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Phase field based peridynamics damage model for delamination of composite structures

机译:基于相场的复合材料分层动力学损伤模型

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摘要

We extend and exploit a phase field based peridynamics (PD) damage model ([ 39]) for studying delamination of composite structures. Utilizing a phase field augmented PD framework, our idea is to model the interfacial cohesive damage through degradation functions and the fracture or fragmentation through the critical energy release rate. Our model eliminates the conventional traction-separation law (TSL) that is known to result in the popular cohesive zone model (CZM). In the process, the approach potentially addresses some limitations of the existing techniques, for example, CZM, virtual crack closure technique (VCCT) and so on, which make use of an empirical interaction among different modes of loading (e.g., mode I, mode II etc.). By regarding delamination under different loading conditions as problems that differ only in their boundary conditions, our approach provides for a more general scheme for tracking delamination growth. Our proposal thus accords no special treatment to the different modes and can handle general spatial locations of weaker interface layers. With no special crack tracking algorithms or additional ad-hoc criteria for crack propagation, considerable computational simplicity also accrues. The approach admits an easy extension to cases where cracks can propagate even in the bulk material body. The new bond breaking criterion that we employ replaces the ad-hoc approach inherent in bond-stretch-based or bond-energy-based conditions. Unlike standard phase field models, physical fragmentation of the body is feasible in the present model. The proposed methodology also eliminates the problem of matter interpenetration by its very construction. Apart from an initial validation exercise for a laminated composite plate with a hole where no or little damage occurs, we also use numerical simulations on mode I, mode II, and mixed mode delamination cases in order to assess the performance of our model by benchmarking it against available experimental evidence. Simulations on modified mixed mode bending and multiple layer delamination are also presented. (C) 2017 Elsevier Ltd. All rights reserved.
机译:我们扩展和利用基于相场的周动力(PD)损伤模型([39])来研究复合结构的分层。利用相场增强的PD框架,我们的想法是通过退化函数模拟界面内聚破坏,并通过临界能量释放率模拟断裂或破碎。我们的模型消除了传统的牵引分离法则(TSL),已知该法则导致了流行的粘聚区模型(CZM)。在此过程中,该方法潜在地解决了现有技术的一些局限性,例如CZM,虚拟裂缝闭合技术(VCCT)等,这些局限性利用了不同加载方式(例如,方式I,方式II等)。通过将在不同载荷条件下的分层视为仅在其边界条件上不同的问题,我们的方法为跟踪分层的增长提供了一种更通用的方案。因此,我们的建议对不同的模式不做任何特殊处理,并且可以处理较弱的界面层的一般空间位置。由于没有特殊的裂纹跟踪算法或裂纹扩展的额外临时标准,因此也大大简化了计算。该方法允许容易扩展到甚至在散装材料主体中裂纹也可能传播的情况。我们采用的新的断裂键标准取代了基于键拉伸或基于键能量的条件中固有的临时方法。与标准相场模型不同,在本模型中,身体的物理破碎是可行的。所提出的方法还通过其构造消除了物质互穿的问题。除了对没有孔或几乎没有损坏的孔的层压复合板的初始验证工作之外,我们还对模式I,模式II和混合模式分层情况进行了数值模拟,以便通过对模型进行基准测试来评估其性能反对现有的实验证据。还介绍了修改的混合模式弯曲和多层分层的仿真。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2017年第11期|972-993|共22页
  • 作者单位

    Indian Inst Sci, Dept Civil Engn, Computat Mech Lab, Bangalore 560012, Karnataka, India;

    Indian Inst Sci, Dept Civil Engn, Computat Mech Lab, Bangalore 560012, Karnataka, India;

    Indian Inst Sci, Dept Civil Engn, Computat Mech Lab, Bangalore 560012, Karnataka, India;

    Indian Inst Sci, Dept Civil Engn, Computat Mech Lab, Bangalore 560012, Karnataka, India;

    Texas A&M Univ, Dept Mech Engn, Adv Computat Mech Lab, College Stn, TX 77843 USA;

  • 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

    Phase field; Peridynamics; Delamination; Mixed mode; Multiple-layer delamination;

    机译:相场;空气动力学;分层;混合模式;多层分层;

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