The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal Pressure
- 1 August 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (8) , 587-596
- https://doi.org/10.2514/8.3911
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Buckling of Thin-Walled Circular Cylinders Under Axial Compression and Internal PressureJournal of the Aeronautical Sciences, 1957
- Discussion: “Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial Compression” (Donnell, L. H., and Wan, C. C., 1950, ASME J. Appl. Mech., 17, pp. 73–83)Journal of Applied Mechanics, 1950
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950
- 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
- The strength of tubular strutsProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1928