Buckling of anisotropic laminated cylindrical plates
- 1 November 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (11) , 1641-1645
- https://doi.org/10.2514/3.8830
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Initial buckling of curved panels of generally layered composite materialsComposite Structures, 1983
- Moisture and temperature effects on the instability of cylindrical composite panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- A Refined Theory for Laminated Anisotropic, Cylindrical ShellsJournal of Applied Mechanics, 1974
- Shear Deformation in Heterogeneous Anisotropic PlatesJournal of Applied Mechanics, 1970
- Geometric Design of Composite Cylindrical Characterization SpecimensJournal of Composite Materials, 1970
- On the Theory of Laminated Anisotropic Shells and PlatesJournal of the Aerospace Sciences, 1962