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Deformation of Perforated Aluminium Plates inder In-Plane Compressive Loading

机译:穿孔铝板进入面内压缩载荷的变形

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Aluminium plates containing a single hole or multiple holes in a row are recently becoming very popular among architects and consultant engineers in many constructional applications, due to their reduced weight, as well as facilitating ventilation and light penetration of the buildings. However, there are still uncertainties concerning their structural behaviour, preventing them from wider utilization. In the present paper, local buckling phenomenon of perforated aluminium plates has been studied using the finite element method. For the purposes of the research work, plates with simply supported edges in the out-of-plane direction and subjected to uniaxial compression are examined. In view of perforations, circular cut-outs and the total cut-out size has been varied between 5 and 40% of the total plate area. Moreover, different perforation patterns have been investigated, from a single, central cut-out to a more refined pattern consisting of up to 25 holes equally distributed over the plate. Regarding the material characteristics, several aluminium alloys are considered and compared to steel grade A3 6 on plates of different slenderness. For each case the critical (Euler) buckling load and the ultimate resistance has been determined.A study into the boundary conditions of the plate showed that the restrictions at the edges parallel to the load direction have a large influence on the critical buckling load. Restraining the top or bottom edge does not significantly influence the resistance of the plate.The results showed that the ultimate resistance of aluminium plates containing multiple holes occurs at considerably larger out-of-plane displacement as that of full plates. For very large total cut-out, a plate containing a central hole has a larger resistance than a plate with equal cut-out percentage but with multiple holes. The strength and deformation in the post-critical regime, i.e. the difference between the critical buckling load and the ultimate resistance, differs significantly for different number of holes and cut-out percentage.
机译:由于其重量减轻,最近,含有单孔或多孔的铝板在许多建筑应用中,在建筑师和顾问工程师中非常受欢迎,以及促进建筑物的通风和光渗透。然而,仍有关于其结构行为的不确定性,防止它们更广泛利用。在本文中,采用有限元法研究了多孔铝板的局部屈曲现象。出于研究工作的目的,检查具有在平面外方向上的支撑边缘并进行单轴压缩的平板。鉴于穿孔,圆形剪裁和总切断尺寸在总板面积的5至40%之间变化。此外,已经研究了不同的穿孔图案,从单个中央切割到更精细的图案,其由最多25个孔组成,该图案等于板上的均匀分布在板上。关于材料特性,考虑了几种铝合金,并与不同细长的板上的钢级A3 6进行了比较。对于每种情况,临界(欧拉)屈曲负荷和最终电阻已经确定。研究板的边界条件表明,平行于负载方向的边缘对关键屈曲负荷有很大影响。抑制顶部或底部边缘不会显着影响板的电阻。结果表明,含有多孔的铝板的最终电阻发生在显着的平面外位移,作为全板的相当大的位移。对于非常大的总切断,含有中心孔的板具有比具有相同切出百分比的板更大的电阻,但有多个孔。临界后政策中的强度和变形,即关键屈曲负荷和最终阻力之间的差异,不同于不同数量的孔和切出百分比。

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