Instability of Composite Panels
- 1 September 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (9) , 739-743
- https://doi.org/10.2514/3.57555
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Buckling of cylindrical panels under axial compressionComputers & Structures, 1976
- Edge restraint effect on buckling of compressed curved panels.AIAA Journal, 1968