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contributor authorD. S. Whitehead
date accessioned2017-05-08T23:56:39Z
date available2017-05-08T23:56:39Z
date copyrightJanuary, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26775#115_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120474
description abstractIn 1966 it was shown that the maximum factor by which the amplitude of forced vibration of blades can increase due to mistuning is, with certain assumptions, 1/2(1 + N), where N is the number of blades in the row. This report gives a further investigation of the circumstances when this factor can be obtained. These are small damping, and a relationship must hold between the mistuning distribution γ(s) and the interblade coupling function c(r), where r is the model number. The mistuning distribution must be symmetric about the blade on which maximum amplitude is to occur, s = 0. The coupling function must be symmetric about r = R, where R is the mode number of the excitation. If the coupling is purely mechanical, additional conditions apply. The coupling function c(r) must consist of a number of identical symmetric substrips. A 1976 result for mechanical coupling is amended.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Maximum Factor by Which Forced Vibration of Blades Can Increase Due to Mistuning
typeJournal Paper
journal volume120
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818061
journal fristpage115
journal lastpage119
identifier eissn0742-4795
keywordsVibration
keywordsBlades AND Damping
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001
contenttypeFulltext


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