Modified Efficient Global Optimization for a Hat-Stiffened Composite Panel with Buckling Constraint
Author:
Affiliation:
1. Tokyo Institute of Technology, Tokyo 152-8552, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34548
Reference28 articles.
1. Simplified Design Techniques for Laminated Cylindrical Pressure Vessels under Stiffness and Strength Constraints
2. Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
3. Application of Genetic Algorithms to Stiffness Optimization of Laminated Composite Plates with Stress-Concentrated Open Holes
4. Optimal structural damping of skis using a genetic algorithm
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