Repair of Interfacial De-bonding in a Single Carbon Fiber/PP Model Composite by Means of Selective Direct Heating of Carbon Fiber Inside
Author:
Affiliation:
1. Composite Materials Research Center., Gifu Univ.
2. Graduate School of Eng., Dept. of Mechanical Eng., Gifu Univ.
3. Nagoya Municipal Industrial Research Institute
Publisher
Society of Materials Science, Japan
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Link
https://www.jstage.jst.go.jp/article/jsms/70/9/70_663/_pdf
Reference20 articles.
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2. 2) G. Williams, R. Trask and I. Bond, “A self-healing carbon fibre reinforced polymer for aerospace applications”, Composites: Part A, Vol.38, pp.1525–1532 (2007).
3. 3) K. Sanada, T. Suyama and Y. Nassho, “Interlaminar shear strength and self-healing of spread carbon fiber/epoxy laminates containing microcapsules”, Journal of the Society of Materials Science, Japan, Vol.66, No.4, pp.299-305 (2017).
4. 4) G. Reyes and U. Sharma, “Modeling and damage repair of woven thermoplastic composites subjected to low velocity impact”, Composite Structures, Vol.92, pp.523-531 (2010).
5. 5) M. Kanesaki, C. Uchijo, M. Tanaka, H. Saito, M. Nishikawa, M. Hojo and I. Kimpara, “Repair of impact damage by thermal fusion bonding and recovery of residual compressive strength on CF/PA6 laminates”, Journal of Japan Society for Composite Materials, Vol.41, No. 1, pp.33-44 (2015).
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