Mode III interlaminar fracture of carbon/epoxy laminates using the Six-Point Edge Crack Torsion (6ECT)-Reference-Cited by-同舟云学术

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

Published:2011-11 Issue:11 Volume:42 Page:1793-1799
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

de Morais A.B.,Pereira A.B.,de Moura M.F.S.F.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference33 articles.

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3. O’Brien TK, Raju IS. Strain energy release rate analysis of delamination around an open hole in composite materials. In: 25th AIAA/ASME/ASCE/AHS structures, structural dynamics and materials conference, Palm Springs, CA; 1984: p. 526–36.

4. Effect of mode III fracture on composite laminates;Ge;Compos Struct,2004

5. Mode III interlaminar fracture characterization of composite materials;Donaldson;Compos Sci Technol,1988

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