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Fatigue life prediction of GFRP laminates using averaged Bayesian predictive distribution and Lamb wave velocity

机译:使用平均贝叶斯预测分布和LAMB波速度GFRP层压板的疲劳寿命预测

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摘要

This paper presents a fatigue life prediction approach for GFRP laminates using laser ultrasonic technique for data acquisition and a hierarchical Bayesian model for damage characterization as well as life prediction. Fatigue damage is measured as the degradation of the Lamb wave velocity and described using a scalar damage variable. Due to the complexity of the damage mechanisms involved in the fatigue process and the difficulties in distinguishing different damage modes, i.e. fiber breakage, matrix cracks and delamination, from a single damage variable, multiple degradation models of various levels of complexity are proposed to form a meta-model. Bayesian inference is applied to obtain the distributions of model parameters to include uncertainty information. Then a stacking approach is applied to average the predictive distributions to obtain the optimal combination of each sub-model to generate a meta-prediction with the least diverge from the experimental observation. Experimental results of both traditional stiffness data and Lamb wave velocity data are used for validation. A credible interval (CI) based criterion is also proposed for fatigue life prediction, where consistent results are achieved with reasonable use of informative priors.
机译:本文介绍了使用激光超声技术的GFRP层压板的疲劳寿命预测方法,用于数据采集,以及用于损伤表征的分层贝叶斯模型以及生命预测。测量疲劳损坏作为羊隙波速度的劣化,并使用标量损伤变量描述。由于疲劳过程中涉及损伤机制的复杂性和区分不同损伤模式的困难,即纤维破损,矩阵裂缝和分层,从单个损伤变量,提出了各种复杂性的多种降级模型来形成a元模型。应用贝叶斯推断以获得模型参数的分布,包括不确定性信息。然后将堆叠方法应用于平均预测性分布以获得每个子模型的最佳组合,以产生具有从实验观察中最不分歧的元预测。传统刚度数据和羊羔波速度数据的实验结果用于验证。对于疲劳寿命预测,还提出了一种可靠的间隔(CI)标准,其中通过合理使用信息前瞻性实现了一致的结果。

著录项

  • 来源
    《Composites Science and Technology》 |2020年第18期|108213.1-108213.12|共12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;

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

    Polymer-matrix composites (PMCs); Fatigue; Statistics; Ultrasonics; Life prediction;

    机译:聚合物 - 基质复合材料(PMC);疲劳;统计;超声波;生活预测;

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