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首页> 外文期刊>Polymer Composites >Hygrothermal degradation of the composite laminates from woven carbon/SC-15 epoxy resin and woven glass/SC-15 epoxy resin
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Hygrothermal degradation of the composite laminates from woven carbon/SC-15 epoxy resin and woven glass/SC-15 epoxy resin

机译:碳纤维/ SC-15环氧树脂和玻璃纤维/ SC-15环氧树脂对复合层压板的湿热降解

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摘要

The degradation mechanism for hygrothermal aging of woven carbon-epoxy and woven glass-epoxy composite laminates was investigated in the micro-scale. Interlaminar shear and cross laminar flexural tests were performed on notched and unnotched specimens to know the mechanical performance of the composite laminates. The Interlaminar Shear Stress (ISS) for both the composites was also evaluated and correlated with the number of hygrothermal cycles. Four-point bending and tensile or compression shear loading configurations were also used. The stress at the onset of delamination (Delamination Damage Tolerance, DDT) was identified from the load-deflection curve of the flexural specimens and correlated with the number of hygrothermal cycles. It was found that both the ISS and DDT decrease with the exposure time. Dimensional stability was almost unchanged throughout the aging process, although there was a very little moisture absorption (similar to 1.3%) in glass-epoxy and carbon-epoxy composite laminates. SEM photomicrographs of the delaminated surface show that failure occurs suddenly in a macroscopically brittle mode by crack initiation and propagation method.
机译:在微观尺度上研究了编织碳-环氧树脂和编织玻璃-环氧树脂复合层压板湿热老化的降解机理。在有缺口和无缺口的样品上进行层间剪切和交叉层弯曲测试,以了解复合材料层压板的机械性能。还评估了两种复合材料的层间剪切应力(ISS),并将其与湿热循环次数相关联。还使用了四点弯曲和拉伸或压缩剪切载荷配置。从挠曲试样的载荷-挠度曲线确定了分层开始时的应力(分层损伤容限,DDT),并将其与湿热循环次数相关联。发现ISS和DDT都随着暴露时间而降低。尽管在玻璃环氧和碳环氧复合材料层压板中吸湿率很小(约1.3%),但在整个老化过程中尺寸稳定性几乎没有变化。脱层表面的SEM显微照片显示,通过裂纹萌生和扩展方法,宏观脆性破坏是突然发生的。

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