Minimum-weight stiffened shells with slight meridional curvature designed to support axial compressive loads.
- 1 August 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (8), 1599-1601
- https://doi.org/10.2514/3.5438
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Some recent advances in the investigation of shell buckling.AIAA Journal, 1968
- Computer analysis of various shells of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968