Uncertainty quantification for an industrial mistuned bladed disk with geometrical nonlinearities - Archive ouverte HAL Access content directly
Conference Papers Year :

Uncertainty quantification for an industrial mistuned bladed disk with geometrical nonlinearities

Abstract

Recently, a methodology allowing a stochastic nonlinear reduced-order model to be constructed in the context of the non-linear mistuning induced by geometric nonlinearities has been proposed. The present work is devoted to an industrial application for which the centrifugal stiffening due to rotational effects is also included. The nonlinear mistuned forced response is investigated in the time-domain by using a spatial cyclic load over a given excitation frequency range. The geometric nonlinear mis-tuned analysis is performed over the frequency range by using the Fast-Fourier Transform of the time response. A sensitivity analysis is conducted with respect to the load level, giving rise to secondary resonances, which appear outside the excitation frequency range and which can exhibit a particular sensitivity to uncertainties. Such new complex dynamical situation, induced by the coupling between the geometrical nonlinearities and the mistuning phenomenon, is analyzed in details.
Fichier principal
Vignette du fichier
conference-2015-TURBOEXPO-Montreal-Canada-June-15-19-capiez-soize-mbaye-preprint.pdf (1.01 Mo) Télécharger le fichier
Origin : Files produced by the author(s)
Loading...

Dates and versions

hal-01164483 , version 1 (17-06-2015)

Identifiers

  • HAL Id : hal-01164483 , version 1

Cite

Evangéline Capiez-Lernout, Christian Soize, Moustapha Mbaye. Uncertainty quantification for an industrial mistuned bladed disk with geometrical nonlinearities. 60th ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, ASME, Jun 2015, Montreal, Canada. pp.1-10. ⟨hal-01164483⟩
88 View
194 Download

Share

Gmail Facebook Twitter LinkedIn More