Experimental investigation of CFRP fracture toughness by delamination type
- Authors: Chernyakin S.A.1
-
Affiliations:
- Samara National Research University
- Issue: Vol 20, No 1 (2021)
- Pages: 97-108
- Section: MECHANICAL ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/8651
- DOI: https://doi.org/10.18287/2541-7533-2021-20-1-97-108
- ID: 8651
Cite item
Full Text
Abstract
The results of analyzing fracture toughness in carbon fiber-reinforced plastics by the type of delamination are presented in the article. The goal of this paper is investigation of delamination propagation process and fracture mechanics parameters in modern CFRPs. This type of composite materials is extensively used in high load aerospace structures. Modern polymer composite materials are the subject of our research. A technique of manufacturing specimens for testing by the vacuum infusion process is presented in the paper. Experimental investigation of delamination propagation process by mode I and II was performed with the aid of up-to-date testing equipment using a special type of specimens such as a double cantilever beam. Researchers usually use this type of specimen for the validation of their numerical models. Critical values of energy release rate and load-displacement curves were obtained for two types of material – unidirectional and woven. Examination of microscopic sections of the tested specimens using an optical microscope allowed us to identify the specific fracture mechanisms of material structure.
About the authors
S. A. Chernyakin
Samara National Research University
Author for correspondence.
Email: chernyakin-sa@mail.ru
ORCID iD: 0000-0002-8796-7833
Senior Lecturer of the Department of Space Engineering named after Chief Designer D.I. Kozlov
Russian FederationReferences
- ASTM D5528-13. Method for mode i interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. ASTM International, West Conshohocken, PA, 2013. doi: 10.1520/D5528-13
- Berry J.P. Determination of fracture surface energies by the cleavage technique. Journal of Applied Physics. 1963. V. 34, Iss. 1. P. 62-68. doi: 10.1063/1.1729091
- Hashemi S., Kinloch A.J., Williams J.G. Corrections needed in double-cantilever beam tests for assessing the interlaminar failure of fibre-composites. Journal of Materials Science Letters. 1989. V. 8, Iss. 2. P. 125-129. doi: 10.1007/BF00730701
- Nasuha N., Azmi A.I., Tan C.L. A review on mode-I interlaminar fracture toughness of fibre reinforced composites. Journal of Physics: Conference Series. 2017. V. 908, Iss. 1. doi: 10.1088/1742-6596/908/1/012024
- Zhu X.K., Joyce J.A. Review of fracture toughness (G, K, J, CTOD, CTOA) testing and standardization. Engineering Fracture Mechanics. 2012. V. 85. P. 1-46. doi: 10.1016/j.engfracmech.2012.02.001
- ASTM D7905 / D7905M-19e1. Standard test method for determination of the mode II interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. ASTM International, West Conshohocken, PA, 2019. doi: 10.1520/D7905_D7905M-19E01
- Russell A.J., Street K.N. Factors affecting the interlaminar fracture energy of graphite/epoxy laminates. Proceedings of the 4th International Conference on Composite Materials «Progress in Science and Engineering of Composites» (Oct. 25-28, 1982, Tokyo, Japan). P. 279-286.
- Vu‐Khanh T. Crack‐arrest study in mode II delamination in composites. Polymer Composites. 1987. V. 8, Iss. 5. P. 331-341. doi: 10.1002/pc.750080508
- Kageyama K., Kikuchi M., Yanagisawa N. Stabilized end notched flexure test: characterization of mode II interlaminar crack growth. Third Symposium on Composite Materials: Fatigue and Fractur (November, 6-7, 1989, Lake Buena Vista, FL, USA). P. 210-225. doi: 10.1520/STP17720S