Optimization of Long Anisotropic Laminated Fiber Composite Panels with T-Shaped Stiffeners
Author:
Affiliation:
1. University of Bristol, Bristol, England, BS8 1TR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.26321
Reference46 articles.
1. Optimum laminate design for strength and stiffness
2. Optimum design of laminated fibre composite plates
3. Analysis of Anisotropic Plates
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