The Optimum Proportions of a Long Unstiffened Circular Cylinder in Pure Bending
- 1 October 1948
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 15 (10) , 616-624
- https://doi.org/10.2514/8.11667
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Buckling of Curved Sheet in Compression and Its Relation to the Secant ModulusJournal of the Aeronautical Sciences, 1948
- Secant Modulus Method for Determining Plate Instability Above the Proportional LimitJournal of the Aeronautical Sciences, 1946