Report on analysis of the non-linear behaviour using bifurcation theory applied to the coupled aeroelastic system with an assumed mode model of the non-linear structure.

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Report on analysis of the nonlinear behaviour using bifurcation theory applied to the coupled aeroelastic system with an assumed mode model of the nonlinear structure
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Web resources: https://ec.europa.eu/research/participants/documents/downloadPublic?documentIds=080166e5ad28a478&appId=PPGMS
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