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contributor authorE. P. Petrov
date accessioned2017-05-09T00:26:07Z
date available2017-05-09T00:26:07Z
date copyrightJuly, 2007
date issued2007
identifier issn0889-504X
identifier otherJOTUEI-28739#495_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137010
description abstractA method has been developed to calculate directly resonance frequencies and resonance amplitudes as functions of design parameters or as a function of excitation levels. The method provides, for the first time, this capability for analysis of strongly nonlinear periodic vibrations of bladed disks and other structures with nonlinear interaction at contact interfaces. A criterion for determination of major, sub-, and superharmonic resonance peaks has been formulated. Analytical expressions have been derived for accurate evaluation of the criterion and for tracing resonance regimes as function of such contact interface parameters as gap and interference values, friction and contact stiffness coefficients, and normal stresses. High accuracy and efficiency of the new method have been demonstrated on numerical examples including a large-scale nonlinear bladed disk model and major types of contact interfaces including friction contact interfaces, gaps, and cubic nonlinearities.
publisherThe American Society of Mechanical Engineers (ASME)
titleDirect Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Disks
typeJournal Paper
journal volume129
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2720487
journal fristpage495
journal lastpage502
identifier eissn1528-8900
treeJournal of Turbomachinery:;2007:;volume( 129 ):;issue: 003
contenttypeFulltext


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