High-speed perforation of IN718 plates by spherical TC4 Ti alloy projectiles: Experiments and modeling

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-01 DOI:10.1016/j.ast.2024.109356
J.Y. Hua , Q. Liu , Z.Y. Liu , C.H. Mi , Y.D. Chen , J.C. Cheng , J. Wu , L. Lu , Y. Cai , S.N. Luo
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Abstract

Data and knowledge on ballistic performance of Inconel-718 (IN718) alloy is critical for evaluating the resistance of turbine blades against foreign object impacts in aeronautical and astronautical industries. Ballistic perforation experiments (impact velocity 480 m s−1 to 1340 m s−1) with TC4 spherical projectiles (5-mm-diameter) are conducted on IN718 target plates (2-mm-thick) in this work, along with high-speed photography. The IN718 plates show multiple deformation and failure modes (bulging, dishing, petaling and plugging). The ballistic limit velocity for the investigated projectile/target combination is 823 m s−1. Postmortem material characterizations (optical photography, scanned electron microscopy and energy dispersive spectrometry) are conducted on recovered projectiles and bullet hole inner walls, and the observations indicate adiabatic shearing, surface melting and abrasion of projectile material. A finite element model based on the Johnson–Cook constitutive model and failure criterion is established, and reproduces the ballistic experiments. Dimensionless analyses are conducted on the dimensions of postmortem projectiles and bullet holes, and the projectile residual velocity/mass. On the basis of experimental observations and theoretical analysis of the projectile dynamics, the whole perforation process is divided into three stages (the entering, cratering and plugging stages). A multi-stage analytical model on perforation is then developed considering the effects of cavity expansion, projectile deformation and abrasion, and can well predict the projectile dynamics during entering and cratering stages.

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球形 TC4 Ti 合金射弹对 IN718 板材的高速穿孔:实验与建模
有关 Inconel-718 (IN718) 合金弹道性能的数据和知识对于评估航空和航天工业中涡轮叶片的抗异物冲击能力至关重要。在这项工作中,使用 TC4 球形射弹(直径 5 毫米)对 IN718 靶板(2 毫米厚)进行了弹道穿孔实验(冲击速度为 480 m s-1 至 1340 m s-1),并进行了高速摄影。IN718 钢板显示出多种变形和失效模式(隆起、盘形、花瓣形和堵塞)。所研究的弹丸/目标组合的弹道极限速度为 823 m s-1。对回收的弹丸和弹孔内壁进行了死后材料表征(光学摄影、扫描电子显微镜和能量色散光谱分析),观察结果表明弹丸材料存在绝热剪切、表面熔化和磨损。基于约翰逊-库克(Johnson-Cook)构成模型和失效准则建立的有限元模型再现了弹道实验。对死后弹丸和弹孔的尺寸以及弹丸的残余速度/质量进行了无量纲分析。在实验观察和弹丸动力学理论分析的基础上,将整个穿孔过程分为三个阶段(进入阶段、弹坑阶段和堵塞阶段)。考虑到空腔膨胀、弹丸变形和磨损的影响,建立了穿孔的多阶段分析模型,可以很好地预测弹丸在进入阶段和缩孔阶段的动力学特性。
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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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