Damage coupling mechanical behaviors of 2D-SiC/SiC composite

By using axial and off-axis loading tests with off-axis angle as 45°, the tensile, compressive and in-plane shear stress-strain behaviors along the fiber bundles directions of a 2D-SiC/SiC composite were obtained, and the damage coupling mechanical behaviors of composite under combined stress condit...

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Main Authors: GUO Hong-bao, XIE Jun
Format: Article
Language:zho
Published: Journal of Materials Engineering 2019-10-01
Series:Journal of Materials Engineering
Subjects:
Online Access:http://jme.biam.ac.cn/CN/Y2019/V47/I10/160
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spelling doaj-fdb5c1afff58456ab7041fffec0551442020-11-25T01:08:10ZzhoJournal of Materials EngineeringJournal of Materials Engineering1001-43811001-43812019-10-01471016016510.11868/j.issn.1001-4381.2018.000674201910000674Damage coupling mechanical behaviors of 2D-SiC/SiC compositeGUO Hong-bao0XIE Jun1AECC Commercial Aircraft Engine Co., Ltd., Shanghai 201108, ChinaAECC Commercial Aircraft Engine Co., Ltd., Shanghai 201108, ChinaBy using axial and off-axis loading tests with off-axis angle as 45°, the tensile, compressive and in-plane shear stress-strain behaviors along the fiber bundles directions of a 2D-SiC/SiC composite were obtained, and the damage coupling mechanical behaviors of composite under combined stress condition were studied. The results show that the initial stress levels for the damage coupling mechanical behaviors of composite under 45° off-axis tensile and compressive loading conditions are 40MPa and -110MPa, separately. Under combined stress conditions, there exists obvious mutual acceleration between the tensile and the in-plane shear damage evolutions in the fibre bundles directions of composite, and the in-plane shear damage has accelerative effect on the compressive damage evolution, but the in-plane shear damage evolution is suppressed by compressive stress components obviously. These coupling effects become more significant with increasing stress level. The SEM (scanning electron microscope) pictures of fractured surfaces on off-axis loading specimens indicate that, in the fiber bundles directions, the mutual effects between the three stress components and the cracking evolutions of the three kinds of matrix cracks (oriented at 0°, 90° and 45°) are the main micro-damage mechanisms for the damage coupling mechanical behaviors of 2D-SiC/SiC composite under combined stress conditions.http://jme.biam.ac.cn/CN/Y2019/V47/I10/1602d-sic/sic compositestress-strain behaviorcombined stress conditiondamage coupling
collection DOAJ
language zho
format Article
sources DOAJ
author GUO Hong-bao
XIE Jun
spellingShingle GUO Hong-bao
XIE Jun
Damage coupling mechanical behaviors of 2D-SiC/SiC composite
Journal of Materials Engineering
2d-sic/sic composite
stress-strain behavior
combined stress condition
damage coupling
author_facet GUO Hong-bao
XIE Jun
author_sort GUO Hong-bao
title Damage coupling mechanical behaviors of 2D-SiC/SiC composite
title_short Damage coupling mechanical behaviors of 2D-SiC/SiC composite
title_full Damage coupling mechanical behaviors of 2D-SiC/SiC composite
title_fullStr Damage coupling mechanical behaviors of 2D-SiC/SiC composite
title_full_unstemmed Damage coupling mechanical behaviors of 2D-SiC/SiC composite
title_sort damage coupling mechanical behaviors of 2d-sic/sic composite
publisher Journal of Materials Engineering
series Journal of Materials Engineering
issn 1001-4381
1001-4381
publishDate 2019-10-01
description By using axial and off-axis loading tests with off-axis angle as 45°, the tensile, compressive and in-plane shear stress-strain behaviors along the fiber bundles directions of a 2D-SiC/SiC composite were obtained, and the damage coupling mechanical behaviors of composite under combined stress condition were studied. The results show that the initial stress levels for the damage coupling mechanical behaviors of composite under 45° off-axis tensile and compressive loading conditions are 40MPa and -110MPa, separately. Under combined stress conditions, there exists obvious mutual acceleration between the tensile and the in-plane shear damage evolutions in the fibre bundles directions of composite, and the in-plane shear damage has accelerative effect on the compressive damage evolution, but the in-plane shear damage evolution is suppressed by compressive stress components obviously. These coupling effects become more significant with increasing stress level. The SEM (scanning electron microscope) pictures of fractured surfaces on off-axis loading specimens indicate that, in the fiber bundles directions, the mutual effects between the three stress components and the cracking evolutions of the three kinds of matrix cracks (oriented at 0°, 90° and 45°) are the main micro-damage mechanisms for the damage coupling mechanical behaviors of 2D-SiC/SiC composite under combined stress conditions.
topic 2d-sic/sic composite
stress-strain behavior
combined stress condition
damage coupling
url http://jme.biam.ac.cn/CN/Y2019/V47/I10/160
work_keys_str_mv AT guohongbao damagecouplingmechanicalbehaviorsof2dsicsiccomposite
AT xiejun damagecouplingmechanicalbehaviorsof2dsicsiccomposite
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