Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description


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

01/03/2014

Resumo

The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently introduced methodology: the asymptotic mistuning model. The asymptotic mistuning model is an extremely reduced, simplified model that is derived directly from the full formulation of the mistuned bladed disk using a consistent perturbative procedure based on the relative smallness of the mistuning distortion. A detailed description of the derivation of the asymptotic mistuning model for a realistic bladed disk configuration is presented. The asymptotic mistuning model results for several different mistuning patterns and forcing conditions are compared with those from a high-resolution finite element model. The asymptotic mistuning model produces quantitatively accurate results, and, probably more relevant, it gives precise information about the factors (tuned modes and components of the mistuning pattern) that actually play a role in the vibrational forced response of mistuned bladed disks.

Formato

application/pdf

Identificador

http://oa.upm.es/37740/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/37740/7/INVE_MEM_2014_203420.pdf

http://arc.aiaa.org/doi/abs/10.2514/1.B34631

info:eu-repo/semantics/altIdentifier/doi/10.2514/1.B34631

Direitos

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

info:eu-repo/semantics/openAccess

Fonte

Journal of Propulsion and Power, ISSN 0748-4658, 2014-03, Vol. 30, No. 2

Palavras-Chave #Mecánica #Aeronáutica
Tipo

info:eu-repo/semantics/article

Artículo

PeerReviewed