Stability of Flat, Simply Supported Corrugated-Core Sandwich Plates Under Combined Loads
- 1 July 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (7) , 525-534
- https://doi.org/10.2514/8.8622
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- The Buckling and Bending of Orthotopic Sandwich Panels With All Edges Simply-SupportedAeronautical Quarterly, 1955
- Analysis of the Elastic and Plastic Stability of Sandwich Plates by the Method of Split Rigidities-IJournal of the Aeronautical Sciences, 1951