Inversion of the Eccentricity Effect in Stiffened Cylindrical Shells Buckling under External Pressure
- 1 December 1966
- journal article
- Published by SAGE Publications in Journal of Mechanical Engineering Science
- Vol. 8 (4), 363-373
- https://doi.org/10.1243/jmes_jour_1966_008_048_02
Abstract
The analysis of the general instability of stiffened cylindrical shells under hydrostatic pressure carried out earlier is continued in order to study the inversion of the eccentricity effect: 500 typical shells of varying geometries are considered. The results show that for lateral pressure loading the inversion of the eccentricity effect is practically independent of the geometry of the rings but depends very strongly on the shell geometry parameter Z, whereas for hydrostatic pressure the inversion is also influenced by the bending stiffness of the rings. A range of inversion is found for both loadings. A detailed physical explanation of the cause of the eccentricity effect and its inversion is proposed.Keywords
This publication has 7 references indexed in Scilit:
- Influence of stiffener eccentricity and end moment on stability of cylinders in compression.AIAA Journal, 1966
- FURTHER REMARKS ON THE EFFECT OF ECCENTRICITY OF STIFFENERS ON THE GENERAL INSTABILITY OF STIFFENED CYLINDRICAL SHELLSPublished by Defense Technical Information Center (DTIC) ,1965
- Effects of asymmetric stiffening on buckling of shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Static and dynamic effects on eccentric stiffening of plates and cylindrical shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,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