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Theoretical and computational modelling of instrumented indentation of viscoelastic composites

机译:粘弹性复合材料压痕的理论和计算模型

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摘要

In this study, we investigate the indentation of viscoelastic composites. The composite is assumed to consist of two phases, i.e., the filler and the matrix, which are linear elastic and linear viscoelastic material, respectively. Two cases are investigated: (1) hard fillers are scattered in a very soft matrix; (2) the matrix is much harder than the fillers. Particular attention is paid to the correlation between the indentation relaxation loads and the material and geometric parameters of the composite system. To this end, we perform a theoretical analysis which is followed by finite element analysis. Our main result is a simple relation correlating the reduced relaxation modulus of the matrix, E m,r (t), with the indentation relaxation load P(t), i.e., E m,r (t)=P(t)/P(0), where P(0) represents the indentation load at the starting point of the relaxation test. This result on one hand indicates that for the two cases under study the relaxation feature of the indentation load is determined by the reduced relaxation modulus of the matrix. On the other hand, the result shows that the reduced relaxation modulus of the matrix of the composites may be simply determined from the indentation relaxation load without invoking the knowledge of both the indenter geometry and the profile of indented solids.
机译:在这项研究中,我们研究了粘弹性复合材料的压痕。假定该复合材料由两相组成,即填料和基质,它们分别是线性弹性材料和线性粘弹性材料。研究了两种情况:(1)硬质填料分散在非常柔软的基质中; (2)基体比填料硬得多。特别要注意的是压痕松弛载荷与复合系统的材料和几何参数之间的相关性。为此,我们执行理论分析,然后进行有限元分析。我们的主要结果是一个简单的关系,该关系将矩阵的减小的松弛模量E m,r (t)与压痕松弛载荷P(t)相关,即E m,r (t)= P(t)/ P(0),其中P(0)表示松弛测试起点处的压痕载荷。一方面,该结果表明,对于所研究的两种情况,压痕载荷的松弛特征取决于基体减小的松弛模量。另一方面,结果表明,可以从压痕弛豫载荷简单地确定复合材料基质的降低的弛豫模量,而无需调用压头几何形状和压痕固体轮廓的知识。

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