Interaction Between Coriolis Forces and Mistuning on a Cyclic Symmetric Structure With Geometrical Nonlinearity

Author:

Tacher Anthony1,Thouverez Fabrice2,Armand Jason3

Affiliation:

1. Laboratoire de Tribologie et Dynamique des Systèmes, École Centrale de Lyon, UMR CNRS 5513, 36 Avenue Guy de Collongue, Écully 69134, France; Safran Tech, Modelling & Simulation, Rue des Jeunes Bois, Châteaufort, Magny-Les-Hameaux 78114, France

2. École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Systèmes, UMR CNRS 5513, 36 Avenue Guy de Collongue, Écully 69134, France

3. Safran Tech, Modelling & Simulation, Rue des Jeunes Bois, Châteaufort, Magny-Les-Hameaux 78114, France

Abstract

Abstract An investigation of the interaction between Coriolis forces and mistuning on a cyclic symmetric structure is presented in this paper. The sensitivity of the eigenvalues and eigenvectors to mistuning is first studied with the perturbation method. A lumped parameter model is used to perform a modal analysis using a numerical approach after which geometrical nonlinearity is added to compare behavior with the linear case. Two different modes are thoroughly investigated for different rotational speeds, the first with an eigenvalue isolated from the others and the second presenting a frequency veering zone. The evolution from a standing wave domination at low speeds to a traveling wave domination at high speeds is observed for the isolated mode, whereas a standing wave domination remains around the veering zone for the second mode studied. It is also shown that the geometrical nonlinearity reinforces the mistuning effect versus the Coriolis forces.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference27 articles.

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3. Coriolis Forces in Forced Response Analysis of Mistuned Bladed Disks;ASME J. Turbomach.,2007

4. On Forced Response of a Rotating Integrally Bladed Disk: Predictions and Experiments,2010

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