Buckling and vibration of laminated composite plates using various plate theories
- 1 December 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (12), 1808-1817
- https://doi.org/10.2514/3.10338
Abstract
No abstract availableThis publication has 28 references indexed in Scilit:
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