A Phantom Paired Element Based Discrete Crack Network (DCN) Toolkit for Residual Strength Prediction of Laminated Composites
Author:
Affiliation:
1. Global Engineering and Materials, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1579
Reference20 articles.
1. Internal State Variable Approach for Predicting Stiffness Reductions in Fibrous Laminated Composites with Matrix Cracks
2. A Progressive Failure Model for Composite Laminates Containing Openings
3. An Accumulative Damage Model for Tensile and Shear Failures of Laminated Composite Plates
4. Three-Dimensional Modeling of Damage in Laminated Composites Containing a Central Hole
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