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Flexural properties of a novel foam core sandwich structure reinforced by stiffeners

机译:加强筋增强的新型泡沫芯夹层结构的抗弯性能

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The purpose of this paper is to investigate the flexural properties of a novel foam core sandwich structure with stiffeners. 3-point bending tests of two load levels were performed on three stiffened specimens (220 mm x 74 mm x 28.2 mm) and three unstiffened specimens (220 mm x 74 mm x 27.4 mm). Mechanical tests were firstly conducted under 1kN to determine the flexural and shear stiffness, and then under the destructive load to research the ultimate carrying capacity and failure modes. The skins of the specimens are fiberglass and vinyl resin, and the core is PVC foam. The mechanism of this novel structure was studied using Allen's theory on antiplane core and thick faces. Tests indicated that, without increase in weight, shear stiffness of the stiffened specimens increased by 25% and total deflection decreased by 19%. After inserting stiffeners, the failure mode changed from indentation failure to core shear and the ultimate load increased from 2.11kN to 2.74kN. The ultimate load and failure modes obtained from theoretical prediction and FEA both showed good correlations with experimental results. (C) 2019 Elsevier Ltd. All rights reserved.
机译:本文的目的是研究具有加强筋的新型泡沫芯夹层结构的挠曲特性。在三个加劲的样品(220毫米x 74毫米x 28.2毫米)和三个未加劲的样品(220毫米x 74毫米x 27.4毫米)上进行了两种载荷水平的三点弯曲测试。首先在1kN下进行机械测试以确定弯曲和剪切刚度,然后在破坏性载荷下研究极限承载力和破坏模式。标本的表皮为玻璃纤维和乙烯基树脂,内芯为PVC泡沫。使用艾伦关于反平面核心和厚面的理论研究了这种新颖结构的机理。测试表明,在不增加重量的情况下,加劲试样的剪切刚度增加了25%,总挠度减少了19%。插入加劲肋后,破坏模式从压痕破坏变为岩心剪切,极限载荷从2.11kN增加到2.74kN。从理论预测和有限元分析获得的极限载荷和破坏模式都与实验结果具有良好的相关性。 (C)2019 Elsevier Ltd.保留所有权利。

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