Delamination in cross-ply laminated composite subjected to low-velocity impact
Author:
Affiliation:
1. Boeing Commercial Airplane Group, Seattle, Washington 98124
2. University of Washington, Seattle, Washington 98122
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11800
Reference12 articles.
1. Initiation and extent of impact damage in graphite/epoxy and graphite/PEEK composites
2. Modelling of impact damage in composite laminates
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