1. 北京理工大学 爆炸科学与技术国家重点实验室, 北京 100081
2. 北京机电工程研究所, 北京 100074
*邮箱: wuhj@bit.edu.cn
收稿:2022-08-17,
网络出版:2024-01-12,
纸质出版:2023-12-30
移动端阅览
邓希旻, 田泽, 武海军, 等. 上下非对称结构弹体侵彻金属薄板的特性及薄板破坏形式[J]. 兵工学报, 2023,44(12):3836-3850.
Ximin DENG, Ze TIAN, Haijun WU, et al. Penetration Characteristics and Plate Failure Modes of Asymmetrically Shaped Projectiles Penetrating Thin Metal Targets[J]. Acta Armamentarii, 2023, 44(12): 3836-3850.
邓希旻, 田泽, 武海军, 等. 上下非对称结构弹体侵彻金属薄板的特性及薄板破坏形式[J]. 兵工学报, 2023,44(12):3836-3850. DOI: 10.12382/bgxb.2022.0724.
Ximin DENG, Ze TIAN, Haijun WU, et al. Penetration Characteristics and Plate Failure Modes of Asymmetrically Shaped Projectiles Penetrating Thin Metal Targets[J]. Acta Armamentarii, 2023, 44(12): 3836-3850. DOI: 10.12382/bgxb.2022.0724.
为支撑超高声速导弹终点毁伤理论设计
适应异型弹体穿甲力学基础理论发展需求
非对称异型弹体贯穿金属薄板的穿甲特性及靶板损伤机理是当前亟需解决的关键科学问题。开展上下非对称结构异型弹体正/斜贯穿多层间隔921A薄钢板实验
基于Abaqus/Explicit、VUMAT和Python子程序开展数值模拟研究
分析弹体速度变化及偏转特性
结合靶板破坏形貌和能量耗散分析靶板损伤机理
讨论了研究结果在实际工程应用中的适用性。研究结果表明:上下非对称结构异型弹体具有维持弹体姿态稳定的特点
初速低于600m/s时速度降和弹道极限随倾角的增加而增大
靶板破坏模式以剪切冲塞、瓣裂和整体横向变形主导
初速高于600m/s时同初始倾角的弹道极限曲线重合
无量纲速度降随初速增加而降低
靶板破坏模式向延性扩孔、瓣裂和破碎转变;靶板塑性变形时切向塑性功占比最大、环向塑性功最小、轴向和径向塑性功相近
高速侵彻过程中靶板碎片动能为塑性功的25%~50%;基于几何相似的缩比模型可反映原型弹体高速穿甲时的速度变化情况及靶板的毁伤特性;研究成果可为异型弹体高速穿甲的弹靶响应及阻力特性的理论建模提供物理认识及数据支撑。
In order to support the theoretical design of terminal damage of hypersonic missile and the basic theory of armor-piercing mechanics of special-shaped projectile
the penetration ability of asymmetrically shaped projectile penetrating metal target and the damage mechanism of target plate need to be solved. The velocity variation and deflection characteristics of the projectile are analyzed through the experiment of asymmetrically shaped projectile penetrating the multi-layer spaced 921A steel plate and the numerical simulation based on Abaqus/Explicit
VUMAT and Python subroutines. The damage mechanism of target plate is analyzed from damage morphology and energy dissipation
and the applicability of the research results in practical engineering application is discussed. The results show that the asymmetric structure has the ability to maintain the stability of projectile attitude. When the initial velocity is lower than 600 m/s
the velocity drop and the ballistic limit increase with the increase of the oblique angle
and the failure modes of the target plate are shear plugging
pealing and transverse deformation. When the initial velocity is higher than 600 m/s
the ballistic limit curves of different oblique angles overlap
the dimensionless velocity drop decreases with the increase of the initial velocity
and the failure mode of target plate changes to ductile enlargement
pealing and fragmentation. During the penetration progress
the tangential component of plastic work done has the largest proportion
the circumferential component is the smallest
and the axial and radial plastic works are similar. During the high-speed penetration
the kinetic energy of plate fragments is 25%-50% of the plastic work done. The scaled model based on geometric similarity can reflect the speed change of the prototype projectile during the high-speed penetration and the damage characteristics of trget plate.
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李营 . 液舱防爆炸破片侵彻作用机理研究 [D ] . 武汉 : 武汉理工大学 , 2014 .
LI Y . Fragment resistrant mechanism research of safety liquid cabin [D ] . Wuhan : Wuhan University of Technology , 2014 . (in Chinese)
MATIAS SILVA W T , MENDES BEZERRA L . A radial return algorithm application in elastoplastic frame analysis using plastic hinge approach [J ] . Mathematical Problems in Engineering , 2010 , 2010 : 142743 .
GANJIANI M . A damage model for predicting ductile fracture with considering the dependency on stress triaxiality and Lode angle [J ] . European Journal of Mechanics—A/Solids , 2020 , 84 : 104048 . DOI: 10.1016/j.euromechsol.2020.104048 http://doi.org/10.1016/j.euromechsol.2020.104048 https://linkinghub.elsevier.com/retrieve/pii/S0997753820304368 https://linkinghub.elsevier.com/retrieve/pii/S0997753820304368
MUIRURI A , MARINGA M , DU PREEZ W . Development of VUMAT and VUHARD subroutines for simulating the dynamic mechanical properties of additively manufactured parts [J ] . Materials , 2022 , 15 ( 1 ): 372 . DOI: 10.3390/ma15010372 http://doi.org/10.3390/ma15010372 https://www.mdpi.com/1996-1944/15/1/372 https://www.mdpi.com/1996-1944/15/1/372 Numerical modelling and simulation can be useful tools in qualification of additive manufactured parts for use in demanding structural applications. The use of these tools in predicting the mechanical properties and field performance of additive manufactured parts can be of great advantage. Modelling and simulation of non-linear material behaviour requires development and implementation of constitutive models in finite element analysis software. This paper documents the implementation and verification process of a microstructure-variable based model for DMLS Ti6Al4V (ELI) in two separate ABAQUS/Explicit subroutines, VUMAT and VUHARD, available for defining the yield surface and plastic deformation of materials. The verification process of the implemented subroutines was conducted for single and multiple element tests with varying prescribed loading conditions. The simulation results obtained were then compared with the analytical solutions at the same conditions of strain rates and temperatures. This comparison showed that both developed subroutines were accurate in predicting the flow stress of various forms of DMLS Ti6Al4V (ELI) under different conditions of strain rates and temperatures.
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RUSINEK A , RODRÍGUEZ-MARTÍNEZ J A , ZAERA R , et al . Experimental and numerical study on the perforation process of mild steel sheets subjected to perpendicular impact by hemispherical projectiles [J ] . International Journal of Impact Engineering , 2009 , 36 ( 4 ): 565 - 587 . DOI: 10.1016/j.ijimpeng.2008.09.004 http://doi.org/10.1016/j.ijimpeng.2008.09.004 https://linkinghub.elsevier.com/retrieve/pii/S0734743X08002303 https://linkinghub.elsevier.com/retrieve/pii/S0734743X08002303
TAYLOR G I . The Formation and enlargement of a circular hole in a thin plastic sheet [J ] . Quarterly Journal of Mechanics and Applied Mathematics , 1948 , 1 ( 1 ): 103 - 124 . DOI: 10.1093/qjmam/1.1.103 http://doi.org/10.1093/qjmam/1.1.103 https://academic.oup.com/qjmam/article-lookup/doi/10.1093/qjmam/1.1.103 https://academic.oup.com/qjmam/article-lookup/doi/10.1093/qjmam/1.1.103
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