Minimum Weight of Stiffened Cylindrical Shells in Pure Bending
- 1 April 1950
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 17 (4) , 211-216
- https://doi.org/10.2514/8.1594
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Simplified Analysis of General Instability of Stiffened Shells in Pure BendingJournal of the Aeronautical Sciences, 1949
- Principles of Structural Design for Minimum WeightJournal of the Aeronautical Sciences, 1949