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Kink crack problem in fiber reinforced composites.

机译:纤维增强复合材料的扭结裂纹问题。

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This study is concerned in the problem of a kink crack in unidirectional fiber-reinforced composite materials. This work studies the singularity index, driving forces, stress intensity factors, and the strain energy release rates in the kink crack embedded in anisotropic materials (composite materials).; Specifically, the singularity index was studied analytically where a kink crack is embedded in an infinite anisotropic plate (the unidirectional laminate); the crack makes an arbitrary angle with the fibers and the plate is loaded in uniform tension. Which was formulated and solved exactly based on two-dimensional anisotropic elasticity. The numerical effort involves developing a finite element technique to verify the singularity index and obtain the driving forces, stress intensity factors, and the strain energy release rates.; In finite element a finite-width rectangular plate containing a kink crack is considered. To simulate an infinite plate, the length and width of the plate are made very large compared to the size of the kink crack.; The plate is loaded by a far-field displacement uy = 1.0. The resulting stress field was highly concentrated near the crack tips.; Three composite materials where used to carry out the analysis, graphite/epoxy, glass/epoxy, and kevlar49/epoxy, with various fiber angles and kink angles.; The results showed that the singularity index and the driving forces (stress intensity factors, and the strain energy release rates) depend on the material properties, fiber angle, and kink angle.
机译:这项研究涉及单向纤维增强复合材料的扭结裂纹问题。这项工作研究了各向异性材料(复合材料)中嵌入的纽结裂纹的奇异性指数,驱动力,应力强度因子和应变能释放率。具体来说,是在无限各向异性板(单向层压板)中埋有扭结裂纹的情况下,对奇异性指数进行了分析研究。裂纹与纤维成任意角度,板以均匀的张力加载。它是根据二维各向异性弹性精确地制定和解决的。数值工作涉及开发有限元技术,以验证奇异性指标并获得驱动力,应力强度因子和应变能释放率。在有限元中,考虑了包含扭折裂纹的有限宽度矩形板。为了模拟无限大的板,与扭结裂纹的尺寸相比,将板的长度和宽度做得很大。板的远场位移u y = 1.0。产生的应力场高度集中在裂纹尖端附近。用于进行分析的三种复合材料,石墨/环氧树脂,玻璃/环氧树脂和凯夫拉尔49 /环氧树脂,具有不同的纤维角度和扭结角度。结果表明,奇异性指数和驱动力(应力强度因子和应变能释放速率)取决于材料性能,纤维角和扭结角。

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