The Ultimate Strength of Aluminum-Alloy Formed Structural Shapes in Compression
- 1 April 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (4) , 217-229
- https://doi.org/10.2514/8.2985
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Inelastic Column TheoryJournal of the Aeronautical Sciences, 1947
- Predicting Stiffener and Stiffened Panel Crippling StressesJournal of the Aeronautical Sciences, 1942