Behavior of Composite Shells Under Transverse Impact and Quasi-Static Loading
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.481
Reference32 articles.
1. Impact damage in small diameter graphite/epoxy composite struts
2. Impact on Laminated Composites: Recent Advances
3. Impact on Laminated Composite Materials
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