Finite Element Method for Nonlinear Free Vibrations of Composite Plates
- 1 January 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 35 (1), 159-166
- https://doi.org/10.2514/2.78
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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