An Adaptive Floating Node Based Formulation for Progressive Fatigue Analysis of Multiple Delaminations

G. Trabal, B. Bak, B. Chen, E. Lindgaard
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Abstract

Fatigue-driven delamination is one of the main damage modes leading to the final failure of composite laminated structures. Great advances have been achieved in recent years on accurate modelling of delamination onset and growth under fatigue loading by the use of Cohesive Zone Models (CZM) integrated into cohesive interface finite elements. Although the implementation of such models in Finite Elements Analysis (FEA) through decohesion elements is available in literature and research codes, resulting models are still computationally expensive and require intensive modelling work by the user. These disadvantages make the simulation of multiple delaminations on a general layup at the structural level an impossible task. A new analysis methodology named the Floating Node Method (FNM) has recently been proposed [1] that has the potential to overcome these issues. In this work, a new numerical fatigue formulation based on an FNM enhanced element and a new adaptive refinement scheme is presented. The FNM-based element is capable of including new cohesive elements at any interface in the model as well as refining existing elements without the use of remeshing. The adaptive refinement scheme is based on local information at the element level, i.e. damage state, without hard-coded and problem-dependent user inputs. The suggested adaptive refinement scheme successfully refine and coarse the mesh adaptively as well as, include CZ elements at needed interfaces during the iterative solution procedure rendering the solution accurate and efficient. The delamination growth in the different interfaces is accounted for using a fatigue model based on [2] which combines a quasi-static
基于自适应浮动节点的多层逐级疲劳分析公式
疲劳驱动脱层是导致复合材料层合结构最终失效的主要损伤形式之一。近年来,结合黏性界面有限元的黏性区模型(CZM)在疲劳载荷下的分层发生和发展的精确建模方面取得了很大进展。尽管在文献和研究代码中可以通过解聚元素在有限元分析(FEA)中实现这种模型,但由此产生的模型仍然需要大量的计算成本,并且需要用户进行大量的建模工作。这些缺点使得在结构层面上对一般层的多重分层进行模拟成为不可能完成的任务。最近提出了一种名为浮动节点法(FNM)的新分析方法[1],它有可能克服这些问题。本文提出了一种新的基于FNM增强单元的疲劳数值公式和一种新的自适应细化方案。基于fnm的元素能够在模型的任何接口上包含新的内聚元素,并在不使用重网格的情况下精炼现有元素。自适应改进方案基于元素级别的局部信息,即损坏状态,不需要硬编码和问题相关的用户输入。所提出的自适应细化方案成功地对网格进行了自适应细化和粗化,并在迭代求解过程中在需要的接口处包含了CZ元素,使求解更加准确和高效。使用基于[2]的准静态疲劳模型来解释不同界面中的分层生长
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