00:32:44Z
date available2017-05-09T00:32:44Z
date copyrightMarch, 2009
date issued2009
identifier issn1528-8919
identifier otherJETPEZ-27059#022506_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140508
description abstractThe problem of determining the maximum forced response vibration amplification that can be produced just by the addition of a small mistuning to a perfectly cyclical bladed disk still remains not completely clear. In this paper we apply a recently introduced perturbation methodology, the asymptotic mistuning model (AMM), to determine which are the key ingredients of this amplification process and to evaluate the maximum mistuning amplification factor that a given modal family with a particular distribution of tuned frequencies can exhibit. A more accurate upper bound for the maximum forced response amplification of a mistuned bladed disk is obtained from this description, and the results of the AMM are validated numerically using a simple mass-spring model.
publisherThe American Society of Mechanical Engineers (ASME)
titleAsymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response
typeJournal Paper
journal volume131
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2968868
journal fristpage22506
identifier eissn0742-4795
keywordsDisks
keywordsFrequency
keywordsDamping
keywordsEngines
keywordsSprings AND Vibration
treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002
contenttypeFulltext


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