Rozylo Patryk
Department of Machine Design and Mechatronics, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland.
Materials (Basel). 2021 Dec 27;15(1):167. doi: 10.3390/ma15010167.
The novelty of this paper, in relation to other thematically similar research papers, is the comparison of the failure phenomenon on two composite profiles with different cross-sections, using known experimental techniques and advanced numerical models of composite material failure. This paper presents an analysis of the failure of thin-walled structures made of composite materials with top-hat and channel cross-sections. Both experimental investigations and numerical simulations using the finite element method (FEM) are applied in this paper. Tests were conducted on thin-walled short columns manufactured of carbon fiber reinforced polymer (CFRP) material. The experimental specimens were made using the autoclave technique and thus showed very good strength properties, low porosity and high surface smoothness. Tests were carried out in axial compression of composite profiles over the full range of loading-up to total failure. During the experimental study, the post-buckling equilibrium paths were registered, with the simultaneous use of a Zwick Z100 universal testing machine (UTM) and equipment for measuring acoustic emission signals. Numerical simulations used composite material damage models such as progressive failure analysis (PFA) and cohesive zone model (CZM). The analysis of the behavior of thin-walled structures subjected to axial compression allowed the evaluation of stability with an in-depth assessment of the failure of the composite material. A significant effect of the research was, among others, determination of the phenomenon of damage initiation, delamination and loss of load-carrying capacity. The obtained results show the high qualitative and quantitative agreement of the failure phenomenon. The dominant form of failure occurred at the end sections of the composite columns. The delamination phenomenon was observed mainly on the outer flanges of the structure.
与其他主题相似的研究论文相比,本文的新颖之处在于,利用已知的实验技术和先进的复合材料失效数值模型,对两种不同横截面的复合材料型材的失效现象进行比较。本文对具有帽形和槽形横截面的复合材料制成的薄壁结构的失效进行了分析。本文采用了实验研究和有限元法(FEM)数值模拟两种方法。对由碳纤维增强聚合物(CFRP)材料制成的薄壁短柱进行了测试。实验样本采用热压罐技术制作,因此具有非常好的强度性能、低孔隙率和高表面光洁度。对复合材料型材在直至完全失效的整个加载范围内进行轴向压缩试验。在实验研究过程中,同时使用Zwick Z100万能试验机(UTM)和声发射信号测量设备记录了后屈曲平衡路径。数值模拟使用了复合材料损伤模型,如渐进失效分析(PFA)和内聚区模型(CZM)。对承受轴向压缩的薄壁结构的行为分析,使得在深入评估复合材料失效的同时能够评估稳定性。该研究的一个重要成果是,除其他外,确定了损伤起始、分层和承载能力丧失的现象。所得结果表明失效现象在定性和定量方面具有高度一致性。失效的主要形式发生在复合材料柱的端部。分层现象主要在结构的外翼缘上观察到。