Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11710
Reference11 articles.
1. Optimum design of laminated fibre composite plates
2. OPTIMIZATION OF STIFFENED LAMINATED COMPOSITE PLATES WITH FREQUENCY CONSTRAINTS
3. Stacking-sequence optimization for buckling of laminated plates by integer programming
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