journal article·2024-04-20Open access

Study on the low‐velocity impact response of the repaired carbon fiber‐reinforced plastic laminates: Bonded versus scarf repair

Xuanzhen Chen, Yong Peng, Kui Wang, Xin Wang, Zhixiang Liu, Zhiqiang Huang, Honghao Zhang

Polymer Composites· Volume 45· Issue 6

Abstract

Abstract Experimental and simulation studies of the response of bonded‐repaired and scarf‐repaired carbon fiber‐reinforced polymer laminates under the low‐velocity impact (LVI) were carried out. The center‐ and eccentric‐repaired laminates were prepared for experiments. The experimental results verify the validity of the finite element model in terms of the force response and different modes of damage. The effect of impact energy and the variation of repair position on the impact response of the laminate was investigated based on the benchmark model. The bonded repaired laminates have higher peak impact forces and lower energy absorption than the scarf‐repaired laminates; the damage of the bonded repaired laminate is mainly intralaminar damage and delamination damage of the patch; the adhesive of the scarf repair is prone to failure, leading to poor impact resistance. The relative positions of the impact point and the patch determine the impact response of a laminate repaired at different locations. The impact point at the edge of the patch has a detrimental effect on the repaired laminate. The impact point vertical position near the bottom hole edge of the parent plate in the scarf‐repaired case harms the impact resistance of the laminate. Highlights The low‐velocity impact response of bonded versus scarf‐repaired laminates was compared. Bonding repairs provide superior impact resistance to damaged laminates than scarf repairs. The risk of adhesive failure in scarf repair is significantly higher than in bonded repair. The relative position of the damage (repair) to the impact point critically influences the impact response. Impacts near the edge of the initial damage hole can cause severe damage to scarf‐repaired laminates.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Structural Analysis of Composite Materials

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Key Laboratory of Traffic Safety on Track (Central South University), Ministry of Education Changsha China

Joint International Research Laboratory of Key Technology for Rail Traffic Safety Central South University Changsha China

Key Laboratory of High Efficiency and Clean Mechanical Manufacture (Ministry of Education) School of Mechanical Engineering, Shandong University Jinan China

Funding

National Natural Science Foundation of China · Science Fund for Distinguished Young Scholars of Hunan Province

References (38)

Show source-provided references
1. 10.3390/jmse801002610.3390/jmse8010026 ↗
2. 10.1016/j.jmapro.2022.11.02410.1016/j.jmapro.2022.11.024 ↗
3. 10.1002/pc.2647810.1002/pc.26478 ↗
4. 10.1177/089270571881553010.1177/0892705718815530 ↗
5. 10.1016/j.compositesb.2022.11045010.1016/j.compositesb.2022.110450 ↗
6. 10.1016/j.compstruct.2008.03.02510.1016/j.compstruct.2008.03.025 ↗
7. 10.1016/j.compositesb.2019.10768810.1016/j.compositesb.2019.107688 ↗
8. 10.1016/j.compositesb.2018.03.01610.1016/j.compositesb.2018.03.016 ↗
9. 10.1016/j.paerosci.2013.03.00310.1016/j.paerosci.2013.03.003 ↗
10. 10.1177/073168442094160210.1177/0731684420941602 ↗
11. 10.1016/j.compstruct.2022.11633810.1016/j.compstruct.2022.116338 ↗
12. 10.1016/j.ijimpeng.2015.05.01410.1016/j.ijimpeng.2015.05.014 ↗
13. 10.1016/j.compositesa.2010.02.00510.1016/j.compositesa.2010.02.005 ↗
14. 10.1016/j.compositesa.2015.01.02510.1016/j.compositesa.2015.01.025 ↗
15. 10.1016/j.compstruct.2016.09.09910.1016/j.compstruct.2016.09.099 ↗
16. 10.1016/j.compstruct.2019.11111310.1016/j.compstruct.2019.111113 ↗
17. 10.1016/j.compstruct.2015.04.02310.1016/j.compstruct.2015.04.023 ↗
18. 10.1016/j.compstruct.2019.04.01210.1016/j.compstruct.2019.04.012 ↗
19. 10.1016/j.compstruct.2017.12.01210.1016/j.compstruct.2017.12.012 ↗
20. 10.1016/j.compstruct.2013.02.02710.1016/j.compstruct.2013.02.027 ↗
21. 10.1016/j.engfailanal.2017.12.01910.1016/j.engfailanal.2017.12.019 ↗
22. 10.1016/j.compositesb.2018.09.09610.1016/j.compositesb.2018.09.096 ↗
23. 10.1016/j.ijimpeng.2017.09.00410.1016/j.ijimpeng.2017.09.004 ↗
24. 10.1016/j.compositesb.2017.09.02010.1016/j.compositesb.2017.09.020 ↗
25. 10.1080/15376494.2018.152495210.1080/15376494.2018.1524952 ↗
26. 10.1016/j.compstruct.2018.01.07510.1016/j.compstruct.2018.01.075 ↗
27. 10.1016/j.ijmecsci.2019.10540710.1016/j.ijmecsci.2019.105407 ↗
28. 10.1016/j.compositesa.2011.05.01510.1016/j.compositesa.2011.05.015 ↗
29. 10.12989/scs.2014.17.2.19910.12989/scs.2014.17.2.199 ↗
30. 10.1177/073168441456246510.1177/0731684414562465 ↗
31. 10.1016/j.polymertesting.2019.10600010.1016/j.polymertesting.2019.106000 ↗
32. 10.1016/j.compositesb.2018.12.15310.1016/j.compositesb.2018.12.153 ↗
33. 10.1177/073168440302728510.1177/0731684403027285 ↗
34. ASTM D3518/D3518M‐13.Standard test method for in‐plane shear response of polymer matrix composite materials by tensile test of a ±45° laminate.2008.
35. 10.1016/j.compstruct.2012.07.00210.1016/j.compstruct.2012.07.002 ↗
36. CamanhoPP DavilaCG.Mixed‐Mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials. National Aeronautics and Space Agency USA. NASA‐Technical Paper 2117372002.
37. 10.1016/j.tafmec.2015.09.00710.1016/j.tafmec.2015.09.007 ↗
38. 10.1016/j.compositesb.2016.01.05610.1016/j.compositesb.2016.01.056 ↗