Roger Ballester Claret, Nicolo Fabbiane, Christian Fagiano, Cedric Julien, Didier Lucor
DOI Number: N/A
Conference number: IFASD-2024-017
Composite materials are essential in aerospace engineering due to their superior strength-to-weight ratio. This work explores the reliability-based design optimisation of composite plates under aeroelastic constraints with a focus on cost efficiency. We utilise a simplified approach focusing on generating surrogate models through conditioned Gaussian Processes, which predict various aeroelastic responses like flutter speed, gust loads, and static forces. These models help in the effective navigation of the composite design space. We introduce a 5 step optimisation algorithm in which we prioritise minimising the gust response and structure mass while adhering to predefined limits on flutter and strain. The proposed approach not only simplifies the optimisation process but also enhances the understanding and reliability of composite material design in aerospace applications, aiming for improved safety and performance.