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contributor authorM. P. Mignolet
contributor authorC.-C. Lin
contributor authorB. H. LaBorde
date accessioned2017-05-09T00:04:52Z
date available2017-05-09T00:04:52Z
date copyrightApril, 2001
date issued2001
identifier issn1528-8919
identifier otherJETPEZ-26803#388_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125216
description abstractA recently introduced perturbation technique is employed to derive a novel closed form model for the probability density function of the resonant and near-resonant, steady state amplitude of blade response in randomly mistuned disks. In its most general form, this model is shown to involve six parameters but, in the important practical case of a pure stiffness (or frequency) mistuning, only three parameters are usually sufficient to completely specify this distribution. A series of numerical examples are presented that demonstrate the reliability of this three-parameter model in accurately predicting the entire probability density function of the amplitude of response, and in particular the large amplitude tail of this distribution, which is the most critical effect of mistuning.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Novel Limit Distribution for the Analysis of Randomly Mistuned Bladed Disks1
typeJournal Paper
journal volume123
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1339001
journal fristpage388
journal lastpage394
identifier eissn0742-4795
keywordsDisks
keywordsBlades
keywordsProbability
keywordsDensity
keywordsStiffness
keywordsSteady state
keywordsDamping AND Reliability
treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 002
contenttypeFulltext


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