Strain-Rates Dependent Constitutive Law for Crashworthiness and Parameter Sensitivity Analysis of Woven Composites

R. Lombarkia, A. Gakwaya, D. Nandlall, M. L. Dano, J. Lévesque, P. Vachon-Joannette, P. Gagnon, A. Benkhelifa
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Abstract

The prediction of dynamic crushing behavior of aerospace-grade composites is a hard challenge for researchers. At coupons scale, such behavior implies the understanding of the initiation and propagation of the elementary damage mechanisms. Many results of the research confirm that the modulus and strength of composites increases with strain-rate. This paper presents the improvement of the constitutive model UL-Crush by adding dynamic stiffness modulus and strengths. The improved tool uses new approach by updating the stiffness and the strength values depending on strain-rates. In addition, parameter sensitivity investigations were conducted to assess the specific energy absorption capabilities of different material configurations. A new on-axis compression fixture was designed and manufactured to carry out tests of plain weave fabric composites, under quasi-static (QS) and low-velocity compression using MTS Insight 100 loading frame and drop tower CEAST Instron9340 facility. Two types of cross-section geometries were used: flat-plate and Hat-Shape coupons. Four types of triggering mechanism were adopted, including saw teeth, chamfer45°, steeple and corrugated, to ensure a continuous and stable crushing mode of failure. Detailed parameter sensitivity investigations were performed, including dimension scale, stacking sequences, trigger types and strain-rates. It was shown that the crush response is strain-rate dependent, and dynamic load decreases absorbed energy, which is indicative of microstructure disintegrating. Globally, big dimension scale, corrugated trigger, [0/45/45/0]s layup and decreasing strain-rate are the parameters to enhance the energy absorption capability of composite coupons. It has been observed that the improved numerical tool UL-Crush was able to significantly capture most crush mechanisms, reasonably correlate with experiments, and give an accurate dynamic response for crashworthy structures.

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机织复合材料耐撞性应变率本构关系及参数敏感性分析
航空航天级复合材料动态破碎行为的预测是研究人员面临的一项艰巨挑战。在优惠券规模上,这种行为意味着对基本损伤机制的启动和传播的理解。许多研究结果证实,复合材料的模量和强度随应变速率的增加而增加。本文通过增加动态刚度模量和强度,对UL Crush本构模型进行了改进。改进后的工具使用了新的方法,根据应变速率更新刚度和强度值。此外,还进行了参数敏感性研究,以评估不同材料配置的比能量吸收能力。设计和制造了一种新的轴上压缩夹具,用于在准静态(QS)和低速压缩下使用MTS Insight 100加载架和升降塔CEAST Instron9340设备对平纹织物复合材料进行测试。使用了两种类型的横截面几何形状:平板和帽形试样。采用了四种触发机制,包括锯齿、45°倒角、尖塔和波纹,以确保连续稳定的破碎失效模式。进行了详细的参数敏感性研究,包括尺寸尺度、堆叠顺序、触发类型和应变速率。结果表明,挤压响应与应变速率有关,动态载荷降低了吸收能量,这表明微观结构发生了崩解。在全球范围内,大尺寸尺度、波纹触发器、[0/45/45/0]叠层和降低应变速率是提高复合材料试件能量吸收能力的参数。已经观察到,改进的数值工具UL Crush能够显著捕捉大多数挤压机制,与实验合理相关,并为防撞结构提供准确的动态响应。
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