Allowable Compressive Stresses in Aircraft Structures
- 1 October 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (10) , 657-664
- https://doi.org/10.2514/8.2073
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Effective Width of Elastically Supported Flat PlatesJournal of the Aeronautical Sciences, 1946
- Nondimensional Buckling Curves-Their Development and ApplicationJournal of the Aeronautical Sciences, 1946
- The Buckling of Sandwich-Type PanelsJournal of the Aeronautical Sciences, 1945