Transient response of graphite/epoxy and Kevlar/epoxy laminates subjected to impact
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (11) , 1590-1596
- https://doi.org/10.2514/3.10306
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Thick Composite Plates Subjected to Lateral LoadingJournal of Applied Mechanics, 1987
- On the Impact of Initially Stressed Composite LaminatesJournal of Composite Materials, 1985
- Use of Statical Indentation Laws in the Impact Analysis of Laminated Composite PlatesJournal of Applied Mechanics, 1985
- Vibration of Cantilevered Graphite/Epoxy Plates With Bending-Torsion CouplingJournal of Reinforced Plastics and Composites, 1982
- Shear Deformation in Heterogeneous Anisotropic PlatesJournal of Applied Mechanics, 1970
- On the Solution of Plates of Composite MaterialsJournal of Composite Materials, 1969
- Influence of Rotatory Inertia and Shear on Flexural Motions of Isotropic, Elastic PlatesJournal of Applied Mechanics, 1951