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Title: 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:
 [1];  [2];  [3]; ORCiD logo [4];  [5];  [3];  [6];  [7]
  1. Nanjing University of Aeronautics and Astronautics (China); Ford Motor Company, Dearborn, MI (United States)
  2. The Ohio State Univ., Columbus, OH (United States); Ford Motor Company, Dearborn, MI (United States)
  3. Nanjing University of Aeronautics and Astronautics (China)
  4. Northwestern Univ., Evanston, IL (United States)
  5. Chongqing University (China)
  6. Univ. of Michigan, Dearborn, MI (United States)
  7. 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}
}

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Works referencing / citing this record:

Effect of thickness variation on static behaviour of carbon fiber reinforced polymer multidirectional laminated composite
journal, September 2019

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