Ti/Al3Ti层压板复合材料弹道性能的实验与模拟研究

IF 1.7 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES
Yang Cao, Siyuan Zhao, Limin Sun, W. He, Jun Ma
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引用次数: 2

摘要

金属间化合物复合材料Ti/Al3Ti由于其低密度、高强度和优异的抗冲击性能,可以用作航空航天和军事应用中的防护装甲。采用弹道试验和有限元技术对层压板复合材料的弹道性能进行了研究。弹道试验后发现了自由基裂纹、层间分层和塑性变形等失效模式,并使用比能量吸收来评估材料的弹道性能。通过考虑界面,建立了Ti/Al3Ti受弹丸撞击的有限元模型,并用零厚度的实体单元进行了模拟。仿真结果表明,界面在侵彻过程中发生了破坏。界面失效允许层与其人工层脱离。仿真结果与实验结果吻合较好,验证了模型的实用性和可靠性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental and simulated research on the ballistic performance of Ti/Al3Ti laminate composites
The metal-intermetallic laminate composite Ti/Al3Ti can be used as protective armor in aerospace and military applications, due to its low density, high strength, and superior impact-resistant performance. The ballistic performance of the laminate composite was studied by ballistic testing and finite element technology. The failure modes, such as radical cracks, layer delamination, and plastic deformation, have been found after the ballistic test, and the specific energy absorption was used to evaluate the ballistic capacity of the material. The finite element model of the Ti/Al3Ti impacted by the projectile was established by considering the interface, which was simulated by the solid elements with zero thickness. The simulation results demonstrate the failure process of the interface during penetration. The interfacial failure allowed for layer detachment with its labor layers. The simulation results agree well with that of the experiment, and the practicality and credibility of the model is verified.
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来源期刊
Advanced Composites Letters
Advanced Composites Letters 工程技术-材料科学:复合
自引率
0.00%
发文量
0
审稿时长
4.2 months
期刊介绍: Advanced Composites Letters is a peer reviewed, open access journal publishing research which focuses on the field of science and engineering of advanced composite materials or structures.
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