A High-Accuracy Model Reduction for Analysis of Nonlinear Vibrations in Structures With Contact InterfacesSource: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 010::page 102503Author:E. P. Petrov
DOI: 10.1115/1.4002810Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A highly accurate and computationally efficient method is proposed for reduced modeling of jointed structures in the frequency domain analysis of nonlinear steady-state forced response. The method has significant advantages comparing with the popular variety of mode synthesis methods or forced response matrix methods and can be easily implemented in the nonlinear forced response analysis using standard finite element codes. The superior qualities of the new method are demonstrated on a set of major problems of nonlinear forced response analysis of bladed disks with contact interfaces: (i) at blade roots, (ii) between interlock shrouds, and (iii) at underplatform dampers. The numerical properties of the method are thoroughly studied on a number of special test cases.
keyword(s): Friction , Disks , Frequency , Modeling , Dampers , Blades , Resonance , Finite element model , Vibration AND Shapes ,
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contributor author | E. P. Petrov | |
date accessioned | 2017-05-09T00:43:28Z | |
date available | 2017-05-09T00:43:28Z | |
date copyright | October, 2011 | |
date issued | 2011 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-27174#102503_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/145925 | |
description abstract | A highly accurate and computationally efficient method is proposed for reduced modeling of jointed structures in the frequency domain analysis of nonlinear steady-state forced response. The method has significant advantages comparing with the popular variety of mode synthesis methods or forced response matrix methods and can be easily implemented in the nonlinear forced response analysis using standard finite element codes. The superior qualities of the new method are demonstrated on a set of major problems of nonlinear forced response analysis of bladed disks with contact interfaces: (i) at blade roots, (ii) between interlock shrouds, and (iii) at underplatform dampers. The numerical properties of the method are thoroughly studied on a number of special test cases. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | A High-Accuracy Model Reduction for Analysis of Nonlinear Vibrations in Structures With Contact Interfaces | |
type | Journal Paper | |
journal volume | 133 | |
journal issue | 10 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4002810 | |
journal fristpage | 102503 | |
identifier eissn | 0742-4795 | |
keywords | Friction | |
keywords | Disks | |
keywords | Frequency | |
keywords | Modeling | |
keywords | Dampers | |
keywords | Blades | |
keywords | Resonance | |
keywords | Finite element model | |
keywords | Vibration AND Shapes | |
tree | Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 010 | |
contenttype | Fulltext |