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contributor authorMoustapha Mbaye
contributor authorJean-Philippe Ousty
contributor authorChristian Soize
date accessioned2017-05-09T00:37:27Z
date available2017-05-09T00:37:27Z
date copyrightNovember, 2010
date issued2010
identifier issn1528-8919
identifier otherJETPEZ-27141#112502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143052
description abstractA new reduction method for vibration analysis of intentionally mistuned bladed disks is presented. The method is built for solving the dynamic problem of cyclic structures with geometric modifications. It is based on the use of the cyclic modes of the different sectors, which can be obtained from a usual cyclic symmetry modal analysis. Hence the projection basis is constituted; as well as, on the whole bladed disk, each sector matrix is reduced by its own modes. The method is validated numerically on a real bladed disk model, by comparing free and forced responses of a full model finite element analysis to those of a reduced-order model using the new reduction method.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Reduced-Order Model of Detuned Cyclic Dynamical Systems With Geometric Modifications Using a Basis of Cyclic Modes
typeJournal Paper
journal volume132
journal issue11
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4000805
journal fristpage112502
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 011
contenttypeFulltext


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