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Augmented Cohesive Elements for Efficient Delamination Analyses of Composite Laminates

机译:增强的粘结元件,可对复合材料层压板进行有效的分层分析

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摘要

In this paper, a new type of cohesive element that employs multiple suhdomain integra tion (MSDI) for improved cohesive stress integration accuracy of bonded plate/shell elements has been formulated. Within each suhdomain, stress integration is compatible with existing schemes such as Gaussian integration (GI), Newton-Cotes integration, or the mixed Gaussian and subdomain integration (mixed GI&SDI). The numerical accu racy, efficiency, and robustness of this element when employing three integration methods for MSD cohesive stress integration have been evaluated and compared through a bench mark mode-/ fracture problem of bonded double-cantilever plates. The MSDI offers at least 50% improvement of numerical accuracy as compared to the best integration method in literature and has the best numerical robustness. This significant improvement pushes the structural mesh size restriction from limiting size of 113-115 cohesive zone length to 1.5-2 times the cohesive zone length. The formulation is very easy to be imple mented into any finite element programs including commercial packages. Furthermore, this formulation enables the use of dual-mesh for delamination analyses of bonded struc tural shells/plates, which is of practical importance because it greatly reduces the burden of mesh generation for complicated composite structures. It has also been demonstrated that using high-order shell/plate elements can improve the numerical accuracy in general because the nonlinear deformation profile permitted by this type of elements can better describe the nonlinear deformation in the crack-tip element (partially bonded elements).
机译:在本文中,已经提出了一种新型的粘结元件,该粘结元件采用多重Suhdomain集成(MSDI)来提高粘结板/壳单元的粘结应力集成精度。在每个suhdomain中,应力积分与现有方案兼容,例如高斯积分(GI),Newton-Cotes积分或混合的高斯和子域积分(混合GI&SDI)。通过结合双悬臂板的基准模式/断裂问题,评估并比较了采用三种积分方法进行MSD内聚​​应力积分时该元件的数值精度,效率和鲁棒性。与文献中的最佳积分方法相比,MSDI可使数值精度至少提高50%,并且具有最佳的数值鲁棒性。这一重大改进将结构筛孔尺寸的限制从113-115粘结区长度的极限尺寸提高到粘结区长度的1.5-2倍。该公式很容易在包括商业软件包在内的任何有限元程序中实现。此外,该配方使得能够使用双重网格对粘合的结构壳/板进行分层分析,这具有实际意义,因为它大大减少了复杂复合结构产生网格的负担。还已经证明,使用高阶壳/板单元通常可以提高数值精度,因为这种类型的单元所允许的非线性变形轮廓可以更好地描述裂纹尖端单元(部分结合的单元)中的非线性变形。

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  • 作者单位

    Department of Engineering Mechanics, Zhejiang University, Hangzhou, China 310027;

    Department of Engineering Mechanics, Zhejiang University, Hangzhou, China 310027;

    Department of Mechanical and Aerospace Engineering, University of Miami, Coral Gables, FL 33124;

    Global Engineering and Materials, Inc., 1 Airport Place, Suite 1, Suite 200, Princeton, NJ 08540;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    cohesive element; delamination; fracture; laminates;

    机译:内聚元素分层断裂;层压板;

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