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首页> 外文期刊>Composite Structures >Dynamic constitutive response of novel auxetic Kevlar®/epoxy composites
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Dynamic constitutive response of novel auxetic Kevlar®/epoxy composites

机译:新型增塑Kevlar®/环氧树脂复合材料的动态本构响应

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A comprehensive experimental investigation was performed to study the dynamic compressive constitutive response of novel auxetic Kevlar((R))/epoxy laminated composites. Strain rate response was investigated using the split Hopkinson pressure bar (SHPB) test setup. Laminated composites were fabricated using the vacuum infusion process. Short Nylon fibers were flocked between the laminates with different flock densities and flock length. For obtaining dynamic force equilibrium in SHPB experiments, a copper pulse shaper was used to increase the rising time of incident pulse. To have a comparison, woven Kevlar((R))/epoxy composites were also characterized at similar strain rates. In addition, quasi-static tests were also performed on both woven and auxetic laminated composites for completeness of the study. For quasi-static loading conditions, auxetic composites showed higher peak strain and lower peak stress compared to woven composites. For non-flocked composites, both auxetic and woven composites showed rate dependency. Woven composites provided 353% increase in peak stress when the strain rate increased from 1200 s(-1) (low) to 3300 s(-1) (high). However, in the same conditions, auxetic composites showed only 155% increase in peak stress. For different flocking conditions, woven composites showed rate dependency for all strain rates, but auxetic composites demonstrated rate dependency only from low to medium strain rates. Both auxetic and woven composites experienced shear failure under quasi-static compression, where auxetic composites failed at higher shear angle of 37(degrees), but woven composites had a failure angle of 30(degrees). For impact loads, under no flocking condition, woven composites did undergo severe edge failure at all strain rates, but auxetic composites showed a sign of edge failure only at high strain rates. With the flocking condition, auxetic composites had through thickness shear failure and woven composites experienced splitting and fibrillation of Kevlar((R)) fibers.
机译:进行了全面的实验研究,以研究新型的膨胀型Kevlar(R)/环氧层压复合材料的动态压缩本构响应。使用分开的Hopkinson压力棒(SHPB)测试装置研究了应变率响应。层压复合材料是使用真空灌注工艺制造的。短的尼龙纤维以不同的植绒密度和植绒长度植绒在层压材料之间。为了在SHPB实验中获得动态力平衡,使用了铜脉冲整形器来增加入射脉冲的上升时间。为了进行比较,还以相似的应变速率表征了编织的Kevlar/环氧复合材料。此外,还对机织和膨胀层压复合材料进行了准静态测试,以确保研究的完整性。对于准静态负载条件,与机织复合材料相比,膨胀复合材料显示出更高的峰值应变和更低的峰值应力。对于非植绒复合材料,膨胀和机织复合材料均显示出速率依赖性。当应变率从1200 s(-1)(低)增加到3300 s(-1)(高)时,机织复合材料的峰值应力增加353%。但是,在相同条件下,膨胀复合材料的峰值应力仅增加了155%。对于不同的植绒条件,机织复合材料在所有应变速率下均显示出速率依赖性,而膨胀复合材料仅在低应变速率到中应变速率下显示出速率依赖性。膨松复合材料和机织复合材料均在准静态压缩下经历剪切破坏,其中膨松复合材料在较高的剪切角为37(度)时发生破坏,而梭织复合材料的破坏角为30(度)。对于冲击载荷,在无植绒条件下,机织复合材料在所有应变率下均会发生严重的边缘破坏,但膨胀复合材料仅在高应变率下才显示出边缘破坏的迹象。在植绒条件下,膨胀复合材料经历了厚度剪切破坏,并且机织复合材料经历了Kevlar(R)纤维的分裂和原纤化。

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