初始损伤对复合材料疲劳强度影响的计算估计

IF 3 Q2 MATERIALS SCIENCE, COMPOSITES Journal of Composites Science Pub Date : 2023-10-16 DOI:10.3390/jcs7100438
Konstantin Konstantinovich Shramko, Nikolai Olegovich Kononov, Arina Evgenevna Lutoshkina, Aleksey Viktorovich Shadrinov
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引用次数: 0

摘要

提出了基于计算力学方法的聚合物复合材料(PCM)静强度和疲劳强度的初始损伤(如结构孔区域的分层)影响评估方法。利用Simcenter 3D-Samcef软件包和Specialist耐久性模块对PCM结构构件进行了耐久性计算。选择一种典型的碳纤维增强塑料作为研究材料,该塑料具有从试验中获得的可用物理和力学特性。对典型碳纤维增强塑料的疲劳特性进行了近似计算,以便于后续的耐久性计算。在耐久性计算中,观测参数为研究区域反复荷载作用下材料刚度的退化。估计了无缺陷带孔带材疲劳强度模型与实验结果的收敛性。具有分层型缺陷的样品的疲劳强度也与无损伤样品的疲劳强度进行了比较。
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Computational Estimate of the Initial Damage Effect on the Fatigue Strength of Composite Materials
An estimate of the effect of initial damage, such as delamination in the area of a structural hole, on the static and fatigue strength of polymer composite material (PCM) based on computational mechanics methods is presented. Calculation for durability of structural elements made of PCM is conducted using Simcenter 3D—Samcef package and Specialist Durability module. A typical carbon fiber-reinforced plastic with the available physical and mechanical characteristics obtained from the tests was chosen as the study material. Fatigue characteristics of the typical carbon fiber-reinforced plastic were approximated for subsequent calculation on durability. In the durability calculation, the observed parameter is the degradation of the material stiffness under repeated loading of the investigated area. The convergence with the experimental results of the fatigue strength modeling for a defect-free sample, which is a strip with a hole, is estimated. The fatigue strength of a sample with a delamination-type defect is also compared with the fatigue strength of a damage-free sample.
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来源期刊
Journal of Composites Science
Journal of Composites Science MATERIALS SCIENCE, COMPOSITES-
CiteScore
5.00
自引率
9.10%
发文量
328
审稿时长
11 weeks
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