Buckling of Core-Stabilized Cylinders Under Axisymmetric External Loads
- 1 October 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (10), 1164-1170
- https://doi.org/10.2514/8.9754
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Buckling of a Finite-Length Cylindrical Shell Under a Circumferential Band of PressureJournal of the Aerospace Sciences, 1961