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Modelling damage in multidirectional laminates subjected to multi-axial loading: Ply thickness effects and model assessment

机译:多向层压板的模型损伤,经过多轴载荷:帘布层厚度效应和模型评估

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摘要

A meso-scale damage modelling framework for composite laminates is assessed against multi-axial experimental data obtained from specimens subjected to combined tension/compression and shear loading using a modified Arcan fixture (MAF). Two laminates made from unidirectional carbon fibre-reinforced epoxy plies of different thickness are considered to investigate the ply thickness effect on the damage behaviour of modified open-hole specimens. Intra-laminar damage is predicted using a continuum damage model combined with a fibre-aligned mesh, while cohesive zones are used to account for inter-laminar damage. The multi-axial open-hole specimen strength is predicted with a mean relative error of 15% across all the investigated lay-up and loading configurations, while the predicted damage maps show encouraging agreement with full-field measurements obtained using digital image correlation (DIC). However, the assessment reveals limitations of the assumption of small strains and rotations in the formulation of the model that lead to spurious model behaviour for shear-dominated damage modes.
机译:对复合层压板的间隙尺度损伤建模框架评估了使用改性的arcan夹具(MAF)对组合张力/压缩和剪切载荷进行的试样获得的多轴实验数据。由单向碳纤维增强的不同厚度制成的两个层压板被认为是研究对改性开孔样本的损伤行为的帘布层厚度影响。使用连续损伤模型与光纤对齐网格结合的连续损伤模型预测了层内损伤,而粘性区域用于考虑层间损坏。在所有调查的铺设和加载配置中预测多轴开孔样本强度,平均相对误差为15%,而预测的损伤图显示了使用数字图像相关(DIC)获得的全场测量令人鼓舞的协议(DIC )。然而,评估揭示了对模型的制定中小菌株和旋转的假设的限制,导致剪切主导损伤模式的杂散模型行为。

著录项

  • 来源
    《Composite Structures》 |2021年第6期|113766.1-113766.15|共15页
  • 作者单位

    Univ Southampton Sch Engn Southampton SO17 1BJ Hants England|Univ Bristol Sch Civil Aerosp & Mech Engn Bristol Composites Inst Queens Bldg Bristol BS8 1TR Avon England;

    Univ Southampton Sch Engn Southampton SO17 1BJ Hants England|Univ Southampton Malaysia Sch Engn Iskandar Puteri 79200 Johor Malaysia;

    Univ Porto Fac Engn DEMec Rua Dr Roberto Frias S-N P-4200465 Porto Portugal|Inst Ciencia & Inovacao Engn Mecan & Engn Ind INEGI Rua Dr Roberto Frias 400 P-4200465 Porto Portugal|Univ Ghent Dept Mat Text & Chem Engn Mech Mat & Struct UGent MMS Technol Pk Zwijnaarde 46 B-9052 Zwijnaarde Belgium;

    Univ Porto Fac Engn DEMec Rua Dr Roberto Frias S-N P-4200465 Porto Portugal|Inst Ciencia & Inovacao Engn Mecan & Engn Ind INEGI Rua Dr Roberto Frias 400 P-4200465 Porto Portugal|MIT Dept Aeronaut & Astronaut 77 Massachusetts Ave Cambridge MA 02139 USA;

    Univ Porto Fac Engn DEMec Rua Dr Roberto Frias S-N P-4200465 Porto Portugal|Inst Ciencia & Inovacao Engn Mecan & Engn Ind INEGI Rua Dr Roberto Frias 400 P-4200465 Porto Portugal;

    Univ Porto Fac Engn DEMec Rua Dr Roberto Frias S-N P-4200465 Porto Portugal|Inst Ciencia & Inovacao Engn Mecan & Engn Ind INEGI Rua Dr Roberto Frias 400 P-4200465 Porto Portugal;

    Univ Bristol Sch Civil Aerosp & Mech Engn Bristol Composites Inst Queens Bldg Bristol BS8 1TR Avon England;

    Univ Southampton Sch Engn Southampton SO17 1BJ Hants England|Univ Bristol Sch Civil Aerosp & Mech Engn Bristol Composites Inst Queens Bldg Bristol BS8 1TR Avon England;

  • 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; Carbon fibre; Multiaxial loading; Finite element analysis (FEA); Damage mechanics; Modified Arcan Fixture (MAF);

    机译:复合层压板;碳纤维;多轴加载;有限元分析(FEA);损伤力学;改装arcan夹具(MAF);

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