Nonlinear response of cylindrical shells subjected to dynamic axial loads
- 1 October 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (10) , 1788-1794
- https://doi.org/10.2514/3.2666
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950
- 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