Effect of layer thickness of prepreg on tensile properties of quasi-isotropic carbon fiber reinforced polyamide 6
Author:
Affiliation:
1. Headquarters for Innovative Society-Academia Cooperation, University of Fukui
2. Research Center for Fibers and Materials, University of Fukui
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/88/910/88_22-00073/_pdf
Reference17 articles.
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2. Hine, P. J., Brew, B., Duckett, R. A. and Wardet, I. M., Failure mechanisms in continuous carbon-fibre reinforced PEEK composites, Composites Science and Technology, Vol. 35 (1989), pp.31-51.
3. Hirai, T., Semba, T. and Tarui, M., Three-Dimensional Interlaminar Stress Distribution in Symmetric Composite Laminate, Proceedings of Fourth International Conference on Composite Materials, ICCM-IV, Japan Society for Composite materials, Oct. 25-27 (1982), pp.243-250.
4. Kageyama, K., Kato, T. and Abe, S., Proposal of a new analytical procedure for transverse lamina cracking in multidirectionally laminated composites, Journal of the Japan Society for Composite Materials, Vol.28, No.1 (2002), pp.11-20 (in Japanese).
5. Kanesaki, M., Saito, H., Tanaka, M., Hojo, M. and Kimpara, I., Improvement of CAI Strength and Its Mechanisms on CFRTP Laminate with Thinning in Ply-thickness, Journal of the Japan Society for Composite Materials, Vol. 39, No. 3 (2013), pp.89-98 (in Japanese).
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1. Effect of layer thickness of prepreg and fiber/matrix interfacial properties on impact resistance of carbon fiber reinforced polyamide 6;Transactions of the JSME (in Japanese);2023
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