带添加型蜂窝芯的夹芯板弹道冲击性能的实验和数值研究

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-11-14 DOI:10.1016/j.ast.2024.109733
Ahsan Ul Haq, Suresh Kumar Reddy Narala
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引用次数: 0

摘要

对轻质而坚固的材料和结构的追求推动了防护技术的快速发展。快速成型制造(AM)已成为一种变革性工具,可制造出具有定制特性的复杂蜂窝结构。在弹道防护领域使用增材制造蜂窝尚未得到广泛探索。有鉴于此,目前的研究通过实验和数值程序进行了全面调查,以了解嵌入快速成型蜂窝芯的夹芯板在受到弧形和锥形弹丸冲击时的响应。通过选择性激光熔化技术,使用 AlSi10Mg 粉末加成制造了三种不同的蜂窝芯,即六角形、星形和 AuxHex。每个蜂窝芯都与一对 1 毫米厚的 SS 316 板粘合在一起。射弹的发射速度介于 180 米/秒和 260 米/秒之间。在 ABAQUS/Explicit 中创建了有限元模型,以模拟弹道冲击情况。在变形、破坏模式和残余速度方面,预测结果与实验结果非常一致。结果显示,采用 AuxHex 内核的夹芯板具有更强的能量吸收能力,吸收的能量分别比六边形内核和星形内核多 15% 和 12%。此外,还观察到,与锥形弹丸相比,椭圆形弹丸击穿相同夹芯板所需的能量要高出 14%。此外,与采用六角形蜂窝芯的夹芯板相比,星形夹芯板和 AuxHex 夹芯板的弹道极限分别提高了 5% 和 9%。这项研究为增材制造蜂窝芯的应用提供了宝贵的见解,为航空航天和国防工业中至关重要的轻质弹性结构的开发提供了潜在的空间。
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Experimental and numerical investigation on the ballistic impact performance of sandwich panels with additively manufactured honeycomb cores
The pursuance of lightweight yet robust materials and structures has led to the rapid evolution of protective technologies. Additive Manufacturing (AM) has emerged as a transformative tool, enabling the fabrication of intricate cellular structures with tailored properties. The use of additively manufactured honeycombs in the field of ballistic protection has not been explored extensively. In this view, the current work presents a comprehensive investigation involving experimental and numerical procedures, to understand the impact response of sandwich panels embedded with additively manufactured honeycomb cores against ogive and conical projectile impacts. Three different honeycomb cores, namely Hexagonal, Star, and AuxHex are additively manufactured using AlSi10Mg powder via selective laser melting technique. Each core is bonded to a pair of 1 mm thick SS 316 sheets. The projectiles are launched at velocities varying between 180 m/s and 260 m/s. Finite element models are created in ABAQUS/Explicit to simulate ballistic impact scenarios. A strong consistency between the predicted results and experimental outcomes in terms of deformation, damage modes and residual velocities was obtained. The results revealed that the sandwich panel featuring an AuxHex core exhibits a superior energy absorption capacity, absorbing 15 % and 12 % more energy than hexagonal and star cores, respectively. Additionally, it was observed that, when compared to a conical projectile, an ogive projectile requires 14 % more energy to perforate the same sandwich panel. Furthermore, the ballistic limit of star and AuxHex panels is found to be increased by 5 % and 9 %, respectively compared to panels with hexagonal honeycomb cores. This work contributes valuable insights into the application of additively manufactured honeycomb cores, offering potential scope for the development of lightweight and resilient structures crucial in aerospace and defense industries.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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