Effect of a circular hole on the buckling of cylindrical shells loaded by axial compression.
- 1 November 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (11), 1466-1472
- https://doi.org/10.2514/3.6644
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Buckling of cylinders with cutoutsAIAA Journal, 1970
- The Effect of General Imperfections on the Buckling of Cylindrical ShellsJournal of Applied Mechanics, 1969
- Stresses about a circular hole in a cylindrical shellAIAA Journal, 1965