空间和运载火箭用纳米粘土增强聚合物的弹性参数

K. Mallick, C. Paul
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引用次数: 1

摘要

本研究导出了纳米粘土增强聚合物基体有效弹性模量的解析表达式。当前工作背后的动机是,通常的混合计算规则对复合材料的弹性参数提供了非常差的估计。采用基于细观力学的模型和有效弹性连续体理论,推导了嵌有以圆盘状纳米粘土颗粒为代表的直线包裹体的弹性介质的有效模量。为了简单起见,在当前的分析中考虑了纳米粘土分散的空间分布平行阵列。复合材料的有效模量是根据纳米粘土的体积分数和原始基质和纳米粘土颗粒的弹性参数推导出来的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Elastic parameters of nanoclay-reinforced polymers for space and launch vehicles
The present study derives an analytical expression for the effective elastic modulus of nanoclay-reinforced polymer matrix. The motivation behind the current work is that the usual rule of mixture calculations provides very poor estimates of the elastic parameters of the composite. A micromechanics based model and effective elastic continuum theory are used to derive the effective moduli of an elastic medium embedded with rectilinear inclusions representing disk like nanoclay particles. For simplicity a spatially distributed parallel array of nanoclay dispersion is considered in the current analysis. The effective modulus of the composite is derived in terms of the volume fraction of the nanoclays and the elastic parameters of the virgin matrix and the nanoclay particles.
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