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contributor authorJ. H. Kuang
contributor authorB. W. Huang
date accessioned2017-05-08T23:59:38Z
date available2017-05-08T23:59:38Z
date copyrightApril, 1999
date issued1999
identifier issn1528-8919
identifier otherJETPEZ-26788#335_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122161
description abstractIn this paper, the effect of blade crack on the mode localization of a rotating blade disk is studied. Pretwisted taper beams are used to simulate blades of a blade disk. The crack on the blade can be regarded as a local disorder of this periodically coupled blades system. An application of Hamilton’s principle and Galerkin’s method is used to formulate the equations of motion of the mistuned system. Effects of pretwisted angle, rotating speed, and crack depth of the blade on the in-plane and off-plane mode localizations of a rotating system are investigated. Numerical results indicate that the increase of rotating speed, pretwisted angle, and crack depth could enhance the localization phenomenon significantly.
publisherThe American Society of Mechanical Engineers (ASME)
titleMode Localization of a Cracked Blade Disk
typeJournal Paper
journal volume121
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2817125
journal fristpage335
journal lastpage341
identifier eissn0742-4795
keywordsDisks
keywordsBlades
keywordsFracture (Materials)
keywordsHamilton's principle
keywordsRotating blades AND Equations of motion
treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002
contenttypeFulltext


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