TY - JOUR
T1 - RECENT ADVANCES IN THE POSTBUCKLING ANALYSIS OF COMPOSITE LAMINATED STRUCTURES
AU - Liguori, Francesco S.
AU - Zucco, Giovanni
AU - Madeo, Antonio
N1 - Publisher Copyright:
© 2024, Scipedia S.L., All rights reserved.
PY - 2024
Y1 - 2024
N2 - 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.
AB - 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.
KW - Composite laminates
KW - FEM
KW - Geometrically nonlinear analysis
KW - Thin-walled structures
UR - https://www.scopus.com/pages/publications/105012421528
U2 - 10.23967/eccomas.2024.012
DO - 10.23967/eccomas.2024.012
M3 - Conference article
AN - SCOPUS:105012421528
SN - 2696-6999
JO - World Congress in Computational Mechanics and ECCOMAS Congress
JF - World Congress in Computational Mechanics and ECCOMAS Congress
T2 - 9th European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2024
Y2 - 3 June 2024 through 7 June 2024
ER -