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      Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures

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          Abstract

          Cycle-dependent damage evolution in self-healing, 2.5D woven Hi-Nicalon TM SiC/[Si-B-C] and 2D woven Hi-Nicalon TM SiC/[SiC-B 4C] ceramic-matrix composites (CMCs) at 600 and 1200 °C was investigated. The cycle-dependent damage parameters of internal friction, dissipated energy, Kachanov’s damage parameter, and broken fiber fraction were obtained to describe damage development in self-healing CMCs. The relationships between cycle-dependent damage parameters and multiple fatigue damage mechanisms were established. The experimental fatigue damage development of self-healing Hi-Nicalon TM SiC/[Si-B-C] and Hi-Nicalon TM SiC/[SiC-B 4C] composites was predicted for different temperatures, peak stresses, and loading frequencies. The cycle-dependent damage evolution of self-healing Hi-Nicalon TM SiC/[Si-B-C] and Hi-Nicalon TM SiC/[SiC-B 4C] composites depends on temperature, testing environment, peak stress, and loading frequency. For the Hi-Nicalon TM SiC/[Si-B-C] composite, temperature is a governing parameter for the fatigue process. At an elevated temperature of 600 °C in an air atmosphere, the internal frictional parameter of Hi-Nicalon TM SiC/[Si-B-C] composite decreases first and then increases with applied cycle number; however, at an elevated temperature of 1200 °C in an air atmosphere, the internal frictional parameter of Hi-Nicalon TM SiC/[Si-B-C] composite decreases with applied cycle number, and the interface shear stress at 1200 °C is much lower than that at 600 °C. For Hi-Nicalon TM SiC/[SiC-B 4C] composite at 1200 °C, loading frequency is a governing parameter for the fatigue process. The degradation rate of interface shear stress is much higher at the loading frequency of 0.1 Hz than that at the loading frequency of 1 Hz.

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          Most cited references38

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          Advanced structural ceramics in aerospace propulsion.

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                Author and article information

                Journal
                Materials (Basel)
                Materials (Basel)
                materials
                Materials
                MDPI
                1996-1944
                24 March 2020
                March 2020
                : 13
                : 6
                : 1478
                Affiliations
                [1 ]College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, No.29, Yudao St., Nanjing 210016, China
                [2 ]Université de Lyon, INSA-Lyon, MATEIS (UMR CNRS 5510), 7 Avenue Jean Capelle, 69621 Villeurbanne Cedex, France; pascal.reynaud@ 123456insa-lyon.fr (P.R.); gilbert.fantozzi@ 123456insa-lyon.fr (G.F.)
                Author notes
                [* ]Correspondence: llb451@ 123456nuaa.edu.cn ; Tel.: +86-25-8489-5963
                Author information
                https://orcid.org/0000-0002-7689-2098
                Article
                materials-13-01478
                10.3390/ma13061478
                7143090
                32214023
                dd27fa2e-c017-4466-8fea-773351d74195
                © 2020 by the authors.

                Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license ( http://creativecommons.org/licenses/by/4.0/).

                History
                : 29 January 2020
                : 18 March 2020
                Categories
                Article

                ceramic-matrix composites (cmcs),self-healing,cycle-dependent,damage evolution,damage parameters,internal friction,interface damage,fiber failure

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