Postbuckling behavior of anisotropic laminated plates under pure shear and shear combined with compressive loading
- 1 February 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (2) , 281-286
- https://doi.org/10.2514/3.8380
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Initial buckling of curved panels of generally layered composite materialsComposite Structures, 1983
- Postbuckling behaviour of curved panels of generally layered composite materialsComposite Structures, 1983
- Diagonal Tension Behavior of Boron-Epoxy Shear PanelsJournal of Composite Materials, 1971