Postbuckling and Growth of Delaminations in Composite Plates Subjected to Axial Compression
Author:
Affiliation:
1. NASA Langley Research Center
2. Swales Aerospace
3. Eagle Aeronautics
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1746
Reference23 articles.
1. Computational Structural Analysis and Testing: An Approach to Understand Delamination Growth
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