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    Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Disks

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003::page 495
    Author:
    E. P. Petrov
    DOI: 10.1115/1.2720487
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A 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.
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      Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Disks

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    http://yetl.yabesh.ir/yetl1/handle/yetl/137010
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian