Continuum Damage Micromechanics Model for the Compressive Failure of Flax Fiber Composites and Experimental Validation

V. Tojaga, A. Prapavesis, J. Faleskog, T. Gasser, A. Vuure, S. Östlund
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Abstract

We develop a thermodynamically consistent continuum damage micromechanics model for the compressive failure of flax fiber composites. We used a micromechanics-based constitutive model reported recently [1]. It describes the microstructure of a unidirectional composite and captures the material behavior of the fiber and matrix constituents, respectively. The description has been formulated in the reference configuration (i.e. the undeformed state of the composite) and is therefore independent of fiber rotations that may appear during the deformation of the composite. A hyperelastic finite deformation plasticity with power law hardening [3] mimics the compressive elastic-plastic stress-strain response of the fiber (reported in [2]) and the matrix. The model has been extended to account for fiber damage, resulting in a thermodynamically consistent continuum damage micromechanics model. Our results indicate that fiber damage plays an utmost role in the compressive failure of flax fiber composites – it is a major determinant of the material’s compressive stress-strain response. X-ray Computed Tomography and Scanning Electron Microscopy show that fiber damage can be attributed to intra-fiber splitting and elementary fiber crushing.
亚麻纤维复合材料压缩破坏连续损伤细观力学模型及实验验证
建立了亚麻纤维复合材料压缩破坏的热力学一致连续损伤细观力学模型。我们使用了最近报道的基于微观力学的本构模型[1]。它描述了单向复合材料的微观结构,并分别捕获了纤维和基体成分的材料行为。所述描述是在参考配置(即复合材料的未变形状态)中制定的,因此与复合材料变形期间可能出现的纤维旋转无关。具有幂律硬化的超弹性有限变形塑性[3]模拟了纤维(文献[2])和基体的压缩弹塑性应力-应变响应。该模型已扩展到考虑纤维损伤,从而得到一个热力学一致的连续损伤微观力学模型。我们的研究结果表明,纤维损伤在亚麻纤维复合材料的压缩破坏中起着最大的作用,它是材料压缩应力-应变响应的主要决定因素。x射线计算机断层扫描和扫描电镜显示,纤维损伤可归因于纤维内分裂和初级纤维破碎。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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