论文标题
间隙测试:裂纹平行压缩对碳纤维复合材料断裂的影响
The Gap Test: Effects of Crack Parallel Compression on Fracture in Carbon Fiber Composites
论文作者
论文摘要
本文探讨了碳纤维复合材料的全局模式I断裂能在裂纹尖端处于双轴应力状态,特别是一种应力分量是压缩的,并且与裂纹平行。基于先前创造为GAP测试和Bazant II型尺寸效应定律的实验技术,发现随着裂纹平行压缩应力的增加,模式I断裂能的单调降低。与不施加裂纹平行压缩的断裂能的名义值相比,观察到裂缝能量的压缩应力等于该复合材料的压缩故障极限的44%。这种弱化的作用归因于由于裂纹平行压缩而在裂纹尖端引起的裂纹,该裂纹通过裂纹尖端显微镜检查鉴定出来。这是一个新的结果,它挑战了骨折能量是恒定材料特性的世纪旧假设,进一步表明,裂纹平行压缩导致复合结构的危险性较弱,比预期的要弱。实验活动还带有一个计算活动,该活动提供了一个框架,能够捕获裂纹并行压缩的影响。通过使用裂纹带模型,该模型正确地表征了断裂过程区域的张力区域,并与完全张力的损伤定律相结合,模拟结果与实验数据提供了令人满意的一致性。相反,当减少的张力损害定律定义了裂纹条带时,结果表明结构强度和断裂能量危险地高估了。这强调了使用裂纹谱带模型与完全张力损伤定律的重要性,以准确预测复合材料中的断裂。
This paper explores the global Mode I fracture energy of a carbon fiber composite subject to a biaxial stress state at a crack tip, specifically in which one stress component is compressive and parallel to the crack. Based on an experimental technique previously coined as The Gap Test and Bazant's Type II Size Effect Law, it is found that there is a monotonic decrease in the Mode I fracture energy as the crack parallel compressive stress increases. Compared to the nominal value of fracture energy, where no crack parallel compression is applied, the fracture energy is observed to decrease by up to 37% for a compressive stress equal to 44% of the compressive failure limit of the composite. This weakening effect is attributed to splitting cracks that are induced at the crack tip due to the crack parallel compression, which are identified via crack tip photomicroscopy. This is a novel result that challenges the century old hypothesis of fracture energy being a constant material property and further, shows for the first time that crack parallel compression leads to a composite structure being dangerously weaker than expected. The experimental campaign is also buttressed with a computational campaign that provides a framework capable of capturing the effects of crack parallel compression. Through the use of the crack band model, which correctly characterizes the fracture process zone tensorially, coupled with a fully tensorial damage law, the simulated results provide satisfactory agreement with the experimental data. Conversely, when a reduced tensorial damage law defines the crack band it is shown that the structural strength and fracture energy are dangerously overpredicted. This emphasizes the importance of using a crack band model coupled with a fully tensorial damage law to accurately predict fracture in composites.