A continuum damage description for a discrete crack modeling approach for delamination migration in composite laminates
Author:
Affiliation:
1. Global Engineering and Materials, Inc.
2. University of Connecticut, Storrs
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1222
Reference18 articles.
1. A Phantom Paired Element Based Discrete Crack Network (DCN) Toolkit for Residual Strength Prediction of Laminated Composites
2. A discrete crack network toolkit for Abaqus for damage and residual strength prediction of laminated composites
3. Mesh independent modelling of cracks by using higher order shape functions
4. Mesh-independent matrix cracking and delamination modeling in laminated composites
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