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A novel understanding of the normalized fatigue delamination model for composite multidirectional laminates

机译:对复合多向层压板归一化疲劳分层模型的新理解

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摘要

Normalized fatigue delamination models have been widely applied by researchers in the characterization of the fatigue delamination behavior of composite laminates. However, the inherent mechanism of this normalization method has not been explored. This study aims to present a physical understanding on the normalized fatigue delamination model from a viewpoint of energy. The fatigue delamination behavior is considered to be governed by the driving force and delamination resistance, and based on this principle the physical mechanism of the fatigue delamination is studied. A new physics-based normalized fatigue delamination model is proposed in this paper. In order to experimentally validate the proposed fatigue delamination model, mode I fatigue delamination tests are performed on double cantilever beam specimens to obtain the experimental data with different amounts of the fiber bridging. The results show that the normalized model is suitable to accurately characterize the fatigue delamination behavior of the composite laminates by using a single master curve. The master curve is finally employed as a standard approach to predict the fatigue results. Good agreement between the predicted and the experimental results is achieved, therefore it approves the applicability of the proposed fatigue delamination model in characterizing the fatigue delamination growth behavior.
机译:研究人员已广泛地使用归一化疲劳分层模型来表征复合材料层压板的疲劳分层行为。但是,尚未探讨此归一化方法的内在机理。这项研究旨在从能量的角度提出对归一化疲劳分层模型的物理理解。疲劳分层行为被认为是受驱动力和抗分层性支配的,并且基于该原理,研究了疲劳分层的物理机理。提出了一种新的基于物理的归一化疲劳分层模型。为了通过实验验证所提出的疲劳分层模型,对双悬臂梁试样进行了I型疲劳分层测试,以获取不同数量的纤维桥接的实验数据。结果表明,归一化模型适合于通过使用单个主曲线来准确表征复合材料层压板的疲劳分层行为。最后,将主曲线用作预测疲劳结果的标准方法。在预测结果和实验结果之间取得了很好的一致性,因此,它证明了所提出的疲劳分层模型在表征疲劳分层生长行为方面的适用性。

著录项

  • 来源
    《Composite Structures》 |2019年第12期|111395.1-111395.8|共8页
  • 作者单位

    Chongqing Univ Coll Aerosp Engn Chongqing 400044 Peoples R China|Shenyang Aerosp Univ Key Lab Fundamental Sci Natl Def Aeronaut Digital Shenyang 110136 Liaoning Peoples R China;

    Zhejiang Univ Technol Coll Mat Sci & Engn Hangzhou 310014 Zhejiang Peoples R China;

    Chongqing Univ Coll Aerosp Engn Chongqing 400044 Peoples R China;

    Chongqing Univ Posts & Telecommun Coll Opto Elect Engn Chongqing 400065 Peoples R China;

    Cardiff Univ Cardiff Sch Engn Cardiff CF24 3AA S Glam Wales;

    Univ Siegen Dept Civil Engn D-57068 Siegen Germany;

  • 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

    Composite laminates; Fatigue; Delamination growth; Fiber bridging;

    机译:复合层压板;疲劳;分层增长;光纤桥接;

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