The Crippling Strength of Compression Elements
- 1 January 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (1) , 37-52
- https://doi.org/10.2514/8.7482
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Buckling Efficiencies of Plate Materials at Elevated TemperaturesJournal of the Aeronautical Sciences, 1955
- The Ultimate Strength of Aluminum-Alloy Formed Structural Shapes in CompressionJournal of the Aeronautical Sciences, 1954
- Instability of Extrusions Under Compressive LoadsJournal of the Aeronautical Sciences, 1945
- Predicting Stiffener and Stiffened Panel Crippling StressesJournal of the Aeronautical Sciences, 1942