Secant Modulus Method for Determining Plate Instability Above the Proportional Limit
- 1 January 1946
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 13 (1) , 38-44
- https://doi.org/10.2514/8.11303
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Buckling of Aluminum-Alloy Columns and PlatesJournal of the Aeronautical Sciences, 1943