Symmetric and nonsymmetric buckling of finitely deformed eccentrically stiffened shells of revolution.
- 1 August 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (8) , 1455-1462
- https://doi.org/10.2514/3.4219
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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- Influence of stiffener eccentricity and end moment on stability of cylinders in compression.AIAA Journal, 1966
- Vibration and buckling of pressurized torus shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Asymmetric buckling of finitely deformed conical shellsAIAA Journal, 1965
- General instability and optimum design of grid- stiffened spherical domesAIAA Journal, 1965
- 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
- Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells under Hydrostatic PressureJournal of Mechanical Engineering Science, 1963
- On axisymmetrical deformations of thin shells of revolutionPublished by American Mathematical Society (AMS) ,1950