Buckling of composite cylindrical shells under pure bending.
- 1 February 1968
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (2) , 349-354
- https://doi.org/10.2514/3.4501
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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- Stability of stiffened cylinders.AIAA Journal, 1965
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- STABILITY OF HETEROGENEOUS AEOLOTROPIC CYLINDRICAL SHELLS UNDER COMBINED LOADINGAIAA Journal, 1963
- On the Theory of Laminated Anisotropic Shells and PlatesJournal of the Aerospace Sciences, 1962
- Effects of Internal Pressure on the Buckling of Circular-Cylindrical Shells Under BendingJournal of the Aerospace Sciences, 1962
- Elastic Stability of Orthotropic ShellsJournal of the Aerospace Sciences, 1962
- Bending and Stretching of Certain Types of Heterogeneous Aeolotropic Elastic PlatesJournal of Applied Mechanics, 1961
- On the Buckling of Circular Cylindrical Shells Under Pure BendingJournal of Applied Mechanics, 1961
- Stability of Orthotropic Cylindrical Shells Under Combined LoadingARS Journal, 1961