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Numerical simulation of large elastoplastic deformation of shells of revolution in the 'spacesuit' under the influence of pulse overload

机译:在脉冲过载的影响下“SPACESUIT”中旋转壳大型弹塑性变形的数值模拟

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An axisymmetric problem of high strains in a spherical lead shell enclosed into an aluminum 'spacesuit' under the influence of pulse overload is considered. The shell straining is described with the use of equations of mechanics of elastoviscoplastic media in Lagrangian variables. Kinematic relations are determined in the current state metrics. Equations of state are taken in the form of equations of the flow theory with isotropic hardening. Contact interaction of a shell and a 'spacesuit' is modeled by conditions of non-penetration with friction. Numerical solution under the given boundary and initial conditions is based on the moment schema of the finite element method and the explicit time integration scheme of the 'cross'. For sampling the space variables 4-node isoparametric finite elements with multilinear forms features are used. As it was shown by the results of calculations, spherical shell suffers significant local forming, characterized by large displacements and rotation angles of finite elements as a rigid body in the process of loading. The calculation results of the residual form are in good agreement with the experimental data.
机译:考虑了在脉冲过荷的影响下封装在铝'Spaceue'中的球形引线壳中高菌株的轴对称问题。利用拉格朗日变量在拉格朗日变量中的机械结构方程描述了壳体断裂。在当前的国家指标中确定了运动关系。状态的方程是具有各向同性硬化的流动理论的方程的形式。壳体和“SPACESUIT”的接触相互作用是由不穿透摩擦的条件建模的。在给定边界和初始条件下的数值解决方案基于有限元方法的矩模式和“十字”的明确时间集成方案。为了对空间变量进行采样,使用具有多线性表单特征的空间变量4节点等偶像有限元。如所示的计算结果所示,球形壳体遭受显着的局部成形,其特征在于在装载过程中作为刚性体的有限元的大容量和旋转角度。残差形式的计算结果与实验数据吻合良好。

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