Formulation and Numerical Solution of the Stability Loss Problem of Elastic-Plastic Shells of Revolution with an Elastic Filler under Combined Axisymmetric and Torsional Loadings

Q3 Materials Science
В.Г. Баженов, Д. А. Казаков, Александр Иванович Кибец, Елена Владимировна Нагорных, Дарья Анатольевна Самсонова, V. Bazhenov, A. Kibec, Elena V. Nagornykh – CSc, D. Kazakov, E. Nagornykh, D. A. Samsonova
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引用次数: 0

Abstract

A dynamic statement and a method for numerically solving the buckling problems of elastoplastic shells of revolution with filler in axisymmetric and non-axisymmetric shapes under quasi-static and dynamic loading are presented within the framework of two approaches. In the first approach, the problem of elastic-plastic deformation and buckling of shells of revolution with an elastic filler under combined axisymmetric loading with torsion is formulated in a two-dimensional (generalized axisymmetric) formulation based on the hypotheses of the shells theory of the Timoshenko type and the Winkler foundation. The constitutive relations are written in the cylindrical system of Euler coordinates. For each shell element, a local Lagrangian coordinate system is introduced. Kinematic relations are recorded in the current state metric. The distribution of the displacement velocity components over the shell thickness and strain rate tensors in the local basis is written as the sum of the momentless and moment components, which, in turn, are written as the sum of the symmetric and asymmetric parts in the local and in the general basis. The elastoplastic properties of the shell material are taken into account within the framework of the theory of flow with nonlinear isotropic hardening. To take into account non-axisymmetric forms of buckling, the desired functions (both displacements and forces, moments, contact pressure) are expanded into a Fourier series in the circumferential direction. The variational equations of shell motion are derived from the general equation of dynamics. The contact between the shell and the deformable filler is modeled based on the conditions of non-penetration along the normal and free slip along the tangent. The variational equations of shell dynamics for axisymmetric and nonaxisymmetric processes are interconnected through the physical relations of the theory of plasticity. They take into account large axisymmetric shape changes and the instantaneous stress-strain state of the shell. At the initial stage of the nonaxisymmetric buckling process, the deflections are small; therefore, the equations of nonaxisymmetric buckling are obtained as linearized with respect to nonaxisymmetric forms. To initiate nonaxisymmetric buckling modes, initial nonaxisymmetric deflections are introduced. To solve the defining system of equations, a finite-difference method and an explicit time integration scheme of the “cross” type are used. The second approach is based on continuum mechanics hypotheses and implemented in a three-dimensional setting. Both approaches make it possible to simulate the nonlinear subcritical deformation of shells of revolution with an elastic filler, to determine the ultimate (critical) loads in a wide range of loading rates, taking into account geometric shape imperfections, to study the processes of buckling in axisymmetric and non-axisymmetric shapes under dynamic and quasi-static complex loading by tension, compression, torsion, internal and external pressure. The results of numerical simulation are compared with experimental data on the torsion of steel cylindrical elastoplastic shells ( R / h = 1.45) with an elastic filler.
轴对称和扭转复合载荷下带弹性填料的旋转弹塑性壳稳定性损失问题的公式和数值解
在两种方法的框架内,提出了一种数值求解轴对称和非轴对称形状的带填料的弹塑性旋转壳在准静态和动态载荷下的屈曲问题的动力学声明和方法。在第一种方法中,基于Timoshenko型壳理论和Winkler基础的假设,将带有弹性填料的旋转壳在轴对称和扭转组合载荷下的弹塑性变形和屈曲问题公式化为二维(广义轴对称)公式。本构关系是在欧拉坐标的圆柱系统中书写的。对于每个壳单元,引入了一个局部拉格朗日坐标系。运动关系记录在当前状态度量中。位移速度分量在壳体厚度和应变速率张量上的分布在局部基础上被写成无力矩分量和力矩分量的总和,而无力矩分量又被写成对称和非对称部分在局部基础和一般基础上的总和。在非线性各向同性硬化流动理论的框架内,考虑了壳体材料的弹塑性特性。为了考虑非轴对称形式的屈曲,将所需函数(位移和力、力矩、接触压力)扩展为周向上的傅立叶级数。从一般动力学方程出发,导出了壳体运动的变分方程。壳体和可变形填料之间的接触是基于沿法线的未穿透和沿切线的自由滑动的条件来建模的。轴对称和非轴对称过程的壳动力学变分方程通过塑性理论的物理关系相互联系。它们考虑了大的轴对称形状变化和壳体的瞬时应力-应变状态。在非轴对称屈曲过程的初始阶段,挠度较小;因此,得到了关于非轴对称形式的线性化的非轴对称屈曲方程。为了启动非轴对称屈曲模式,引入了初始非轴对称挠度。为了求解定义方程组,使用了有限差分法和“交叉”型显式时间积分格式。第二种方法基于连续体力学假设,并在三维环境中实现。这两种方法都可以模拟带有弹性填料的旋转壳体的非线性亚临界变形,在考虑几何形状缺陷的情况下,确定宽加载速率范围内的极限(临界)载荷,研究轴对称和非轴对称形状在动态和准静态张力复合载荷下的屈曲过程,压缩、扭转、内部和外部压力。将数值模拟结果与含弹性填料的弹塑性钢圆柱壳(R/h=1.45)的扭转试验数据进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
PNRPU Mechanics Bulletin
PNRPU Mechanics Bulletin Materials Science-Materials Science (miscellaneous)
CiteScore
1.10
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