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A computationally efficient method for the limit elasto plastic analysis of space frames

机译:一种计算高效的空间框架极限弹性塑性分析方法

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摘要

A computationally efficient method for the first order step-by-step limit analysis of space frames is presented. The incremental non-holonomic analysis is based on the generalized plastic node method. The non-linear yield surface is approximated by a multi-faceted surface, thus avoiding the iterative formulation at each load step. In order to prevent the occurrence of very small load steps a second internal and homothetic to the initial yield surface is implemented which creates a plastic zone for the activation of the plastic modes. This implementation reduces substantially the computational effort of the procedure without affecting the value of the final load. The solution of the linear equilibrium equation at each load step is obtained with the preconditioned conjugate gradient method. Special attention is paid to the fact that the overall stiffness matrix changes gradually with the successive formation of plastic nodes. The application of the conjugate gradient method is based on some recent developments on improved matrix handling techniques and efficient preconditioning strategies. A number of test problems have been performed which show the usefulness of the proposed approach and its superiority in respect to efficient direct methods of solution in both storage requirements and computing time.
机译:该文提出了一种计算效率高的空间帧一阶阶步进极限分析方法。增量非完整分析基于广义塑性节点方法。非线性屈服面由多面曲面近似,从而避免了每个载荷步骤的迭代公式。为了防止发生非常小的载荷阶跃,在初始屈服面上实现了第二个内部同质化,从而为塑性模态的激活创造了一个塑性区。这种实现大大减少了过程的计算工作量,而不会影响最终载荷的值。采用预条件共轭梯度法得到各载荷阶跃的线性平衡方程的解。特别需要注意的是,整体刚度矩阵随着塑性节点的连续形成而逐渐变化。共轭梯度法的应用基于改进的基质处理技术和高效预处理策略的最新发展。已经进行了许多测试问题,这些测试问题表明了所提方法的实用性及其在存储需求和计算时间方面相对于高效直接求解方法的优越性。

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