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Numerical studies on stability and load capacity of compressed channel section columns made of composite reinforced with flax fibers

机译:亚麻纤维增强复合材料压缩通道截面柱稳定性和承载能力的数值研究

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摘要

In this article, the results for compressed channel section profiles made of glass and flax fiber reinforced polymer were presented. Six symmetric arrangements of layers were tested: [0/-45/45/90]s, [90/-45/45/0]s, [90/0/90/0]s, [0/90/0/90]s, [45/-45/45/-45]s, [45/-45/90/0]s. The study concerns the buckling and failure modes and loads determination. To obtain load capacity of analyzed structures the ANSYS program based on finite element method was employed. Linear (LBA) and nonlinear buckling analyses (NBA) with an implementation of the progressive failure algorithm (PFA) with the Hashin criterion as the damage onset criterion, were performed. Structures made of natural fibers were characterized by small differences in relation to the successive buckling loads, similar load carrying capacity values determined for the implementation of successive buckling modes and, in opposition to GFRP channel section profiles, by a lack of or a small range of deformations in the postbuckling stage. Wherefore, the obtained results with results for analogous profiles made of GFRP were compared. Furthermore, the effect of laying the laminate layers on the magnitude of the critical force and the occurrence of a specific failure mechanism depending on the number of degraded layers were presented.
机译:在本文中,介绍了由玻璃和亚麻纤维增强聚合物制成的压缩通道截面轮廓的结果。测试了六个对称的层排列:[0 / -45 / 45/90] s,[90 / -45 / 45/0] s,[90/0/90/0] s,[0/90/0 / 90] s,[45 / -45 / 45 / -45] s,[45 / -45 / 90/0] s。研究涉及屈曲和破坏模式以及载荷确定。为了获得分析结构的承载能力,采用了基于有限元方法的ANSYS程序。进行了线性(LBA)和非线性屈曲分析(NBA),并以渐进失效算法(PFA)的实施方式为基础,以Hashin准则作为损伤发作准则。由天然纤维制成的结构的特征是,相对于连续屈曲载荷有很小的差异,为实现连续屈曲模式而确定的相似的承载能力值,并且与GFRP通道截面轮廓相反,其特征是缺乏或较小后屈曲阶段的变形。因此,将获得的结果与由GFRP制成的类似轮廓的结果进行比较。此外,提出了层压层的放置对临界力的大小的影响以及取决于降解层数的特定破坏机理的出现。

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