Influential Factors of a Reactive Materials Projectile’s Damage Evolution Behavior

Author:

Li Xiangrong,Hou Cong,Tong Huan,Yang Lei,Chen Yongkang

Abstract

To determine the mechanism of penetration of multi-layer aluminum targets (MLAT) by a reactive materials projectile (RMP), AUTODYN-3D numerical simulations and experimental tests were carried out. The Powder Burn equation of the state ignition model was introduced for the reactive core activation under different projectile–target interaction conditions, which effectively simulated the deflagration reaction damage effects behavior of the RMP and the damage evolution behavior of the MLAT. The activation rate of the reactive core increased significantly when the thickness of the steel target was 8–15 mm; a significant combined destructive effect of kinetic and chemical energy was produced on the MLAT. The initial velocity was proportional to the penetration and destruction effect of the front-layer aluminum target. For the rear-layer aluminum target, the detonation damage showed a tendency to increase and then decrease. If the head metal block was too thick, the penetration ability would be improved at the same time, and the deflagration reaction damage effects ability of the steel target would be significantly reduced. In order to achieve good battlefield damage efficacy, all of the influencing factors should be comprehensively considered.

Publisher

MDPI AG

Subject

Inorganic Chemistry,Condensed Matter Physics,General Materials Science,General Chemical Engineering

Reference31 articles.

1. Jazon, B., Backofen, J., Brown, R.E., Cayzac, R., Giraud, M., Held, M., and Diederen, A. (2007, January 16–20). The future of warheads, armour and ballistics. Proceedings of the 23rd International Symposium on Ballistics, Tarragona, Spain.

2. Damage effect of doublespaced aluminum plates by reactive material projectile impact;Int. J. Impact Eng.,2017

3. Interval rupturing damage to multi-spaced aluminum plates impacted by reactive materials filled projectile;Int. J. Impact Eng.,2019

4. Ames, R.G. (December, January 27). Energy Release Characteristics of Impact-Initiated Energetic Materials. Proceedings of the Materials Research Society Symposium, Boston, MA, USA.

5. Ames, R.G. (2005, January 10–13). Vented Chamber Calorimetry for Impact-Initiated Energetic Materials. Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3