Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses
Abstract
Here, this study investigates the failure mechanisms of cross-ply laminates subjected to longitudinal compressive loading. A sequence of failure initiation and propagation process is observed based on optical microscopy images of failed specimens. Specifically, the failure process in the cross-ply laminates involves a combination of four failure mechanisms: fiber kinking, delamination, matrix cracking, and fiber/matrix splitting. We find that the kink-bands in the middle 0° plies of the cross-ply laminates most often show a wedge shape and the angle of matrix cracks in the 90° plies is slightly larger than that of pure 90° plies. The reason has been attributed to the constraining effects by the adjacent plies. The next focus of this study is to propose hybrid micro-macro models to more systematically study the failure mechanisms of the cross-ply laminates. We show that these models accurately predict the combined failure modes of the cross-ply laminates and enable us to closely investigate the interactions of different failure mechanisms. More importantly, the hybrid models achieve great computational efficiency compared to full-scale microstructural models. Finally, the combined experimental and computational analyses presented here provide a new level of understanding of the kink-band morphology and damage mechanisms in the cross-ply laminates.
- Authors:
-
- Nanjing University of Aeronautics and Astronautics (China); Ford Motor Company, Dearborn, MI (United States)
- The Ohio State Univ., Columbus, OH (United States); Ford Motor Company, Dearborn, MI (United States)
- Nanjing University of Aeronautics and Astronautics (China)
- Northwestern Univ., Evanston, IL (United States)
- Chongqing University (China)
- Univ. of Michigan, Dearborn, MI (United States)
- Ford Motor Company, Dearborn, MI (United States)
- Publication Date:
- Research Org.:
- Ford Motor Company, Detroit, MI (United States)
- Sponsoring Org.:
- USDOE Office of Energy Efficiency and Renewable Energy (EERE), Vehicle Technologies Office (EE-3V)
- OSTI Identifier:
- 1504747
- Grant/Contract Number:
- EE0006867
- Resource Type:
- Accepted Manuscript
- Journal Name:
- Composites Part B: Engineering
- Additional Journal Information:
- Journal Volume: 167; Journal Issue: C; Journal ID: ISSN 1359-8368
- Publisher:
- Elsevier
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING; 97 MATHEMATICS AND COMPUTING; Cross-ply laminates; Longitudinal compression; Kink band; Constraining effect; Hybrid micro-macro model
Citation Formats
Sun, Qingping, Zhou, Guowei, Guo, Haiding, Meng, Zhaoxu, Chen, Zhangxing, Liu, Haolong, Kang, Hongtae, and Su, Xuming. Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses. United States: N. p., 2018.
Web. doi:10.1016/j.compositesb.2018.12.041.
Sun, Qingping, Zhou, Guowei, Guo, Haiding, Meng, Zhaoxu, Chen, Zhangxing, Liu, Haolong, Kang, Hongtae, & Su, Xuming. Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses. United States. https://doi.org/10.1016/j.compositesb.2018.12.041
Sun, Qingping, Zhou, Guowei, Guo, Haiding, Meng, Zhaoxu, Chen, Zhangxing, Liu, Haolong, Kang, Hongtae, and Su, Xuming. Wed .
"Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses". United States. https://doi.org/10.1016/j.compositesb.2018.12.041. https://www.osti.gov/servlets/purl/1504747.
@article{osti_1504747,
title = {Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses},
author = {Sun, Qingping and Zhou, Guowei and Guo, Haiding and Meng, Zhaoxu and Chen, Zhangxing and Liu, Haolong and Kang, Hongtae and Su, Xuming},
abstractNote = {Here, this study investigates the failure mechanisms of cross-ply laminates subjected to longitudinal compressive loading. A sequence of failure initiation and propagation process is observed based on optical microscopy images of failed specimens. Specifically, the failure process in the cross-ply laminates involves a combination of four failure mechanisms: fiber kinking, delamination, matrix cracking, and fiber/matrix splitting. We find that the kink-bands in the middle 0° plies of the cross-ply laminates most often show a wedge shape and the angle of matrix cracks in the 90° plies is slightly larger than that of pure 90° plies. The reason has been attributed to the constraining effects by the adjacent plies. The next focus of this study is to propose hybrid micro-macro models to more systematically study the failure mechanisms of the cross-ply laminates. We show that these models accurately predict the combined failure modes of the cross-ply laminates and enable us to closely investigate the interactions of different failure mechanisms. More importantly, the hybrid models achieve great computational efficiency compared to full-scale microstructural models. Finally, the combined experimental and computational analyses presented here provide a new level of understanding of the kink-band morphology and damage mechanisms in the cross-ply laminates.},
doi = {10.1016/j.compositesb.2018.12.041},
journal = {Composites Part B: Engineering},
number = C,
volume = 167,
place = {United States},
year = {Wed Dec 12 00:00:00 EST 2018},
month = {Wed Dec 12 00:00:00 EST 2018}
}
Web of Science
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