Buckling of Curved Sheet in Compression and Its Relation to the Secant Modulus
- 1 January 1948
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 15 (1) , 18-22
- https://doi.org/10.2514/8.11492
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Secant Modulus Method for Determining Plate Instability Above the Proportional LimitJournal of the Aeronautical Sciences, 1946