Damage Evolution of Laminated Composites Using Continuum Damage Mechanics Incorporate with Interface Element

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Abstract:

In this paper, 3D continuum damage mechanics (CDM) incorporated with layer-wise theory and interface element is employed to investigate the progressive damage inside and between the laminate's layers under quasi-static axial loading. For this purpose, a finite element program is developed. To simulate the delamination, a quadratic interface element is used which is compatible with the 8-node numerical layers of layer-wise theory. Matrix cracking and delamination initiation and propagation of [302/-302]s angle-ply laminate are investigated and the obtained results are compared with the available experimental evidence.

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Periodical:

Key Engineering Materials (Volumes 385-387)

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277-280

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Online since:

July 2008

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© 2008 Trans Tech Publications Ltd. All Rights Reserved

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