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On large deformations of thin elasto-plastic shells: Implementation of a finite rotation model for quadrilateral shell element

机译:关于弹塑性薄壳的大变形:四边形壳单元有限旋转模型的实现

摘要

A large-deformation model for thin shells composed of elasto-plastic material is presented in this work, Formulation of the shell model, equivalent to the two-dimensional Cosserat continuum, is developed from the three-dimensional continuum by employing standard assumptions on the distribution of the displacement held in the shell body, A model for thin shells is obtained by an approximation of terms describing the shell geometry. Finite rotations of the director field are described by a rotation vector formulation. An elasto-plastic constitutive model is developed based on the von Mises yield criterion and isotropic hardening. In this work, attention is restricted to problems where strains remain small allowing for all aspects of material identification and associated computational treatment, developed for small-strain elastoplastic models, to be transferred easily to the present elasto-plastic thin-shell model. A finite element formulation is based on the four-noded isoparametric element. A particular attention is devoted to the consistent linearization of the shell kinematics and elasto-plastic material model, in order to achieve quadratic rate of asymptotic convergence typical for the Newton-Raphson-based solution procedures. To illustrate the main objective of the present approach-namely the simulation of failures of thin elastoplastic shells typically associated with buckling-type instabilities and/or bending-dominated shell problems resulting in formation of plastic hinges-several numerical examples are presented, Numerical results are compared with the available experimental results and representative numerical simulations.
机译:提出了一种由弹塑性材料构成的薄壳大变形模型,通过对分布进行标准假设,从三维连续体发展了等效于二维Cosserat连续体的壳模型公式。在保留壳体内位移的基础上,通过描述壳几何形状的项的近似值获得了薄壳模型。方向矢场的有限旋转由旋转矢量公式描述。基于冯·米塞斯屈服准则和各向同性硬化,建立了弹塑性本构模型。在这项工作中,注意力集中在应变保持较小的问题上,这些问题使得为小应变弹塑性模型开发的材料识别和相关计算处理的各个方面都可以轻松地转移到当前的弹塑性薄壳模型中。有限元公式基于四节点等参元素。为了实现基于牛顿-拉夫森的求解程序典型的渐近收敛的二次速率,需要特别注意壳运动学和弹塑性材料模型的一致线性化。为了说明本方法的主要目的,即模拟薄弹塑性壳体的破坏,该破坏通常与导致塑性铰链形成的屈曲型不稳定性和/或弯曲为主的壳问题有关,给出了几个数值示例,数值结果如下:与可用的实验结果和代表性的数值模拟进行比较。

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