Computer analysis of various shells of revolution
- 22 January 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Nonlinear axisymmetric behavior of shells of revolution.AIAA Journal, 1967
- Computer analysis of asymmetric buckling of ring-stiffened orthotropic shells of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Buckling of axially compressed cylindrical shells with ring-stiffened edges.AIAA Journal, 1966
- A survey of some buckling problems.AIAA Journal, 1966
- 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
- Stiffness and buckling in filament-wound motorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- On the Stability Problem for Shallow Spherical ShellsJournal of Mathematics and Physics, 1959