Static buckling of moderately thick, anisotropic, laminated and sandwich cylindrical shell panels
- 1 October 1990
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (10), 1782-1793
- https://doi.org/10.2514/3.10474
Abstract
No abstract availableThis publication has 40 references indexed in Scilit:
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