Mode III interlaminar fracture of carbon/epoxy laminates using the Six-Point Edge Crack Torsion (6ECT)

The recently proposed Six-Point Edge Crack Torsion (6ECT) test was used to evaluate the mode III interlaminar fracture of carbon/epoxy laminates. Plate specimens with starter delaminations in 0/0, 0/90 and 0/45 interfaces were tested. Data reduction was performed with an effective crack scheme valid...

ver descrição completa

Detalhes bibliográficos
Autor principal: Morais, A.B. de (author)
Outros Autores: Pereira, A.B. (author), Moura, M.F.S.F. de (author)
Formato: article
Idioma:eng
Publicado em: 1000
Assuntos:
Texto completo:http://hdl.handle.net/10773/5221
País:Portugal
Oai:oai:ria.ua.pt:10773/5221