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...

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Bibliographic Details
Main Author: Morais, A.B. de (author)
Other Authors: Pereira, A.B. (author), Moura, M.F.S.F. de (author)
Format: article
Language:eng
Published: 1000
Subjects:
Polymer-matrix composites (PMCs)
Delamination
Fracture toughness
Mechanical testing
Online Access:http://hdl.handle.net/10773/5221
Country:Portugal
Oai:oai:ria.ua.pt:10773/5221

Internet

http://hdl.handle.net/10773/5221

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