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首页> 外文期刊>Journal of Reinforced Plastics and Composites >Experimental study on flexural fatigue behavior of glass fibers/epoxy hybrid composites with statistical analysis
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Experimental study on flexural fatigue behavior of glass fibers/epoxy hybrid composites with statistical analysis

机译:统计分析法研究玻璃纤维/环氧混杂复合材料弯曲疲劳行为的实验研究

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Flexural fatigue behaviors were investigated experimentally for unidirectional glass fiber (U)/random glass fiber (R)/epoxy hybrid composite laminates. Three different hybrid composites, i.e. [0.5R/U/U]_S, [U/0.5R/U]_S and [U/U/0.5R]_S were fabricated using hand lay-up technique with 37% total fiber volume fraction (V_(fT)), unidirectional glass fiber relative volume fraction (V_(fU)/V_(fT)) = 0.8 and of 5.5 ±0.2 mm thickness. Flexural fatigue tests were performed at zero mean stress. A 20% reduction of the flexural stiffness was taken as a failure criterion. The effects of layer stacking sequences on both initial stress-no. of cycles to failure relationships and the relative surface temperature increase of the mentioned composites were investigated. The specimen failure modes have been recorded and discussed. The S-N curves and fatigue safe workability areas for the fabricated hybrid composites have been constructed as design curves. Two-parameter Weibull distribution function was used to obtain the scatter in the experimental results and to construct the reliability graphs for the fabricated hybrid composites.
机译:实验研究了单向玻璃纤维(U)/无规玻璃纤维(R)/环氧混合复合材料层压板的弯曲疲劳行为。使用手工铺网技术制造了三种不同的混合复合材料,即[0.5R / U / U] _S,[U / 0.5R / U] _S和[U / U / 0.5R] _S,总纤维体积分数为37% (V_(fT)),单向玻璃纤维相对体积分数(V_(fU)/ V_(fT))= 0.8,厚度为5.5±0.2毫米。在零平均应力下进行弯曲疲劳测试。弯曲刚度降低20%被视为破坏标准。层堆叠顺序对两个初始无应力的影响。研究了与上述复合材料的失效关系的循环和相对表面温度的升高。样本破坏模式已被记录和讨论。所制造的混合复合材料的S-N曲线和疲劳安全可加工性区域已作为设计曲线构建。利用两参数威布尔分布函数获得了实验结果中的散射,并构建了所制备的混杂复合材料的可靠性图。

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