Analysis of Delamination Initiation in Postbuckled Dropped-Ply Laminates
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49019
Reference15 articles.
1. Tensile strength of tapered composite structures
2. Effect of dropped plies on the strength of graphite-epoxy laminates
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