Postbuckling compressive strength of graphite/epoxy laminated cylindrical panels loaded in compression
- 1 February 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (2), 217-222
- https://doi.org/10.2514/3.12428
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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