Buckling of orthotropic plates with one free edge
- 1 July 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (7) , 1352-1354
- https://doi.org/10.2514/3.5900
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Minimum-weight analysis of filamentary composite wide columns.Journal of Aircraft, 1968