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Impact Performance Of Nanophased Foam Core Sandwich Composites

机译:纳米相泡沫芯夹芯复合材料的冲击性能

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摘要

In this study, sandwich panels were fabricated with neat and nanophased foam core and three-layered plain weave carbon fabric/Sc-15 epoxy composite face sheets. Neat and nanophased foam cores with Nanocor~R I-28E nanoclay at a loading of 0.5% and 1% by weight were prepared. Sandwich panels were then fabricated using co-injection resin transfer molding process. Samples of size 100 mm x 100 mm were then cut from the panels and subjected to low-velocity impact loading using an instrumented impact test setup. Impact response of the panels was recorded and analyzed in terms of peak load, absorbed energy, time and deflection at peak load. The tested samples were then sectioned into two halves and scanned using a scanner, optical and scanning electron microscopes to understand the failure patterns. Samples with nanophased foam sustained higher loads and had lower damage areas as compared with neat counterparts. Nanophased foam cores exhibited relatively more brittle fracture.
机译:在这项研究中,夹层板是用纯净的纳米相泡沫芯和三层平纹碳纤维织物/ Sc-15环氧复合材料面板制成的。制备具有Nanocor_R I-28E纳米粘土的净重和纳米相泡沫芯,其负载量为0.5%和1%(重量)。然后使用共注射树脂传递模塑工艺来制造夹芯板。然后从板上切下尺寸为100 mm x 100 mm的样品,并使用仪器化的冲击测试装置进行低速冲击加载。记录面板的冲击响应,并根据峰值载荷,吸收能量,时间和峰值载荷下的挠度进行分析。然后将测试样品切成两半,并使用扫描仪,光学和扫描电子显微镜进行扫描,以了解失效模式。与纯净的样品相比,具有纳米相泡沫的样品承受较高的载荷,并具有较低的破坏面积。纳米相泡沫芯表现出相对更大的脆性断裂。

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