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

机译:一种计算有效的空间框架极限弹塑性分析方法

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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:提出了一种对空间框架进行一阶逐步极限分析的有效计算方法。增量非完整分析基于广义塑性节点法。非线性屈服面由多面曲面近似,因此避免了每个荷载步骤的迭代公式。为了防止出现很小的载荷阶跃,实现了第二内部且与初始屈服面相似的第二步,该第二屈服面形成了用于激活塑性模的塑性区。该实施方式在不影响最终负载的值的情况下大大减少了该过程的计算量。用预处理的共轭梯度法获得每个载荷阶跃的线性平衡方程的解。特别要注意的是,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矩阵处理技术和有效的预处理策略的一些最新进展。已经进行了许多测试问题,这些问题表明了所提出方法的有效性及其相对于存储需求和计算时间方面有效的直接解决方案的优越性。

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