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Experimental investigation on damage evolution in cross-ply laminates subjected to quasi-static and fatigue loading

机译:准静态和疲劳载荷作用下交叉层压板损伤演化的实验研究

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摘要

In this paper an experimental investigation on damage evolution in cross-ply glass fiber reinforced plastic (GFRP) laminates under quasi-static and fatigue loading is presented. Four configurations of lay-up ([0(2)/90(4)](s), [0(2)/90(2)](s), [0/90(4)](s) and [0/90(3)/0/90(3)](s)) with different thicknesses of cracking plies were selected to study the in-situ behavior in the damage initiation, evolution and saturation. Combined with the imaging features of different damages and the characteristic of damage evolution in the laminates, light transmission method was employed to observe the damage state and to record matrix crack density. In fatigue tests, eight stress levels were chosen for each configuration of laminates, including four lower stress levels below the stress level corresponding to the first transverse crack initiation. A conclusion was drawn from the comparison of the results that the fatigue loading with lower stress level accelerates the process of damage evolution and generates damages more thoroughly at failure. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文提出了在准静态和疲劳载荷下玻璃纤维增​​强塑料(GFRP)层压板损伤演化的实验研究。叠加的四种配置([0(2)/ 90(4)](s),[0(2)/ 90(2)](s),[0/90(4)](s)和[选择具有不同厚度的开裂帘布层的0/90(3)/ 0/90(3)](s),以研究损伤破坏,演化和饱和的原位行为。结合不同损伤的成像特征和层压板损伤演化的特点,采用光透射法观察损伤状态并记录基体裂纹密度。在疲劳测试中,为层压板的每种配置选择了八个应力水平,包括低于对应于第一次横向裂纹萌生的应力水平的四个较低应力水平。从结果的比较得出结论,较低应力水平的疲劳载荷会加速损伤的发展过程,并在失效时更彻底地产生损伤。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composites》 |2017年第7期|10-26|共17页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Tech, Nanjing 210016, Jiangsu, Peoples R China|Nanjing Res Inst Simulat Tech, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Tech, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Tech, Nanjing 210016, Jiangsu, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Quasi-static loading; Fatigue loading; Matrix crack; Stress level; In-situ behavior;

    机译:准静态载荷;疲劳载荷;基体裂纹;应力水平;原位行为;

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