Damage model for composites defined in terms of available data

被引:32
作者
Barbero, EJ [1 ]
Lonetti, P
机构
[1] W Virginia Univ, Dept Mech & Aerosp Engn, Construct Facil Ctr, Morgantown, WV 26506 USA
[2] Univ Calabria, Arcavacata Di Rende, Italy
来源
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES | 2001年 / 8卷 / 04期
关键词
D O I
10.1080/107594101753172539
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A model to predict stiffness reduction and stress redistribution due to damage of laminated polymer composites is presented. The material properties required by the model are limited to those already available for unidirectional composites. Classical lamination theory is generalized for the case of a continuously damaging material using concepts from continuous damage mechanics. The Tsai-Wu failure criteria can be recovered as a limiting case. The damage model is validated with experimental results for various laminates built with aramid/epoxy, T300/5208, and T300/914 carbon/epoxy.
引用
收藏
页码:299 / 315
页数:17
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