Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior
The adhesive joint of composite materials is one of the typical structures in aircraft structures, and the delamination damage is one of the most important damage modes in composite adhesive joints. In this paper, static and fatigue tests were carried out on L-shaped adhesive joints to analyze the d...
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Language: | zho |
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EDP Sciences
2021-04-01
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Series: | Xibei Gongye Daxue Xuebao |
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Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/02/jnwpu2021392p309/jnwpu2021392p309.html |
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collection | DOAJ |
description | The adhesive joint of composite materials is one of the typical structures in aircraft structures, and the delamination damage is one of the most important damage modes in composite adhesive joints. In this paper, static and fatigue tests were carried out on L-shaped adhesive joints to analyze the damage evolution and failure modes of delamination damage under static and fatigue loadings. Based on the cohesive constitutive models, the static and high-cycle fatigue delamination constitutive models were developed. The static and fatigue numerical models of composite L-shaped adhesive joints were established by using finite element software. The stress distribution, deformation modes and delamination propagation laws were systematically studied. The simulation results are in good agreement with the experimental results. The delamination damage initiation, evolution and failure mechanism of L-shaped adhesive joints under static and fatigue loads were revealed by combining the experimental and the numerical results, which will provide theoretical and engineering guidance for strength and fatigue analysis of composite adhesive structures. |
first_indexed | 2024-03-09T09:04:48Z |
format | Article |
id | doaj.art-21fbcc0f64984424a4ac87484951df9c |
institution | Directory Open Access Journal |
issn | 1000-2758 2609-7125 |
language | zho |
last_indexed | 2024-03-09T09:04:48Z |
publishDate | 2021-04-01 |
publisher | EDP Sciences |
record_format | Article |
series | Xibei Gongye Daxue Xuebao |
spelling | doaj.art-21fbcc0f64984424a4ac87484951df9c2023-12-02T10:34:55ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252021-04-0139230931610.1051/jnwpu/20213920309jnwpu2021392p309Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior0123School of Science, Chang'an UniversitySchool of Aeronautics, Northwestern Polytechnical UniversityInstitute of Engineering Thermophysics, Chinese Academy of SciencesSchool of Science, Chang'an UniversityThe adhesive joint of composite materials is one of the typical structures in aircraft structures, and the delamination damage is one of the most important damage modes in composite adhesive joints. In this paper, static and fatigue tests were carried out on L-shaped adhesive joints to analyze the damage evolution and failure modes of delamination damage under static and fatigue loadings. Based on the cohesive constitutive models, the static and high-cycle fatigue delamination constitutive models were developed. The static and fatigue numerical models of composite L-shaped adhesive joints were established by using finite element software. The stress distribution, deformation modes and delamination propagation laws were systematically studied. The simulation results are in good agreement with the experimental results. The delamination damage initiation, evolution and failure mechanism of L-shaped adhesive joints under static and fatigue loads were revealed by combining the experimental and the numerical results, which will provide theoretical and engineering guidance for strength and fatigue analysis of composite adhesive structures.https://www.jnwpu.org/articles/jnwpu/full_html/2021/02/jnwpu2021392p309/jnwpu2021392p309.htmlcompositesadhesive jointsfatiguedelamination damagesimulationtest |
spellingShingle | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior Xibei Gongye Daxue Xuebao composites adhesive joints fatigue delamination damage simulation test |
title | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior |
title_full | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior |
title_fullStr | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior |
title_full_unstemmed | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior |
title_short | Study on delamination damage evolution of composite L-shaped adhesive joint based on cohesive behavior |
title_sort | study on delamination damage evolution of composite l shaped adhesive joint based on cohesive behavior |
topic | composites adhesive joints fatigue delamination damage simulation test |
url | https://www.jnwpu.org/articles/jnwpu/full_html/2021/02/jnwpu2021392p309/jnwpu2021392p309.html |