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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University of Chemistry and Technology, Prague
2019-07-01
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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
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work_keys_str_mv |
AT longbiaoli temperaturedependentproportionallimitstressofcarbonfiberreinforcedsiliconcarbideceramicmatrixcomposites |
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