Postbuckling behavior of geometrically imperfect composite cylindrical shells under axial compression
- 1 March 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (3) , 579-581
- https://doi.org/10.2514/3.5715
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Buckling and postbuckling behavior of composite cylindrical shells under axial compressionAIAA Journal, 1970
- Transient Stresses at a Clamped Support of a Circular Cylindrical ShellJournal of Applied Mechanics, 1969
- Vibrations of orthotropic cylindrical sandwich shells under initial stress.AIAA Journal, 1966
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950