Lamination Parameter Interpolation Method for Design of Manufacturable Variable-Stiffness Composite Panels
Author:
Affiliation:
1. Koc University, 34450 Istanbul, Turkey
Funder
FP7 People: Marie-Curie Actions
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057902
Reference32 articles.
1. Optimal design of a composite-material plate to maximize its fundamental frequency
2. Layerwise optimization for the maximum fundamental frequency of laminated composite plates
3. Layer optimisation for maximum fundamental frequency of laminated composite plates for different edge conditions
4. Maximizing the fundamental frequency of laminated cylindrical panels using layerwise optimization
5. Global optimization of laminated cylindrical panels based on fundamental natural frequency
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