This paper describes a systematic numerical investigation into the nonlinear elastic behavior of conical shells, with various types of initial imperfections, subject to a uniformly distributed axial compression. Three different patterns of imperfections, including first axisymmetric linear bifurcation mode, first non-axisymmetric linear bifurcation mode, and weld depression are studied using geometrically nonlinear (mite element analysis. Effects of each imperfection shape and tapering angle on imperfection sensitivity curves are investigated and the lower bound curve is determined. Finally, an empirical lower bound relation is proposed for hand calculation in the buckling design of conical shells
Small geometric imperfections in thin-walled shell structures can cause large reductions in buckling...
AbstractStability of imperfect elastic cylindrical shells which are subjected to uniform axial compr...
In most shell buckling codes, guidance on the design of conical shells is restricted to unstiffened ...
In thin-walled shells of revolution with widely-spaced meridional stiffeners loaded in compression, ...
Since the development of the first theories to predict the buckling induced by axial compression in ...
AbstractStability of imperfect elastic cylindrical shells which are subjected to uniform axial compr...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
This paper aims to provide experimental results into the buckling behavior of cones having single di...
Since the development of the first theories to predict the buckling induced by axial compression in...
Since the development of the first theories to predict the buckling induced by axial compression in...
Since the development of the first theories to predict the buckling induced by axial compression in...
Shell structures have been widely used in engineering applications such as pipelines, aerospace, mar...
AbstractThe effect of pre-buckling nonlinearity on the bifurcation point of a conical shell is exami...
Small geometric imperfections in thin-walled shell structures can cause large reductions in buckling...
AbstractStability of imperfect elastic cylindrical shells which are subjected to uniform axial compr...
In most shell buckling codes, guidance on the design of conical shells is restricted to unstiffened ...
In thin-walled shells of revolution with widely-spaced meridional stiffeners loaded in compression, ...
Since the development of the first theories to predict the buckling induced by axial compression in ...
AbstractStability of imperfect elastic cylindrical shells which are subjected to uniform axial compr...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
Buckling is a critical failure phenomenon for structures, and represents a threat for thin shells su...
This paper aims to provide experimental results into the buckling behavior of cones having single di...
Since the development of the first theories to predict the buckling induced by axial compression in...
Since the development of the first theories to predict the buckling induced by axial compression in...
Since the development of the first theories to predict the buckling induced by axial compression in...
Shell structures have been widely used in engineering applications such as pipelines, aerospace, mar...
AbstractThe effect of pre-buckling nonlinearity on the bifurcation point of a conical shell is exami...
Small geometric imperfections in thin-walled shell structures can cause large reductions in buckling...
AbstractStability of imperfect elastic cylindrical shells which are subjected to uniform axial compr...
In most shell buckling codes, guidance on the design of conical shells is restricted to unstiffened ...