A.Dugeai, A.Placzek, Y. Mauffrey, S. Verley

DOI Number: N/A

Conference number: IFASD-2017-060

This paper presents the status of current development and research activities concerning the modelling of aeroelastic phenomena of rotating machines. A first insight will be given into the activities conducted in the frame of stage and multi-stage configurations of compressors. A second topic will be addressed concerning the development of methodologies for the taking into account of geometrical non-linear structural behaviour in the modelling of static aeroelasticity of large fan blades. An overview of recent applications in the field of turbomachinery aeroelasticity will be drawn. Perspectives of new activities will be given.

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