期刊
COMPOSITES PART C: OPEN ACCESS
卷 8, 期 -, 页码 -出版社
ELSEVIER
DOI: 10.1016/j.jcomc.2022.100265
关键词
Hybrid composites; Fatigue; Sheet Molding Compound; Continuous-discontinuous reinforcement; Damage; Effects of Hybridization
资金
- German Research Foundation (DFG) [GRK 2078]
- German Research Foundation (DFG)
This paper presents an experimental study on the bending fatigue behavior of hybrid continuous-discontinuous sheet molding compound (SMC) composites. The results show that the hybrid composite has higher ultimate flexural strength and fatigue strength compared to the discontinuous SMC, while the relative stiffness degradation is smaller. This indicates the potential of hybrid SMC composites for structural automotive applications.
Hybrid continuous-discontinuous sheet molding compound (SMC) composites are considered suitable candidates for structural automotive applications, due to their high mass-specific mechanical properties combined with high geometrical flexibility and low costs. Since structural automotive parts are subject to repeated loading, profound knowledge of their fatigue behavior is required. This paper presents an experimental study on the bending fatigue behavior of hybrid SMC with discontinuous glass fibers in the core and unidirectional continuous carbon fibers in the face layers. Effects of hybridization on the S-N behavior and stiffness degradation have been analyzed in constant amplitude fatigue tests under 3-point bending load at different temperatures and frequencies. Microscopic investigations on polished specimen edges were used to study the damage behavior. The ultimate flexural strength at quasi-static (UFSS) and fatigue strain rate (UFSF) of the hybrid composite was 54 % and 59 % higher than that of discontinuous SMC, respectively. In contrast, the flexural fatigue strength at 2.6.10(6) cycles increased by 258 %. The relative stiffness degradation of the hybrid composites was smaller during most of their fatigue lives due to the continuous carbon fiber reinforcement. The carbon fiber ply on the compression loaded side was the first ply to fail. Fatigue stress significantly decreased at 80 degrees C due to early kinking of the continuous carbon fiber-reinforced ply on the compression loaded side. Variation of frequency had no significant effect on the fatigue behavior of both discontinuous and continuous-discontinuous SMC.
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