Simplified Analysis of General Instability of Stiffened Shells in Pure Bending
- 1 October 1949
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 16 (10) , 590-592
- https://doi.org/10.2514/8.11864
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Principles of Structural Design for Minimum WeightJournal of the Aeronautical Sciences, 1949