Aeroelastic optimisation of composite structures in aeronautics
Résumé
The main purpose of this work is the aeroelastic optimisation of composite laminates. Composite laminates have become a subject of interest in the past decades due to their high strength to weight ratio. These materials have been widely used in the aeronautics and consequently in aeroelastic tailoring which consists on the optimisation of the composite laminates in order to avoid any kind of aeroelastic instabilities. The Optimisation can be conducted both in a deterministic and a stochastic framework. In this study, both aspects have been modelled and investigated
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