Buckling of axially compressed, core-filled cylinders with transverse shear flexibility
- 1 May 1971
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (5) , 546-548
- https://doi.org/10.2514/3.30308
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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- BUCKLING OF A COMPOSITE ORTHOTROPIC CYLINDER CONTAINING AN ELASTIC FOUNDATIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- The Stability Under Axial Compression and Lateral Pressure of Circular-Cylindrical Shells With a Soft Elastic CoreJournal of the Aerospace Sciences, 1962
- Buckling of Axially Compressed Long Cylindrical Shell With Elastic CoreJournal of Applied Mechanics, 1962
- Elastic Buckling of Cylindrical Thin Shells Filled With an Elastic CoreARS Journal, 1962