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首页> 外文期刊>International Journal of Solids and Structures >A mesh-independent interface technology for simulation of mixed-mode delamination growth
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A mesh-independent interface technology for simulation of mixed-mode delamination growth

机译:与网格无关的接口技术,用于模拟混合模式分层生长

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摘要

An effective interface element technology is presented for connecting and simulating crack growth between independently modeled finite element subdomains (e.g., composite plies). This method has been developed using penalty constraints and allows coupling of finite element models whose nodes do not necessarily coincide along their common interface. Additionally, the present formulation leads to a computational approach that is very efficient and completely compatible with existing commercial software. The present interface element has been implemented in the commercial finite element code ABAQUS as a user element subroutine (UEL), making it easy to test the approach for a wide range of problems. The interface element technology has been formulated to simulate delamination growth in composite laminates. Thanks to its special features, the interface element approach makes it possible to release portions of the interface surface whose length is smaller than that of the finite elements. In addition, the penalty parameter can vary within the interface element, allowing the damage model to be applied to a desired fraction of the interface between the two meshes. Results for double cantilever beam DCB, end-loaded split (ELS) and fixed-ratio mixed mode (FRMM) specimens are presented. These results are compared to measured data to assess the ability of the present damage model to simulate crack growth. (C) 2004 Elsevier Ltd. All rights reserved.
机译:提出了一种有效的界面元素技术,用于连接和模拟独立建模的有限元子域(例如,复合层)之间的裂纹扩展。该方法是使用惩罚约束开发的,并允许耦合其节点不一定沿其公共接口重合的有限元模型。另外,本发明提出了一种非常有效并且与现有商业软件完全兼容的计算方法。本接口元素已经在商业有限元代码ABAQUS中实现为用户元素子例程(UEL),从而可以轻松地针对各种问题测试该方法。界面元素技术已被制定为模拟复合材料层压板中的分层增长。由于其特殊的功能,界面元素方法使得可以释放界面表面的长度小于有限元素的部分。另外,惩罚参数可以在界面元素内变化,从而允许将损坏模型应用于两个网格之间界面的期望部分。给出了双悬臂梁DCB,端载荷分裂(ELS)和固定比率混合模式(FRMM)标本的结果。将这些结果与测量数据进行比较,以评估当前损伤模型模拟裂纹扩展的能力。 (C)2004 Elsevier Ltd.保留所有权利。

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