Computer analysis of various shells of revolution.
- 1 October 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (10) , 1848-1855
- https://doi.org/10.2514/3.4891
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Symmetric and nonsymmetric buckling of finitely deformed eccentrically stiffened shells of revolution.AIAA Journal, 1967
- Nonlinear axisymmetric behavior of shells of revolution.AIAA Journal, 1967
- Stability of toroidal shells under uniform external pressure.AIAA Journal, 1967
- Computer analysis of asymmetric buckling of ring-stiffened orthotropic shells of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Influence of stiffener eccentricity and end moment on stability of cylinders in compression.AIAA Journal, 1966
- Influence of edge conditions on the stability of axially compressed cylindrical shells.AIAA Journal, 1966
- Unsymmetrical Buckling of Thin Shallow Spherical ShellsJournal of Applied Mechanics, 1964
- Effects of boundary conditions on the stability of cylinders subject to lateral and axial pressuresAIAA Journal, 1964
- BUCKLING OF A TRUNCATED HEMISPHERE UNDER AXIAL TENSIONAIAA Journal, 1963
- On the Stability Problem for Shallow Spherical ShellsJournal of Mathematics and Physics, 1959