A High Fidelity Composite Bonded Joint Analysis Validation Study - Part I: Analysis
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company
2. The Boeing Company
3. Bell Helicopter
4. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2166
Reference14 articles.
1. Development of p-Version handbook solutions for analysis of composite bonded joints
2. First-order zig-zag sublaminate plate theory and finite element model for laminated composite and sandwich panels
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