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A Triangular Finite Element for the Study of the Post-Critical Behaviour of Shells

机译:弹壳临界行为研究的三角有限元

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The numerical solution of the limit analysis problem has experienced a growing interestrnin recent years. Methods developed in this context can be employed also to obtainrnindications on the structural response subsequent to collapse, which is required in severalrnsituations, such as for shells employed as shock absorbers or energy dissipators.rnThe procedure is known as sequential limit analysis and, as its name suggests, is basedrnon a sequence of limit analysis solutions referring to progressively updated conu0002gurations.rnIn this paper, the limit analysis procedure proposed in [6] is employed to thisrnpurpose in conjunction with the TRIC shell element developed by Argyris and coworkersrnin [16], which is modiu0002ed to some extent to adapt to the rigid-plastic context.rnSome examples show the effectiveness and the accuracy of the method, which comparesrnwell with results obtained from complete, although computationally demanding,rnincremental elastic-plastic approaches.
机译:极限分析问题的数值解决方案近年来受到越来越多的关注。在这种情况下开发的方法也可以用于获得崩溃后结构响应的指示,这在多种情况下都是必需的,例如用作减震器或消能器的壳体。该过程称为顺序极限分析,其名称为建议使用一系列极限分析解决方案,这些解决方案是指逐步更新的配置。本文中,[6]中提出的极限分析程序与Argyris和同事[16]开发的TRIC壳单元一起用于此目的。某些示例显示了该方法的有效性和准确性,与从完整的结果(尽管在计算上需要增量的弹塑性方法)进行的比较,它的有效性和准确性。

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