POSTBUCKLING BEHAVIOR OF AXIALLY COMPRESSED CIRCULAR CYLINDERS
- 1 March 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (3) , 630-633
- https://doi.org/10.2514/3.1606
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Postbuckling Behavior of Axially Compressed Circular Cylindrical ShellsJournal of the Aeronautical Sciences, 1954
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950
- The Behavior of Thin Cylindrical Shells After Buckling Under Axial CompressionJournal of the Aeronautical Sciences, 1948
- The Buckling of Thin Cylindrical Shells Under Axial CompressionJournal of the Aeronautical Sciences, 1941
- A New Theory for the Buckling of Thin Cylinders Under Axial Compression and BendingTransactions of the American Society of Mechanical Engineers, 1934