Elastic stability of thin-walled cylindrical and conical shells under combined internal pressure and axial compression
- 1 June 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (6) , 1118-1125
- https://doi.org/10.2514/3.3064
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal PressureJournal of the Aeronautical Sciences, 1957
- Buckling of Thin-Walled Circular Cylinders Under Axial Compression and Internal PressureJournal of the Aeronautical Sciences, 1957
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950