Multiscale modelling for fatigue crack propagation of notched laminates using the UMAP clustering algorithm
In this study, a novel multiscale fatigue-damage model was developed based on the parametric finite-volume direct-averaging micromechanics theory (FVDAM), the uniform manifold approximation and projection (UMAP) algorithm, and the extended finite element method (XFEM) to accurately portray the progr...
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| Published in | Thin-walled structures Vol. 199; p. 111819 |
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| Main Authors | , , , , , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.06.2024
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| Subjects | |
| Online Access | Get full text |
| ISSN | 0263-8231 1879-3223 |
| DOI | 10.1016/j.tws.2024.111819 |
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| Abstract | In this study, a novel multiscale fatigue-damage model was developed based on the parametric finite-volume direct-averaging micromechanics theory (FVDAM), the uniform manifold approximation and projection (UMAP) algorithm, and the extended finite element method (XFEM) to accurately portray the progressive propagation of fatigue cracks in notched laminates. The UMAP clustering technique was integrated with fatigue damage evolution for the first time, enabling the construction of a reduced-order unit cell with fatigue information. Compared with the conventional FVDAM unit cell, the data was reduced to 0.4% of its original size, significantly accelerating fatigue damage calculations. The reduced-order unit cell was then incorporated into XFEM, functions as the fatigue damage criterion, transmitting fatigue damage information to meso- and macro-scales, and enables fatigue crack simulation in notched laminates. To further accelerate the calculation, a cycle-jump scheme was integrated, resulting in computational time being 10 times shorter compared to cycle-by-cycle simulation while maintaining accuracy. To validate the effectiveness of the proposed model, experiments of notched [±60]7s glass-fibre/epoxy laminates under three different fatigue loads were conducted. The simulation results of all three loads were within a scatter band of factor two, which was a good accuracy in fatigue, showing the effectiveness of the proposed model.
•A multi-scale fatigue model is built based on the FVDAM, XFEM, and UMAP clustering.•UMAP clustering method is incorporated with the fatigue damage evolution.•The effectiveness of the model is verified by the fatigue tests. |
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| AbstractList | In this study, a novel multiscale fatigue-damage model was developed based on the parametric finite-volume direct-averaging micromechanics theory (FVDAM), the uniform manifold approximation and projection (UMAP) algorithm, and the extended finite element method (XFEM) to accurately portray the progressive propagation of fatigue cracks in notched laminates. The UMAP clustering technique was integrated with fatigue damage evolution for the first time, enabling the construction of a reduced-order unit cell with fatigue information. Compared with the conventional FVDAM unit cell, the data was reduced to 0.4% of its original size, significantly accelerating fatigue damage calculations. The reduced-order unit cell was then incorporated into XFEM, functions as the fatigue damage criterion, transmitting fatigue damage information to meso- and macro-scales, and enables fatigue crack simulation in notched laminates. To further accelerate the calculation, a cycle-jump scheme was integrated, resulting in computational time being 10 times shorter compared to cycle-by-cycle simulation while maintaining accuracy. To validate the effectiveness of the proposed model, experiments of notched [±60]7s glass-fibre/epoxy laminates under three different fatigue loads were conducted. The simulation results of all three loads were within a scatter band of factor two, which was a good accuracy in fatigue, showing the effectiveness of the proposed model.
•A multi-scale fatigue model is built based on the FVDAM, XFEM, and UMAP clustering.•UMAP clustering method is incorporated with the fatigue damage evolution.•The effectiveness of the model is verified by the fatigue tests. |
| ArticleNumber | 111819 |
| Author | Yang, Danhui Song, Xinyi Guan, Zhongwei Ma, Mingze Zhou, Jin Li, Jianping Wei, Viska Chen, Xuefeng |
| Author_xml | – sequence: 1 givenname: Danhui surname: Yang fullname: Yang, Danhui organization: School of Resources and Environmental Engineering, East China University of Science and Technology, Shanghai, 200237, China – sequence: 2 givenname: Mingze surname: Ma fullname: Ma, Mingze organization: College of General Aviation and Flight, Nanjing University of Aeronautics and Astronautics, Liyang 213300, China – sequence: 3 givenname: Viska surname: Wei fullname: Wei, Viska organization: Johns Hopkins University, Baltimore, MD 21211, USA – sequence: 4 givenname: Jianping surname: Li fullname: Li, Jianping email: lijianping1016@scu.edu.cn organization: College of Carbon Neutrality Future Technology, Sichuan University, Chengdu, 610207, China – sequence: 5 givenname: Jin orcidid: 0000-0003-0584-3894 surname: Zhou fullname: Zhou, Jin organization: School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China – sequence: 6 givenname: Xinyi surname: Song fullname: Song, Xinyi organization: School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China – sequence: 7 givenname: Zhongwei orcidid: 0000-0002-6129-0668 surname: Guan fullname: Guan, Zhongwei organization: Advanced Materials Research Centre Technology Innovation Institute, Abu Dhabi, United Arab Emirates – sequence: 8 givenname: Xuefeng surname: Chen fullname: Chen, Xuefeng organization: School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China |
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