Forced response of Bladed Disks with Damping Mistuning


Autoria(s): Khemiri, Oualid; Martel Escobar, Carlos; Corral, Roque
Data(s)

2011

Resumo

The effect of mistuning on the vibration of bladed disks has been extensively studied in the past 30 years. Most of these analysis typically cover the case of small variations of the elastic characteristics (mass and stiffness) of the blades. In this work we study the not so common case of the forced response of a stable rotor with damping mistuning. The Asymptotic Mistuning Model (AMM) is used to analyze this problem. The AMM methodology provides a simplified model that describes the effect of blade to blade damping variation, and gives precise information on the underlying mechanisms involved in the action of damping mistuning.

Formato

application/pdf

Identificador

http://oa.upm.es/12904/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/12904/1/INVE_MEM_2011_108141.pdf

http://dx.doi.org/10.1115/GT2011-45802

Direitos

http://creativecommons.org/licenses/by-nc-nd/3.0/es/

info:eu-repo/semantics/restrictedAccess

Fonte

Proceedings of ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition (GT2011) | ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition (GT2011) | June 6–10, 2011 | Vancouver, British Columbia, Canada

Palavras-Chave #Aeronáutica
Tipo

info:eu-repo/semantics/conferenceObject

Ponencia en Congreso o Jornada

PeerReviewed