Differential Equations for Cylindrical Shells with Arbitrary Temperature Distribution
- 1 September 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (9) , 594-595
- https://doi.org/10.2514/8.7793
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Buckling Stress of Thin Cylindrical Clamped Shells Subject to Hydrostatic PressureJournal of the Aeronautical Sciences, 1954