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Experimental and numerical investigation into fatigue damage mechanisms in multifibre microcomposites

机译:多纤维微复合材料疲劳损伤机理的实验和数值研究

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摘要

Polarised light microscopy has been used to investigate the influnce of stress level, interfibre spacing, and fibre-matrix adhesion on the fatigue micromechanisms in carbon-epoxy model composites consisting of a planar array of five intermediate modulus carbon fibres. It was found that an increase in fatigue stress results in an increase in the number of fibre breaks, a more coordinatefibre fracture pattern as a result of fibre interaction, and extensive interfacial damage. In addition, it was shown that a smaller interfibre spacing results in a higher level of fibre-interaction. Finally, in the case of surface treated carbon fibres (good fibre-matrix adhesion), a more coordinated fibre failure pattern was observed owing to stronger fibre-fibre interaction, whereas in the case of untreated carbon fibres (poor fibre-matrix adhesion), extensive debonding was observed which resulted in a more random fibre failure pattern. Finally, the experimental results were validated by means of a three-dimensional finite element analysis.
机译:偏光显微镜已被用来研究应力水平,纤维间间距和纤维-基质粘附对由五种中模量碳纤维平面排列组成的碳-环氧树脂模型复合材料疲劳微观机制的影响。已经发现,疲劳应力的增加导致纤维断裂的数量增加,由于纤维相互作用而导致更多的配位纤维断裂模式,以及广泛的界面损伤。另外,已经表明,较小的纤维间间距导致较高水平的纤维相互作用。最后,对于经过表面处理的碳纤维(良好的纤维-基体附着力)而言,由于较强的纤维-纤维相互作用,观察到了更为协调的纤维破坏模式,而对于未经处理的碳纤维(较差的纤维-基体附着力),观察到广泛的脱粘,这导致了更随机的纤维破坏模式。最后,通过三维有限元分析验证了实验结果。

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