Critical Buckling Stresses of Simply Supported Flat Rectangular Plates Under Combined Longitudinal Compression, Transverse Compression, and Shear
- 1 June 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (6) , 411-416
- https://doi.org/10.2514/8.3052
Abstract
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