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Finite element based micromechanical modeling of periodic composite microstructures

机译:基于有限元的周期复合微结构微观力学建模

摘要

The mechanical behavior of cellular solids, including stiffness and strength, can be tuned by tailoring the underlying geometry and material constituents of the microstructure. Here the effect of key parameters on the compressive deformation response of composite truss-based cellular solids was investigated. A simple periodic geometry was chosen and studied using finite element based micromechanical models. Simulations were conducted parametrically varying the volume fraction with a fixed strut length, the proportion of the polymer coating to the elastomer core used in the composite struts (coating fraction), and the size of the representative volume element (layer number). An analytical model based on energy methods for buckling columns with elastic restraints was also derived and compared to the simulation data. Materials were then fabricated using 3D printing and then tested in compression. Numerical and experimental results are compared. The simulations showed that an increase in volume fraction with coating fraction and layer number held constant increased the modulus in a linear manner, and increased the peak stress with a nonlinear dependence. An increase in coating fraction with volume fraction and layer number held constant significantly increased the modulus as the square of the volume fraction and the peak stress in a non-linear fashion. An increase in the layer number lowered the critical buckling strength of the geometry non-linearly, the trend verging asymptotically with increasing size and depending heavily on the effective buckling length of the structures. The experimental modulus agreed well with the simulated data for the polymer and elastomer samples, and the experimental peak stress was found to be a lower value than predicted, due mainly to imperfections in the struts. There was a disparity between experimentation and simulation for both the modulus and the peak stress of the composites. One potential cause for this is the non-uniformity of the 3D printed coating, which was examined microscopically and found to have many imperfections along the polymer coating. Off-axis loading of the samples was also determined as a cause. Future work depends on advances in the resolution and repeatability of 3D printing technology.
机译:可以通过调整微结构的基本几何形状和材料成分来调整多孔固体的机械行为,包括刚度和强度。在这里,研究了关键参数对基于桁架的蜂窝状复合材料压缩变形响应的影响。选择了一种简单的周期性几何图形,并使用基于有限元的微机械模型进行了研究。在参数上进行模拟,以固定的支杆长度改变体积分数,复合支杆中聚合物涂层与弹性体核的比例(涂层分数)以及代表性体积元素的大小(层数)。还导出了基于能量方法的具有弹性约束的屈曲柱分析模型,并将其与仿真数据进行了比较。然后使用3D打印制造材料,然后进行压缩测试。比较了数值和实验结果。模拟表明,体积分数随涂层分数和层数的增加而保持恒定,以线性方式增加模量,并以非线性依赖性增加峰值应力。随着体积分数和层数保持恒定,涂层分数的增加以非线性方式显着增加模量,因为体积分数和峰值应力的平方。层数的增加非线性地降低了几何形状的临界屈曲强度,该趋势随着尺寸的增加而渐进地渐近,并且在很大程度上取决于结构的有效屈曲长度。实验模量与聚合物和弹性体样品的模拟数据吻合得很好,并且实验峰值应力被发现比预期值要低,这主要是由于支杆的缺陷。复合材料的模量和峰值应力在实验和模拟之间存在差异。造成这种情况的一个潜在原因是3D打印涂层的不均匀性,在显微镜下对其进行了检查,发现沿着聚合物涂层存在许多缺陷。还确定了样品的离轴加载。未来的工作取决于3D打印技术的分辨率和可重复性的进展。

著录项

  • 作者

    Rosario Matthew J;

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  • 年度 2010
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  • 原文格式 PDF
  • 正文语种 eng
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