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Low-velocity impact performance of nanoflber-interlayered aramid/epoxy nanocomposites

机译:纳米纤维夹层芳纶/环氧树脂纳米复合材料的低速冲击性能

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摘要

Low-velocity impact response of aramid/epoxy laminates containing nano-interlayers with different amounts of the thickness (17.5, 35, and 70 mu m) and various stacking configuration (back-side, central, and two-sides interleaving) has been studied. A hand lay-up method was used for making composites. Instrumented impact tests were compared with quasi-static indentation tests by using the same specimen and test configurations. The results show that generally, quasi-static indentation analysis is sufficient to assess the impact response of interleaved composite only until a certain impact energy level. However, the optimum thickness of interleaves for obtaining the highest value of toughness for interleaved composites is 35 mu m. Moreover, the behavior of backside configuration was similar to static tests in impact tests, but other configurations almost did not follow this trend.
机译:研究了芳族聚酰胺/环氧树脂层压板的低速冲击响应,该层压板包含不同厚度(17.5、35和70μm)和各种堆叠结构(背面,中央和两侧交错)的纳米中间层。使用手工铺网方法来制造复合材料。使用相同的样本和测试配置,将仪器化的冲击测试与准静态压痕测试进行了比较。结果表明,一般而言,准静态压痕分析足以评估交错复合材料的冲击响应,直到达到一定的冲击能级为止。然而,用于获得交错复合材料的最高韧性值的交错的最佳厚度为35μm。此外,背面配置的行为类似于冲击测试中的静态测试,但其他配置几乎没有遵循这种趋势。

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