POSTBUCKLING BEHAVIOR OF PRESSURE- OR CORE-STABILIZED CYLINDERS UNDER AXIAL COMPRESSION
- 1 October 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (10) , 2338-2341
- https://doi.org/10.2514/3.2063
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- POSTBUCKLING BEHAVIOR OF AXIALLY COMPRESSED CIRCULAR CYLINDERSAIAA Journal, 1963
- The Stability Under Axial Compression and Lateral Pressure of Circular-Cylindrical Shells With a Soft Elastic CoreJournal of the Aerospace Sciences, 1962
- 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
- Postbuckling Behavior of Axially Compressed Circular Cylindrical ShellsJournal of the Aeronautical Sciences, 1954