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Mixed-mode I/II delamination fatigue strengthening of polymer composites using z-pins

机译:使用Z销的聚合物复合材料的混合模式I / II分层疲劳增强

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摘要

An experimental investigation is presented into the improvement to the delamination fatigue resistant properties of z-pinned carbon fibre epoxy composite under mixed-mode I/II cyclic interlaminar loading. Delamination fatigue tests are performed on unpinned and z-pinned composites under different mixed mode ratios spanning mode I to mode II interlaminar cyclic conditions. The fatigue resistance and fatigue strengthening mechanisms induced by the z-pins is dependent on the cyclic mixed-mode ratio. The threshold critical strain energy release rate needed to initiate delamination growth in the z-pinned composite increases with the G(I)-to-G(II) ratio. The fatigue crack growth rate slows considerably and the critical strain energy release rate for fast fatigue fracture increases with the G(I)-to-G(II) ratio. The delamination fatigue strengthening induced by the z-pins increases with the G(I)-to-G(II) ratio due to a transition in the crack bridging toughening process from pin pull-out under mode I dominated loads to combined tensile and shear fracture under mixed-mode loads to pin shear rupture under mode II dominated loads. It is also found that the effect of the G(I)-to-G(II) ratio on the fatigue properties is greater for the z-pinned composite compared to the unpinned laminate due to the high fatigue sensitivity of z-pins to the mixed mode ratio. (C) 2017 Elsevier Ltd. All rights reserved.
机译:进行了实验研究,以改善在混合模式I / II循环层间负载下z钉扎碳纤维环氧复合材料的抗分层疲劳性能。在跨越模式I到模式II层间循环条件的不同混合比下,对未固定和Z固定的复合材料执行分层疲劳测试。 z销引起的抗疲劳性和疲劳增强机制取决于循环混合模数比。启动Z钉复合材料中的分层生长所需的阈值临界应变能释放速率随G(I)与G(II)的比率增加而增加。疲劳裂纹的增长速度大大降低,而快速疲劳断裂的临界应变能释放速率随G(I)与G(II)的比值而增加。由于裂纹桥接增韧过程从模式I主导下的销钉拔出过渡到拉伸和剪力组合的过渡,由z销引起的脱层疲劳强度随G(I)与G(II)的比率增加而增加在混合模式载荷作用下发生断裂,而在II型控制载荷作用下发生销钉剪切断裂。还发现与未钉叠层相比,z钉复合材料的G(I)与G(II)比对疲劳性能的影响更大,这是因为z钉对复合材料的高疲劳敏感性混合模式比率。 (C)2017 Elsevier Ltd.保留所有权利。

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  • 来源
    《Composites》 |2017年第8期|219-226|共8页
  • 作者单位

    RMIT Univ, Sch Engn, Sir Lawrence Wackett Aerosp Res Ctr, GPO Box 2476, Melbourne, Vic 3001, Australia;

    RMIT Univ, Sch Engn, Sir Lawrence Wackett Aerosp Res Ctr, GPO Box 2476, Melbourne, Vic 3001, Australia;

    RMIT Univ, Sch Engn, Sir Lawrence Wackett Aerosp Res Ctr, GPO Box 2476, Melbourne, Vic 3001, Australia;

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