Progressive failure studies of composite panels with and without cutouts
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. ICASE/NASA, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1182
Reference23 articles.
1. A thermomechanical constitutive theory for elastic composites with distributed damage—I. Theoretical development
2. A Progressive Damage Model for Laminated Composites Containing Stress Concentrations
3. Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: Part I—Analysis
4. Analytical Prediction of Damage Growth in Notched Composite Panels Loaded in Compression
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