Uncertainty quantification for an industrial mistuned bladed disk with geometrical nonlinearities

Evangéline Capiez-Lernout 1 Christian Soize 1 Moustapha Mbaye 2
1 MSME - Laboratoire de Modélisation et Simulation Multi Echelle
2 Turbomeca
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.
Keywords : Uncertainty quantification Nonlinear structural dynamics Mistuned bladed disk Geometrical nonlinearities
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Conference papers
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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⟩

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