南京航空航天大学学报2024,Vol.56Issue(3) :468-477.DOI:10.16356/j.1005-2615.2024.03.010

基于深度学习的复合材料开孔板拉伸失效行为预测

Prediction of Tensile Failure Behavior of Open-Hole Composite Plates Based on Deep Learning

崔翼扬 陈普会
南京航空航天大学学报2024,Vol.56Issue(3) :468-477.DOI:10.16356/j.1005-2615.2024.03.010

基于深度学习的复合材料开孔板拉伸失效行为预测

Prediction of Tensile Failure Behavior of Open-Hole Composite Plates Based on Deep Learning

崔翼扬 1陈普会1
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作者信息

  • 1. 南京航空航天大学航空学院,南京 210016
  • 折叠

摘要

为研究复合材料开孔板在拉伸载荷下的失效行为,基于开孔板的拉伸试验建立了高精度的有限元仿真模型,并批量生成了拉伸载荷-位移曲线的数据集.提出了一种双长短时记忆(Long short-term memory,LSTM)神经网络模型用于预测载荷-位移曲线,其中第1个LSTM模型进行输入特征的提取,第2个LSTM模型直接给出载荷-位移曲线的预测.结果表明:这一模型能够高效、准确地预测开孔板的拉伸载荷-位移曲线,在测试集上的决定系数R2 可以达到 0.975 5,关键特征如初始刚度E0 的预测误差仅为 1.85%,极限载荷Fmax的预测误差仅为2.16%.

Abstract

To investigate the failure behavior of composite open-hole plates under tensile loads,a high-precision finite element simulation model is established based on tensile tests of open-hole plates,and a dataset of tensile force-displacement curves is generated in batches.Then,dual long short-term memory(LSTM)neural network models are proposed to predict the force-displacement curve.The first LSTM model is responsible for extracting input features,while the second one directly predicts the force-displacement curve.The research results indicate that this model can efficiently and accurately predict the tensile force-displacement curves of open-hole plates.The coefficient of determination R2 on the test set reaches as high as 0.975 5,with the prediction error of key features such as the initial stiffness E0 being only 1.85%and the prediction error of the maximum load Fmax being only 2.16%.

关键词

复合材料开孔板/失效行为预测/载荷-位移曲线/深度学习/长短时记忆模型

Key words

composite open-hole plates/failure behavior prediction/force-displacement curve/deep learning/long short-term memory(LSTM)model

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出版年

2024
南京航空航天大学学报
南京航空航天大学

南京航空航天大学学报

CSTPCDCSCD北大核心
影响因子:0.734
ISSN:1005-2615
参考文献量21
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