Abstract
A method to optimise anisotropic composite plates that vary in thickness and properties across the width is presented. The optimisation problem is divided into two levels. At the first level, Mathematical Programming (MP) is applied, where the plate is divided into several strips, each of them modelled using lamination parameters accounting for their anisotropy. The laminate of each of the strips is assumed to be symmetric, or mid-plane symmetric with 0, 90, 45 or -45 degree ply angles. The plate is subjected to a combined loading under strength, buckling and practical design constraints. Manufacturing details of the plate are embedded within the design variables. At the second level, the actual lay-ups of the plate's strips are obtained using a Genetic Algorithm (GA), accounting for manufacturability and design practices. The novelty of this work lies in: the inclusion of anisotropy for elastic tailoring, manufacturing and practical design considerations, as well as the application of the Rayleigh-Ritz (RR) method to assess buckling analysis in plates that vary in thickness and properties across the width.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 16th International Conference on Composite Materials, ICCM-16 - "A Giant Step Towards Environmental Awareness |
| Subtitle of host publication | From Green Composites to Aerospace" |
| Publisher | International Committee on Composite Materials |
| ISBN (Print) | 9784931136052 |
| Publication status | Published - 2007 |
| Externally published | Yes |
Publication series
| Name | ICCM International Conferences on Composite Materials |
|---|
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 9 Industry, Innovation, and Infrastructure
Keywords
- Anisotropic
- Buckling
- Lamination parameters
- Optimisation
- Rayleigh-Ritz
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