2008
DOI: 10.1016/j.ijsolstr.2007.07.017
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Elastoplastic bifurcation and collapse of axially loaded cylindrical shells

Abstract: International audienceIn this paper, a shell finite element is designed within the total Lagrangian formulation framework to deal with the plastic buckling and post-buckling of thin structures, such as cylindrical shells. First, the numerical formulation is validated using available analytical results. Then it is shown to be able to provide the bifurcation modes-possibly the secondary ones-and describe the complex advanced post-critical state of a cylinder under axial compression, where the theory is no longer… Show more

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Cited by 20 publications
(12 citation statements)
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“…One particular cylinder geometry has been chosen to be numerically computed in [32] and the numerical initial slope obtained compares very well with the analytical one given by Eq. (85).…”
Section: Simply Supported Edge Solutionmentioning
confidence: 85%
“…One particular cylinder geometry has been chosen to be numerically computed in [32] and the numerical initial slope obtained compares very well with the analytical one given by Eq. (85).…”
Section: Simply Supported Edge Solutionmentioning
confidence: 85%
“…Developed within a total Lagrangian framework, the program encompasses finite plasticity and geometric non-linearities (finite displacements and rotations) in order to deal with the plastic buckling and advanced post-critical behavior of general structures. For the computation of interest, the beam is discretized using a finite rotation shell finite element which is described in full details in Le Grognec and Le van (2008) in the context of cylindrical shells under axial compression.…”
Section: Finite Element Validationmentioning
confidence: 99%
“…Only the middle node at each tip is fixed in the z-direction, which enables a uniform stress state in the beam during the pre-critical deformations. Since the thickness is very thin, the numerical solution of the bending problem can be performed using the shell finite element described in Le Grognec and Le van (2008). One single finite element in the z-direction is used, whereas 50 elements along the length are necessary to correctly represent finite rotations.…”
Section: Finite Element Validationmentioning
confidence: 99%
“…The elastoplastic thin shell finite element formulation is briefly reviewed in the following paragraphs. A more detailed description, which is outside the scope of this paper, may be found in Le Grognec and Le van (2008).…”
Section: Shell Finite Element Formulationmentioning
confidence: 99%