Toward a new snap-through buckling criterion for axially compressed circular cylindrical shells.
- 1 September 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (9) , 1526-1530
- https://doi.org/10.2514/3.3730
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Some properties of the energy loadAIAA Journal, 1965
- An experimental study of the bucking of cylinders under axial compressionExperimental Mechanics, 1964
- POSTBUCKLING BEHAVIOR OF AXIALLY COMPRESSED CIRCULAR CYLINDERSAIAA Journal, 1963
- Lower buckling load in the non-linear buckling theory for thin shellsQuarterly of Applied Mathematics, 1947
- A Theory for the Buckling of Thin ShellsJournal of the Aeronautical Sciences, 1942
- The Buckling of Thin Cylindrical Shells Under Axial CompressionJournal of the Aeronautical Sciences, 1941