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Notch Sensitivity on Fatigue Behavior of Carbon-Carbon Composites

机译:碳碳复合材料疲劳行为的缺口敏感性

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The fatigue strengths in notched specimens of carbon-carbon composites were investigated. Slits of different length were cut on both sides of a test section to investigate the impact of notch sensitivity on fatigue life. Specimens with blunt-notches on the both side of the specimen, and center hole were also used to compare the critical stress, σw. The fatigue limit was measured using S-N curves. From the experimental result, it was found that specimens with blunt-notches have lowest fatigue limit. The relationships between critical stress, σw and specimen geometry were investigated by stress concentration factor, Kt and stress intensity factor, KI which was done two dimensional body forced methods. Consequently, it was discussed that the damage condition in the vicinity of the notch or slit, and the crack initiation behavior affects the fatigue strength. Also, the S-N curve and fatigue limit was related to the crack growth in shear mode.
机译:研究了碳 - 碳复合材料缺口标本的疲劳强度。 在试验部分的两侧切割不同长度的狭缝,以研究缺口敏感性对疲劳寿命的影响。 样品上两侧的具有钝槽的标本和中心孔也用于比较临界应力σw。 使用S-N曲线测量疲劳极限。 从实验结果来看,发现具有钝缺口的标本具有最低的疲劳极限。 通过应力浓度因子,Kt和应力强度因子,Ki进行了两维身体强制方法,研究了临界应力,σw和样本几何形状的关系。 因此,讨论了凹口或狭缝附近的损伤条件,并且裂纹引发行为影响疲劳强度。 而且,S-N曲线和疲劳极限与剪切模式的裂缝生长有关。

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