Stress analysis of a rectangular implant in laminated composites using 2-D and 3-D finite elements
Author:
Affiliation:
1. MIT, Cambridge, MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2477
Reference3 articles.
1. Exact Solutions for Composite Laminates in Cylindrical Bending
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