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Effect of interlayer carbon fiber dispersion on the low-velocity impact performance of woven flax-carbon hybrid composites

机译:层间碳纤维分散体对编织亚麻碳杂化复合材料低速冲击性能的影响

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This work investigates the effects of interlayer hybrid fiber dispersion on the impact response of carbon-flax epoxy hybrid laminates at low carbon volume fractions, and benchmarks the mechanical performance enhancement against the non-hybrid flax epoxy. Five hybrid laminate stacking sequences with similar carbon-to-flax weight ratio were fabricated and subjected to low-velocity impact at three different energy values, generating non-perforated and perforated damage states. A virtual drop-weight impact test that models intralaminar failure based on continuum damage mechanics approach, and delamination using cohesive elements, was also implemented to evaluate the material behavior and damage development in the composites. Simulation results were then verified against experimental data. Results suggested that positioning stiffer carbon plies at the impact face does not necessarily lead to enhancement of the hybrid's impact properties. On the contrary, flax plies at the impacted side lead to significant improvement in impact resistance compared to the non-hybrid flax composite with similar thickness. Results of finite element analysis showed that carbon plies play a significant role in the hybrid laminate's energy absorption characteristics due to lower failure strain.
机译:该作品研究了层间杂化纤维分散体对低碳体积分数碳 - 亚麻环氧杂交层压板的影响响应的影响,并对非杂交亚麻环氧树脂进行了力学性能增强的基准。制造具有相似碳 - 亚麻重量比的五种杂化层压堆叠序列,并在三种不同的能量值下进行低速冲击,产生非穿孔和穿孔损伤状态。还实施了基于连续损伤力学方法的历史内失败的虚拟滴重建测试,以及使用粘性元素的分层,以评估复合材料中的材料行为和损伤。然后针对实验数据验证模拟结果。结果表明,在冲击面上定位碳层的定位不一定导致杂交的影响性的增强。相反,与具有相似厚度相似的非杂交亚麻复合材料相比,撞击侧的亚麻帘布层导致抗冲击性的显着改善。有限元分析结果表明,由于较低的故障菌株,碳层在杂交层压板的能量吸收特性中发挥着重要作用。

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