Optimal design of antisymmetric laminated composite plates
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona
2. Purdue University, West Lafayette, Indiana
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45315
Reference5 articles.
1. Some Comments on the Coupling Effects of Angle-Ply Laminates
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Optimum Design of Composite Structures: A Literature Survey (1969–2009);Journal of Reinforced Plastics and Composites;2016-10-01
2. Finite Element Analysis of Wing Design;Proceeding of International Conference on Intelligent Communication, Control and Devices;2016-09-18
3. Lay-up optimization of laminated plates under buckling loads;Buckling and Postbuckling of Composite Plates;1995
4. Optimal design of laminated plates and shells;Composite Structures;1994-01
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