Postbuckling equilibrium of axially compressed circular cylindrical shells.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (1), 126-133
- https://doi.org/10.2514/3.3395
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- The buckling of a free edge of an axially-compressed circular cylindrical shellQuarterly of Applied Mathematics, 1962
- Postbuckling Behavior of Axially Compressed Circular Cylindrical ShellsJournal of the Aeronautical Sciences, 1954
- 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
- Die Stabilität der KreiszylinderschaleArchive of Applied Mechanics, 1932