Study on Prediction of Compression Performance of Composite Laminates After Impact Based on Convolutional Neural Networks

被引:1
作者
Fengyang Jiang
Zhidong Guan
Xiaodong Wang
Zengshan Li
Riming Tan
Cheng Qiu
机构
[1] Beihang University,School of Aeronautic Science and Engineering
[2] Hong Kong University of Science and Technology,Department of Mechanical and Aerospace Engineering
来源
Applied Composite Materials | 2021年 / 28卷
关键词
Damage tolerance; Non-destructive testing; Machine learning; Convolutional neural networks;
D O I
暂无
中图分类号
学科分类号
摘要
This paper proposed a method for predicting composite laminates’ compressive residual strength after impact based on convolutional neural networks. Laminates made by M21E/IMA prepreg were used to introduce low-velocity impact damage and construct a non-destructive testing image dataset. The dataset images characterized the impact damage details, including dents, delamination, and matrix cracking. The convolution kernel automatically extracted and identified these complex features that could be used for classification. The model took the images as input and compressive residual strength labels as output for iterative training, and the final prediction accuracy reached more than 90%, the highest 96%. This method introduced overall damage into the model in the form of images utilizing convolution, which can quickly and accurately predicted laminates’ compression performance after impact.
引用
收藏
页码:1153 / 1173
页数:20
相关论文
共 141 条
  • [1] Talreja R(2019)Assessment of damage tolerance approaches for composite aircraft with focus on barely visible impact damage Compos. Struct. 219 1-7
  • [2] Phan N(2019)Impact resistance and damage tolerance of fiber reinforced composites: A review Compos. Struct. 217 100-121
  • [3] Shah SZH(2011)Analysis and Compression Testing of Laminates Optimised for Damage Tolerance Appl. Compos. Mater. 18 85-100
  • [4] Karuppanan S(2010)Detecting Low Velocity Impact Damage in Composite Plate Using Nonlinear Acoustic/Ultrasound Methods Appl. Compos. Mater. 17 481-488
  • [5] Megat-Yusoff PSM(2008)Detecting Damage in Composite Material Using Nonlinear Elastic Wave Spectroscopy Methods Appl. Compos. Mater. 15 115-126
  • [6] Sajid Z(2017)Simulation of Low Velocity Impact Induced Inter- and Intra-Laminar Damage of Composite Beams Based on XFEM Appl. Compos. Mater. 24 1459-1477
  • [7] Rhead AT(2017)A Progressive Damage Model for Predicting Permanent Indentation and Impact Damage in Composite Laminates Appl. Compos. Mater. 24 1029-1048
  • [8] Butler R(2019)Relationship Between Matrix Cracking and Delamination in CFRP Cross-Ply Laminates Subjected to Low Velocity Impact Materials. 12 3990-242
  • [9] Baker N(2020)A fast and efficient numerical prediction of compression after impact (CAI) strength of composite laminates and structures Thin-Walled Struct. 148 106588-61
  • [10] Polimeno U(2013)Prediction of permanent indentation due to impact on laminated composites based on an elasto-plastic model incorporating fiber failure Compos. Struct. 96 232-182