Impact response of graphite/epoxy cylindrical panels
- 1 July 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (7), 1827-1832
- https://doi.org/10.2514/3.11143
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
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- Large displacement and rotational formulation for laminated shells including parabolic transverse shearInternational Journal of Non-Linear Mechanics, 1990
- Exact Solutions of Moderately Thick Laminated ShellsJournal of Engineering Mechanics, 1984
- Transient response of bonded strain gagesExperimental Mechanics, 1966