Impact Analysis of a Composite Armor System

S. Alam, M. Saquib
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引用次数: 1

Abstract

Present day demands composite material with even lighter weight and higher strength for using in aerospace, automobile and defense industries. Due to posing significantly weight saving and higher stiffness attribute, use of sandwich composite structure is the demand of the time. Impact analysis of sandwich composite armor system is necessary to design and develop new armor for defense sectors. The goal of this study is to design, model and analyze the dynamic response of the composite armor system in terms of residual velocity and energy absorption capacity. The design parameters are investigated for different fiber reinforced polymers (High tensile strength Carbon/epoxy, Carbon Fiber/Carbon Nanotube reinforced polymers) as top and bottom skin, with an Aluminum Alloy 7039 corrugated core structure and square prismoid assembled Ceramic (SiC) core centerpieces at different velocities (50 m/s, 100 m/s, 200 m/s, 400 m/s). This non-linear explicit dynamic study is performed using commercial software ABAQUS CAE 2017. Best combination for the composite armor system is suggested based on the results.
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复合装甲系统的冲击分析
目前,航空航天、汽车和国防工业需要重量更轻、强度更高的复合材料。夹层复合材料结构具有显著的减重和较高的刚度特性,是时代的要求。夹层复合装甲系统的冲击分析是设计和研制新型装甲的必要条件。本研究的目的是设计、建模和分析复合装甲系统在剩余速度和能量吸收能力方面的动态响应。研究了不同纤维增强聚合物(高抗拉强度碳/环氧树脂、碳纤维/碳纳米管增强聚合物)作为上下表皮的设计参数,采用铝合金7039波纹芯结构和方形棱柱形装配陶瓷(SiC)芯中心件,在不同速度下(50 m/s、100 m/s、200 m/s、400 m/s)。该非线性显式动态研究使用商业软件ABAQUS CAE 2017进行。在此基础上提出了复合装甲系统的最佳组合。
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