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J integral for delaminated composite laminates

โœ Scribed by L.J. Lee; D.W. Tu


Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
603 KB
Volume
47
Category
Article
ISSN
0266-3538

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A thermomechanical buckling analysis ofmultilayered laminates with (across-the-width) strip delaminations is conducted on the basis of anisotropic thermoelasticity of the constituent layers and the Kirchhoff Love hypothesis of the classical laminate theory. With the assumption of generalized plane d

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The delamination growth during the pre-or post-buckling phases in composites with a single delamination (one-dimensional model) is investigated. For that purpose, a general nonlinear analysis, using variational principle, with a new set of relations for the decomposition of the total energy release