Stability analysis of shells of revolution by the finite-element method.
- 1 February 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (2), 355-361
- https://doi.org/10.2514/3.4502
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
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- Direct stiffness method analysis of shells of revolution utilizing curved elements.AIAA Journal, 1966
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