Reliability based optimisation of composite plates under aeroelastic constraints via adapted surrogate modelling and genetic algorithms

Author:

Ballester Claret RogerORCID,Coelho LudovicORCID,Fagiano Christian,Julien Cédric,Lucor Didier,Fabbiane NicolòORCID

Funder

ONERA

Publisher

Elsevier BV

Reference53 articles.

1. Propeller containing diagonally disposed fibrous material;Munk,1949

2. Aeroelastic tailoring of forward swept composite wings;Weisshaar;J Aircr,1981

3. Aeroelastic tailoring of transport aircraft wings: State-of-the-art and potential enabling technologies;Jutte,2014

4. Optimal design of laminated composite structures with ply drops using stacking sequence tables;Irisarri;Compos Struct,2014

5. Optimum stacking sequence design of composite materials part II: Variable stiffness design;Ghiasi;Compos Struct,2010

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