Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed DisksSource: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003::page 495Author:E. P. Petrov
DOI: 10.1115/1.2720487Publisher: 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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contributor author | E. P. Petrov | |
date accessioned | 2017-05-09T00:26:07Z | |
date available | 2017-05-09T00:26:07Z | |
date copyright | July, 2007 | |
date issued | 2007 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28739#495_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/137010 | |
description 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Disks | |
type | Journal Paper | |
journal volume | 129 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2720487 | |
journal fristpage | 495 | |
journal lastpage | 502 | |
identifier eissn | 1528-8900 | |
tree | Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003 | |
contenttype | Fulltext |