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contributor authorJ. A. Kenyon
contributor authorJ. H. Griffin
contributor authorD. M. Feiner
date accessioned2017-05-09T00:11:43Z
date available2017-05-09T00:11:43Z
date copyrightApril, 2003
date issued2003
identifier issn0889-504X
identifier otherJOTUEI-28702#352_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129277
description abstractA method is presented for obtaining maximum bladed disk forced response from distortion of a structural mode. It is shown that maximum response from mode distortion in a bladed disk occurs when the harmonic components of a distorted mode superimpose in a certain manner, causing localization of the mode and strong response in a particular blade. In addition, it is shown that the response of an intentionally mistuned system with maximum response does not change significantly when small random mistuning is added to the system. A method is described for calculating the structural mistuning necessary to obtain the distorted mode that gives maximum response. The theory is validated numerically.
publisherThe American Society of Mechanical Engineers (ASME)
titleMaximum Bladed Disk Forced Response From Distortion of a Structural Mode
typeJournal Paper
journal volume125
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1540118
journal fristpage352
journal lastpage363
identifier eissn1528-8900
keywordsDamping
keywordsDisks
keywordsBlades AND Frequency
treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 002
contenttypeFulltext


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