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MD Modeling of Epoxy-base Nanocomposites Reinforced with Functionalized Graphene Nanoplatelets

机译:用官能化石墨烯纳米孔增强环氧基纳米复合材料的MD建模

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The impact on the mechanical properties of aerospace epoxy materials reinforcedwith pristine Graphene Nanoplatelets (GNP), highly concentrated Graphene Oxide(GO), and Functionalized Graphene Oxide (FGO) has been investigated in this study.Molecular Dynamics (MD) using a reactive force field (ReaxFF) has been employedin predicting the effective mechanical properties of the interphase region of the threeproposed nanocomposite materials at the nanoscale level. A systematiccomputational approach to simulate the reinforcing nanoplatelets and probe theirinfluence on the mechanical properties of the epoxy matrix are included in this study.The nanoscale outcome indicates a significant degradation in the in-plane elasticYoung’s (decreased by ~89%) and shear (decreased by ~72.5%) moduli of thenanocomposite when introducing large amounts of oxygen and functional groups tothe robust sp2 structure of the GNP. However, the wrinkled morphology of GO andFGO improves the nanoplatelet-matrix interlocking mechanism which produces asignificant improvement in the out-of-plane shear modulus (increased by ~95%). Theinfluence of the nanoplatelet content and aspect ratio on the mechanical response ofthe nanocomposites has also been determined in this study. Generally, the predictedmechanical response of the bulk nanocomposite materials demonstrates animprovement with increasing nanoplatelet content and aspect ratio. The results showgood agreement with experimental data available from the literature.
机译:对航空航天环氧材料力学性能的影响加固用原始石墨烯纳米缩素(GNP),高度浓缩的石墨烯氧化物(GO)和官能化的石墨烯氧化物(FGO)已经在本研究中进行了研究。使用了使用反应力场(Reaxff)的分子动力学(MD)在预测三个间隔区域的有效机械性能方面在纳米级水平下提出的纳米复合材料。一个系统的模拟增强纳米孔的计算方法和探针本研究包括对环氧基质的力学性质的影响。纳米级结果表明在面内弹性中的显着降解杨(减少〜89%)和剪切(减少〜72.5%)模态纳米复合材料在引入大量氧气和官能团时GNP的鲁棒SP2结构。然而,去的皱纹形态FGO改善了生产A的纳米锁型 - 矩阵互锁机构平面外剪切模量的显着改善(增加〜95%)。这纳米片含量和纵横比对机械响应的影响纳米复合材料也已经在本研究中确定。一般来说,预测散装纳米复合材料的机械响应表明了一个随着纳米片含量增加和纵横比而改善。结果表明与文献提供的实验数据吻合良好。

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