Continuum-based stiffened composite shell element for geometrically nonlinear analysis
- 1 January 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (1) , 95-101
- https://doi.org/10.2514/3.10099
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
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