Abstract
The current demand for lightweight structures in a wide range of engineering applications leads to using thin-walled composite laminated structures whose behaviour is governed by buckling and postbuckling phenomena. Such a demand is pushing the borders of computational mechanics to enhance methods and algorithms for studying those structures' geometrically nonlinear responses. This work presents some of the authors' developments in analysing lightweight composite laminated structures. The literature survey introduces a family of nite elements known as MISS elements, where MISS stands for mixed isostatic self-equilibrated stresses. The description of those elements, which are derived from the Hellinger-Reissner functional, is followed by a discussion on their advantages concerning displacement-based elements when studying composite laminated thin-walled structures. Subsequently, a framework for the postbuckling analysis of composite structures with the MISS-4C element that uses the Koiter multi-modal approach is presented.
| Original language | English |
|---|---|
| Journal | World Congress in Computational Mechanics and ECCOMAS Congress |
| DOIs | |
| Publication status | Published - 2024 |
| Event | 9th European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2024 - Lisbon, Portugal Duration: 3 Jun 2024 → 7 Jun 2024 |
Keywords
- Composite laminates
- FEM
- Geometrically nonlinear analysis
- Thin-walled structures
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