Effective Width of Elastically Supported Flat Plates
- 1 October 1946
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 13 (10), 518-524
- https://doi.org/10.2514/8.11441
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Secant Modulus Method for Determining Plate Instability Above the Proportional LimitJournal of the Aeronautical Sciences, 1946
- The Compressive Strength of Thin Aluminum Alloy Sheet in the Plastic RegionJournal of the Aeronautical Sciences, 1941
- Effect of Rivet Spacing on Stiffened Thin Sheet Under CompressionJournal of the Aeronautical Sciences, 1936