PG-EAM - Programa de Pós-Graduação em Engenharia Aeronáutica e Mecânica
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Artigo 2009

The structural behaviour of stiffened composite panels subjected to in-plane shear loading

Autores

De Almeida, Sérgio F.M.

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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