Optimal laminated composite shells for buckling and vibration
- 1 March 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (3), 430-437
- https://doi.org/10.2514/3.8090
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Buckling of Shells-Pitfall for DesignersAIAA Journal, 1981
- Optimal design of laminated composite shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
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