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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 79
PROCEEDINGS OF THE SEVENTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by: B.H.V. Topping and C.A. Mota Soares
Paper 124
Stability of the FE Computation of Softening Plasticity using an Overlay Model V. Dias da Silva
Department of Civil Engineering, University of Coimbra, Portugal V. Dias da Silva, "Stability of the FE Computation of Softening Plasticity using an Overlay Model", in B.H.V. Topping, C.A. Mota Soares, (Editors), "Proceedings of the Seventh International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 124, 2004. doi:10.4203/ccp.79.124
Keywords: numerical stability, softening, visco-plasticity, elasto-plasticity, visco-elasticity, regularization, overlay model, Duvaut-Lions, Maxwell.
Summary
The visco-plastic models of Duvaut-Lions and Perzyna are often used to
introduce viscosity in inviscid elasto-plastic material laws with
softening, in order to reduce the mesh-dependency of Finite Element
solutions. The first of these models has the limitation that it must be
used in conjunction with an integration algorithm for the inviscid
elasto-plastic rate equations, in which the initial stress is used only
to compute the trial stress, since it may be outside the yield surface.
Usually a backward Euler interpolation is used. Furthermore, an
evolution rule must be postulated for the yield surface, in case of
hardening/softening plasticity. The second one -the Perzyna model- may
not converge to the inviscid solution, when the viscosity goes to zero,
in the case of multi-surface yield locus.
Another possibility to solve the same problem consists of using an overlay model, in which the inviscid elasto-plastic model deforms in parallel with a Maxwell-type visco-elastic element. This alternative is specially attractive in the context of displacement-based finite elements, since in this case the problem is strain-driven and, as a consequence, the visco-elastic and the elasto-plastic parts of the material response may be computed separately. This approach has been developed and used by the author [1] and does not suffer the above referred limitations of the models of Duvaut-Lions and Perzyna. In the computation of the material response, different integration techniques are used for the visco-elastic and for inviscid elasto-plastic elements. However, both are numerically robust: an unconditionally stable and oscillation-free mid-point indirect interpolation scheme for the visco-elastic element and a linear backward Euler approach for the elasto-plastic element. Although the latter model element displays also unconditional numerical stability, when used in hardening plasticity, in the softening case numerical difficulties arise, as a consequence of the strain localization. After an outline of the main features of the overlay model, the constitutive law of the visco-elastic Maxwell element, as well as the numerical integration technique used in the one-dimensional case, are described. The analysis of the numerical stability is subsequently performed on the special case of softening elasto-plasticity. To this end, the deformation of a chain of overlay elements under constant elongation rate is computed. By a trial and error procedure the way as the stability limit varies with the main material parameters is investigated. a similar study is also carried out for the case of the Duvaut-Lions model. The main conclusion, in the case of the overlay model, is that the mesh refinement does not influence the stability limit. This conclusion is then tested in a three-dimensional problem: the simulation of the process of formation of a shear band in a von Mises specimen. It is verified that, also in this case, the maximum time step for numerical stability does not suffer reduction with the mesh refinement. References
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