Four Point Bending of Thin Unidirectional Composite Laminas
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of New Mexico, Albuquerque
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1668
Reference17 articles.
1. Nonlinear stress-strain behavior of graphite/epoxy laminates
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