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The mechanical properties of novel lightweight structures based on corrugated-cores

机译:基于瓦楞芯的新型轻质结构的机械性能

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摘要

The aim of this research work is to investigate the mechanical properties of corrugated-core sandwich structures under quasi-static and dynamic loading conditions and to determine the failure mechanisms and energy-absorbing characteristics of the corrugated-cores with different cell wall thickness and filled with a foam core. Triangular corrugation structures were made from an aluminium alloy (AL), a glass fibre reinforced plastic (GFRP) and a carbon fibre reinforced plastic (CFRP). The composite corrugations were fabricated using a hot press moulding technique and then adhesively bonded to skins based on the same material, to produce a range of lightweight sandwich structures. The role of the number of unit cells, the thickness of the cell walls and the width in determining the mechanical behaviour of the structures was investigated. Buckling of the struts was identified as the initial failure mode in these corrugated systems. Continued loading resulted in plastic deformation in the aluminium system, in contrast, fibre .fracture, matrix cracking and localised delamination in the composite systems, as well as debonding between the skins and the core were observed in the composites. The compression strength and modulus were shown to be dependent on the number of unit cells and the cell wall thickness, but independent of specimen width. Subsequent mechanical testing was undertaken using an Arcan rig capable of generating a range of loading conditions between pure shear and pure compression. The failure strength in the aluminium system was accurately represented using a two dimensional quadratic failure criterion. In contrast, due to the initation of delamination within the composite struts, the composite corrugated-cores were accurately predicted using a modified failure criterion. Low velocity compression loading was subsequently performed on the sandwich structures, where the dynamic strength enhancement factor was shown to increase for all the corrugation systems. This was attributed to both a material strain-rate sensitivity and inertial stabilisation effects. The failure mechanisms in the sandwich structures were found to be similar under both quasi-static and dynamic loading conditions, where damage initiated due to buckling of the struts. To simulate the mechanical response of the corrugation systems, FE models have been developed using the Abaqus finite element package. The FE results were compared to measured responses, and good agreement was achieved. The failure modes predicted by the FE models show reasonably good agreement with the experimental observations. Finally, foam filling the composite corrugation systems significantly improved the specific strength as well as specific energy-absorbing characteristics of the structures. The compression properties of the corrugated structures have been compared to those of other core materials, where the evidence suggests that these systems compare favourably with other cellular core materials.
机译:这项研究的目的是研究瓦楞芯夹心结构在准静态和动态载荷条件下的力学性能,并确定不同泡孔壁厚和填充的瓦楞芯的破坏机理和能量吸收特性。泡沫芯。三角形波纹结构由铝合金(AL),玻璃纤维增​​强塑料(GFRP)和碳纤维增强塑料(CFRP)制成。复合波纹板是使用热压成型技术制造的,然后基于相同的材料粘合到蒙皮上,以生产一系列轻质夹心结构。研究了晶胞数量,晶胞壁的厚度和宽度在确定结构力学行为中的作用。在这些波纹系统中,支柱的屈曲被确定为最初的失效模式。持续的载荷导致铝体系发生塑性变形,与此相反,在复合体系中观察到纤维断裂,基体开裂和局部分层,以及在复合物中的表皮与芯层之间发生剥离。显示抗压强度和模量取决于晶胞的数量和晶胞壁的厚度,但与样品宽度无关。随后的机械测试是使用Arcan钻机进行的,该钻机能够在纯剪切力和纯压缩力之间产生一系列载荷条件。使用二维二次破坏准则准确地表示了铝系统中的破坏强度。相反,由于在复合材料支杆中产生分层,因此使用修改后的破坏准则可以准确地预测复合材料的波纹芯。随后在夹层结构上进行了低速压缩加载,其中所有波纹系统的动态强度增强因子均显示出增加的趋势。这归因于材料的应变速率敏感性和惯性稳定效应。发现在准静态和动态载荷条件下,夹层结构的破坏机理是相似的,在这种情况下,由于支柱的屈曲而引发了破坏。为了模拟瓦楞系统的机械响应,已使用Abaqus有限元软件包开发了有限元模型。将有限元结果与测得的响应进行比较,并取得了良好的一致性。有限元模型预测的失效模式与实验观察结果相当吻合。最后,泡沫填充复合瓦楞纸系统显着提高了结构的比强度以及比能量吸收特性。波纹结构的压缩性能已与其他核心材料的压缩性能进行了比较,证据表明这些系统与其他蜂窝状核心材料相比具有优势。

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    Mohd Ruzaimi Mat Rejab;

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  • 年度 2013
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