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Characterization of fatigue damages in composite laminates using Lamb wave velocity and prediction of residual life

机译:用兰姆波速度表征复合材料层板的疲劳损伤并预测剩余寿命

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摘要

In this paper, the So-mode Lamb wave phase velocity at low frequency range is chosen to characterize fatigue damages accumulated in composite laminates under cyclic loadings. A stiffness velocity degradation model is proposed based on three distinctive damage mechanisms: fiber breaks, matrix cracks and delamination, all of which are always involved in fatigue damage process. In order to reduce the complexity of the damage model, fiber damage is treated as an independent damage and delamination is coupled with matrix cracks. An approximation of shear-lag model is then proposed to avoid any direct measurements of crack density for it is highly impractical in real applications. Following this, energy release rate for formation of matrix cracks is extracted based on measured phase velocity and damage evolution is realized by incorporating a modified Paris law. Controlled fatigue experiments were conducted where in-situ phase velocity was measured by a laser ultrasonic system. The fatigue damages were then characterized using the proposed damage model with the measured velocity. Finally, the ability of proposed model to predict residual lives was also validated and good accuracy has been obtained. (C) 2017 Elsevier Ltd. All rights reserved.
机译:在本文中,选择So-模式Lamb波在低频范围内的相速度来表征复合材料层压板在循环载荷下累积的疲劳损伤。提出了一种基于三种独特的损伤机理的刚度速度退化模型:纤维断裂,基体裂纹和分层,所有这些始终与疲劳损伤过程有关。为了降低损伤模型的复杂性,将纤维损伤视为独立损伤,并将分层与基体裂纹相结合。然后提出了剪切滞后模型的近似值,以避免对裂纹密度进行任何直接测量,因为它在实际应用中非常不切实际。此后,根据测得的相速度提取用于形成基体裂纹的能量释放速率,并通过合并修正的巴黎定律实现损伤演化。进行受控的疲劳实验,其中通过激光超声系统测量原位相速度。然后使用建议的损伤模型和测得的速度来表征疲劳损伤。最后,所提出的模型预测剩余寿命的能力也得到了验证,并获得了良好的准确性。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2017年第15期|219-228|共10页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China;

  • 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 laminate; Fatigue; Lamb wave; Life prediction; Laser ultrasonic;

    机译:复合材料层合板;疲劳;兰姆波;寿命预测;激光超声;

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