Change in Interlayer Strength and Fracture Toughness of Carbon-Carbon Composite Material under the Impact of Cyclic Loads
- 作者: Stepashkin A.A.1, Ozherelkov D.Y.1, Sazonov Y.B.1, Komissarov A.A.1, Mozalev V.V.2
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隶属关系:
- National University of Science and Technology MISiS
- OAO Rubin Aviation Corporation
- 期: 卷 10, 编号 1 (2019)
- 页面: 155-161
- 栏目: Article
- URL: https://journals.rcsi.science/2075-1133/article/view/207799
- DOI: https://doi.org/10.1134/S2075113319010301
- ID: 207799
如何引用文章
详细
The effect of low-cycle fatigue loading on interlayer strength and fracture toughness of discretely reinforced carbon-carbon composite material (CCCM) for friction use is studied. The material demonstrates good resistance to fatigue loads. In the described mechanisms for increasing CCCM fracture toughness after applying fatigue load, the fiber–matrix interface plays a key part. The dependences of CCCM fracture toughness and interlayer strength on the fatigue loading parameters are determined.
作者简介
A. Stepashkin
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow
D. Ozherelkov
National University of Science and Technology MISiS
编辑信件的主要联系方式.
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow
Yu. Sazonov
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow
A. Komissarov
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow
V. Mozalev
OAO Rubin Aviation Corporation
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Balashikha
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