On the stability of eccentrically stiffened cylindrical shells under axial compression
- 1 July 1967
- journal article
- Published by Elsevier in International Journal of Solids and Structures
- Vol. 3 (4), 445-470
- https://doi.org/10.1016/0020-7683(67)90001-7
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Inversion of the Eccentricity Effect in Stiffened Cylindrical Shells Buckling under External PressureJournal of Mechanical Engineering Science, 1966
- General instability of orthotropically stiffened cylinders under axial compression.AIAA Journal, 1966
- EXPERIMENTAL AND THEORETICAL STUDIES ON BUCKLING OF CONICAL AND CYLINDRICAL SHELLS UNDER COMBINED LOADINGPublished by Defense Technical Information Center (DTIC) ,1966
- Influence of edge conditions on the stability of axially compressed cylindrical shells.AIAA Journal, 1966
- Stability of stiffened cylinders.AIAA Journal, 1965
- Low Buckling Stresses of Axially Compressed Circular Cylindrical Shells of Finite LengthJournal of Applied Mechanics, 1965
- Buckling of circular cylindrical shells in axial compressionInternational Journal of Mechanical Sciences, 1965
- General Instability of Stiffened Circular Conical Shells under Hydrostatic PressureAeronautical Quarterly, 1965
- Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells under Hydrostatic PressureJournal of Mechanical Engineering Science, 1963
- Design of a Pressurized Missile BodyAircraft Engineering and Aerospace Technology, 1960