Stability of circumferentially corrugated sandwich cylinders under combined loads
- 1 December 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (12) , 2142-2149
- https://doi.org/10.2514/3.2756
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Stability of Flat, Simply Supported Corrugated-Core Sandwich Plates Under Combined LoadsJournal of the Aerospace Sciences, 1960