Single-Stringer Compression Specimen for the Assessment of Damage Tolerance of Postbuckled Structures
Author:
Affiliation:
1. Politecnico di Milano, 20156 Milano, Italy
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031106
Reference23 articles.
1. Progressive damage modeling in fiber-reinforced materials
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5. A damage model for the simulation of delamination in advanced composites under variable-mode loading
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