TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES

In this paper, the temperature-dependent proportional limit stress of carbon fiber-reinforced silicon carbide ceramic-matrix composites (C/SiC CMCs) is investigated using the energy balance approach. The temperature-dependent micromechanical parameters of fiber and matrix modulus, fiber/matrix inter...

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Main Author: Longbiao Li
Format: Article
Language:English
Published: University of Chemistry and Technology, Prague 2019-07-01
Series:Ceramics-Silikáty
Subjects:
Online Access: http://www.ceramics-silikaty.cz/index.php?page=cs_detail_doi&id=1281
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spelling doaj-9af66e985b4c4f87a8f49a08b56b1e2c2020-11-25T01:29:45ZengUniversity of Chemistry and Technology, PragueCeramics-Silikáty0862-54681804-58472019-07-0163333033710.13168/cs.2019.002810.13168/cs.2019.0028.20190917123736TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITESLongbiao Li0 College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, No.29 Yudao St., Nanjing 210016, PR China In this paper, the temperature-dependent proportional limit stress of carbon fiber-reinforced silicon carbide ceramic-matrix composites (C/SiC CMCs) is investigated using the energy balance approach. The temperature-dependent micromechanical parameters of fiber and matrix modulus, fiber/matrix interface shear stress and interface debonded energy, and matrix fracture energy are incorporated into the analysis of the micro stress analysis, fiber/matrix interface debonding criterion and energy balance approach. The relationships between the proportional limit stress, fiber/matrix interface debonding and temperature are established. The effects of fiber volume fraction, fiber/matrix interface shear stress, interface frictional coefficient, interface debonded energy and matrix fracture energy on the proportional limit stress and fiber/matrix interface debonding length versus temperature curves are discussed. The experimental proportional limit stress and fiber/matrix interface debonding length of 2D C/SiC composite at elevated temperatures of 973K and 1273K are predicted. For C/SiC composite, the proportional limit stress of C/SiC composite increases with temperature, due to the increasing of fiber/matrix interface shear stress and decreasing of the thermal residual stress. http://www.ceramics-silikaty.cz/index.php?page=cs_detail_doi&id=1281 Ceramic-matrix composites (CMCs) Proportional limit stress Interface debonding.
collection DOAJ
language English
format Article
sources DOAJ
author Longbiao Li
spellingShingle Longbiao Li
TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
Ceramics-Silikáty
Ceramic-matrix composites (CMCs)
Proportional limit stress
Interface debonding.
author_facet Longbiao Li
author_sort Longbiao Li
title TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
title_short TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
title_full TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
title_fullStr TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
title_full_unstemmed TEMPERATURE-DEPENDENT PROPORTIONAL LIMIT STRESS OF CARBON FIBER-REINFORCED SILICON CARBIDE CERAMIC-MATRIX COMPOSITES
title_sort temperature-dependent proportional limit stress of carbon fiber-reinforced silicon carbide ceramic-matrix composites
publisher University of Chemistry and Technology, Prague
series Ceramics-Silikáty
issn 0862-5468
1804-5847
publishDate 2019-07-01
description In this paper, the temperature-dependent proportional limit stress of carbon fiber-reinforced silicon carbide ceramic-matrix composites (C/SiC CMCs) is investigated using the energy balance approach. The temperature-dependent micromechanical parameters of fiber and matrix modulus, fiber/matrix interface shear stress and interface debonded energy, and matrix fracture energy are incorporated into the analysis of the micro stress analysis, fiber/matrix interface debonding criterion and energy balance approach. The relationships between the proportional limit stress, fiber/matrix interface debonding and temperature are established. The effects of fiber volume fraction, fiber/matrix interface shear stress, interface frictional coefficient, interface debonded energy and matrix fracture energy on the proportional limit stress and fiber/matrix interface debonding length versus temperature curves are discussed. The experimental proportional limit stress and fiber/matrix interface debonding length of 2D C/SiC composite at elevated temperatures of 973K and 1273K are predicted. For C/SiC composite, the proportional limit stress of C/SiC composite increases with temperature, due to the increasing of fiber/matrix interface shear stress and decreasing of the thermal residual stress.
topic Ceramic-matrix composites (CMCs)
Proportional limit stress
Interface debonding.
url http://www.ceramics-silikaty.cz/index.php?page=cs_detail_doi&id=1281
work_keys_str_mv AT longbiaoli temperaturedependentproportionallimitstressofcarbonfiberreinforcedsiliconcarbideceramicmatrixcomposites
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