contributor author | Carlos Martel | |
contributor author | Roque Corral | |
date accessioned | 2017-05-09T00:32:44Z | |
date available | 2017-05-09T00:32:44Z | |
date copyright | March, 2009 | |
date issued | 2009 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-27059#022506_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/140508 | |
description abstract | The problem of determining the maximum forced response vibration amplification that can be produced just by the addition of a small mistuning to a perfectly cyclical bladed disk still remains not completely clear. In this paper we apply a recently introduced perturbation methodology, the asymptotic mistuning model (AMM), to determine which are the key ingredients of this amplification process and to evaluate the maximum mistuning amplification factor that a given modal family with a particular distribution of tuned frequencies can exhibit. A more accurate upper bound for the maximum forced response amplification of a mistuned bladed disk is obtained from this description, and the results of the AMM are validated numerically using a simple mass-spring model. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response | |
type | Journal Paper | |
journal volume | 131 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2968868 | |
journal fristpage | 22506 | |
identifier eissn | 0742-4795 | |
keywords | Disks | |
keywords | Frequency | |
keywords | Damping | |
keywords | Engines | |
keywords | Springs AND Vibration | |
tree | Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002 | |
contenttype | Fulltext | |