Optimisation of ply drop order in variable stiffness laminates

Journal Article (2016)
Authors

François Xavier Irisarri (Office National d'Etudes et de Recherches Aerospatiales)

Daniël M J Peeters (Aerospace Structures & Computational Mechanics)

M. M. Abdalla (Aerospace Structures & Computational Mechanics)

Research Group
Aerospace Structures & Computational Mechanics
More Info
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Publication Year
2016
Language
English
Research Group
Aerospace Structures & Computational Mechanics
Volume number
152
Pages (from-to)
791-799
DOI:
https://doi.org/10.1016/j.compstruct.2016.05.076

Abstract

Modern composite structures offer multiple avenues of optimising performance. One avenue is to optimise a single stacking sequence over the structure leading to constant stiffness designs. Another avenue is to allow the stacking sequence to vary over the structure leading to variable stiffness laminates. This may be achieved either by dropping plies or by steering the fibres. When using ply drops to optimise the thickness distribution two different set of decisions are involved: the selection of ply drop boundaries, and the selection of the ply drop order. In this paper, the fibre angle distribution, the ply drop boundaries, and the ply drop order are simultaneously optimised. The optimisation of fibre angle distribution lends itself easily to gradient based methods. The ply drop boundary optimisation is formulated using topology optimisation techniques and is thus solvable using gradient based methods as well. The ply drop order optimisation requires discrete variables and is hence approached using an evolutionary algorithm based on stacking sequence tables. In this paper an efficient multi-step algorithm is developed to combine the optimisation of all aspects of variable stiffness laminates. The results indicate that significantly improved designs may be obtained by including the ply drop order in the optimisation.

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