Artigo
2009
The structural behaviour of stiffened composite panels subjected to in-plane shear loading
Autores
Iccm International Conferences on Composite Materials
1
Citações
3
Autores
Resumo
This work deals with a numerical investigation on the structural behaviour of stiffened composite panels subjected to in-plane shear loads in the post-buckling regime. The modelling approach takes into account large deformations and material nonlinearity effects by using a damage mechanics based progressive failure model.
Palavras-chave
Composite
Damage mechanics
Finite elements
Post-buckling
Engineering (all)
(ENGI)
Ceramics and Composites
(MATE)
: Scopus
Última atualização: 2026-06-25
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2-s2.0-85076867581

