Stacking-sequence optimization for buckling of laminated plates by integer programming
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
2. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10989
Reference16 articles.
1. Optimization of Buckling and Yield Strengths of Laminated Composites
2. Optimum design of laminated fibre composite plates
3. Optimum Design of Laminated Plates under Axial Compression
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