The Effects of Geometric and Loading Imperfections on the Response and Lower-Bound Buckling Load of a Compression-Loaded Cylindrical Shell
Authors:
- Benedikt KriegesmannBKBenedikt Kriegesmann
- Mark HilburgerMHMark Hilburger
- Raimund RolfesRRRaimund Rolfes
- 23 April 2012
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Investigations on imperfection sensitivity and deduction of improved knock-down factors for unstiffened CFRP cylindrical shellsComposite Structures, 2010
- Robust design of composite cylindrical shells under axial compression — Simulation and validationThin-Walled Structures, 2008
- Effects of imperfections on the buckling response of compression-loaded composite shellsInternational Journal of Non-Linear Mechanics, 2002