Buckling of cylindrical and conical sandwich shells with orthotropicfacings.
- 1 February 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (2), 250-257
- https://doi.org/10.2514/3.5082
Abstract
No abstract availableThis publication has 17 references indexed in Scilit:
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- Instability of orthotropic cylindrical shells under combined torsionand hydrostatic pressure.AIAA Journal, 1967
- Axially symmetric wave propagation in a two-layered cylinderInternational Journal of Solids and Structures, 1967
- Combination torsion and axial compression tests of conical shells.AIAA Journal, 1967
- Axially Symmetric Motions of a Two-Layered Timoshenko-Type Cylindrical ShellJournal of Applied Mechanics, 1966
- Structural efficiency of orthotropic cylindrical shells subjected toaxial compression.AIAA Journal, 1966
- Influence of edge conditions on the stability of axially compressed cylindrical shells.AIAA Journal, 1966
- Postbuckling equilibrium of axially compressed circular cylindrical shells.AIAA Journal, 1966
- Stability of circumferentially corrugated sandwich cylinders under combined loadsAIAA Journal, 1964
- On the Buckling of Truncated Conical Shells in TorsionJournal of Applied Mechanics, 1962