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Numerical Aspects of Delamination Modeling Using Interface Elements

机译:使用界面元素进行分层建模的数值方面

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In spite of a vast background on cohesive constitutive law and its use for various analyses such as delamination in composite laminates, some numerical aspects of that have been less explored and reported in the literature. The aim of this paper is to study the phenomenon of spurious stress oscillation and also dominant process zone (where damage has its most significant evolution) in delamination modeling. For this purpose, distribution of normal stress and damage parameter of different DCB specimen are analyzed. Distribution of stress around the process zone indicates spurious oscillation just ahead of the delamination tip where damage parameter is zero and no effect of this phenomenon is seen on results of applied load versus opening displacement. Additionally, it is shown that larger values of penalty stiffness lead in smaller length of dominant process zone and very large values of penalty stiffness pushes the distribution of damage parameter to become step-like function. Authors believe that this effect is in fact the main reason of un-converged solution of models with too large penalty values.
机译:尽管内聚本构法及其在​​各种分析中的应用(例如复合层压板的分层)具有广阔的背景,但在文献中却很少探讨和报道这些方面的数值方面。本文的目的是研究分层建模中的虚假应力振荡现象以及主要的过程区域(其中损伤具有最大的演变)。为此,分析了不同DCB试样的正应力分布和损伤参数。应力在工艺区域周围的分布表明,在分层尖端之前出现了虚假振荡,在分层尖端,损伤参数为零,并且在施加的载荷与开口位移的关系中,未发现这种现象的影响。此外,还表明,惩罚刚度的值越大,主导过程区域的长度越短,惩罚刚度的值越大,则破坏参数的分布就呈阶梯状函数。作者认为,这种影响实际上是惩罚值太大的模型未收敛解的主要原因。

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