Hu Dayong, Dang Linwei, Zhang Chong, Zhang Zhiqiang
Department of Aircraft Airworthiness Engineering, School of Transportation Science and Engineering, Beihang University, Beijing 100191, China.
Aircraft/Engine Integrated System Safety Beijing Key Laboratory, Beijing 100191, China.
Materials (Basel). 2019 Mar 13;12(6):854. doi: 10.3390/ma12060854.
Flax fiber-reinforced composites (FFRCs) exhibit excellent environmentally friendly qualities, such as light weight, low cost, recyclability, and excellent mechanical properties. Understanding the dynamic mechanical behavior of FFRCs could broaden their potential applications in lightweight, crashworthy, and impact-critical structures. This study presents a study on the fabrication of FFRCs by vacuum-assisted resin infusion. The dynamic stress⁻strain responses of the fabricated specimens at strain rates ranging from 0.006 s-1 to 2200 s-1 were evaluated using quasi-static tests and the Split⁻Hopkinson pressure bar (SHPB). The results indicated that the FFRC exhibited superior strain rate sensitivity. Final deformation photographs and scanning electron micrographs clearly revealed the damage evolution of the FFRC specimens, as well as various failure mechanisms, including fiber⁻matrix debonding, fiber pull-out, and fiber fracture at different strain rates. On the basis of the experimental results, a simplified Johnson⁻Cook model was established to describe the strain-rate dependent constitutive model of FFRC. The validation of the suggested constitutive model was embedded in the finite element simulations and could well repeat the strain wave observed from the experiment results. Finally, the quasi-static compression and drop-hammer impact of pyramidal lattice structures with FFRC cores were investigated both numerically and experimentally, proving the effectiveness of the simplified Johnson⁻Cook model. This study could potentially contribute to a deeper understanding of the dynamic mechanical behavior of FFRCs and provide fundamental experimental data for future engineering applications.
亚麻纤维增强复合材料(FFRCs)具有优异的环保特性,如重量轻、成本低、可回收性以及出色的机械性能。了解FFRCs的动态力学行为可以拓宽其在轻质、防撞和冲击关键结构中的潜在应用。本研究提出了一项关于通过真空辅助树脂灌注制造FFRCs的研究。使用准静态试验和分离式霍普金森压杆(SHPB)评估了制造的试样在应变率范围为0.006 s-1至2200 s-1时的动态应力-应变响应。结果表明,FFRC表现出卓越的应变率敏感性。最终变形照片和扫描电子显微镜图像清楚地揭示了FFRC试样的损伤演化以及各种失效机制,包括在不同应变率下的纤维-基体脱粘、纤维拔出和纤维断裂。基于实验结果,建立了一个简化的约翰逊-库克模型来描述FFRC的应变率相关本构模型。所建议的本构模型的验证被嵌入到有限元模拟中,并且能够很好地重现从实验结果中观察到的应变波。最后,对具有FFRC芯的金字塔晶格结构的准静态压缩和落锤冲击进行了数值和实验研究,证明了简化的约翰逊-库克模型的有效性。本研究可能有助于更深入地了解FFRCs的动态力学行为,并为未来的工程应用提供基础实验数据。