Ballistic protection and damage mechanism of ceramic composite armor under two-dimensional pre-stressed constraints by molten metal casting

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-02-06 DOI:10.1016/j.ast.2025.110021
Fangfang Qi , Cheng Wang , Wenlong Xu
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Abstract

To meet the requirements for lightweight and high-performance protection in ceramic composite armor, two-dimensional prestressing of brittle ceramics is achieved based on the principle of molten metal cooling shrinkage. The protective performance of two-dimensional prestressed (2DP) and non-prestressed (2DN) ceramic composite armors is evaluated through ballistic impact tests. High-speed cameras and 3D digital image correlation (3D-DIC) techniques are employed to dynamically capture the penetration and damage processes of the ceramic composite armor targets. The Rosin-Rammler distribution model is used to analyze and compare the fragmentation degrees of ceramic targets after penetration. Additionally, full process coupled simulation, encompassing the preparation and the ballistic impact of ceramic composite target, is achieved through the finite element software ProCast and Ls-Dyna. Based on the depth of penetration (DOP) test, the residual depth of witness after penetration is measured, and the protection coefficients of two type of target at different velocities are quantitatively obtained. The experimental and simulation results indicate that, 2DP ceramic composite armor demonstrates better ballistic protection capability compared to 2DN ceramic composite armor. The presence of prestress prolongs the dwell time of the projectile on the projectile-facing surface, which hinders the forward movement of the projectile, resulting in significant velocity attenuation and radial deformation of projectile's nose. Additionally, the fragment size of 2DP ceramic composite armor is smaller, and the ceramic fragmentation energy absorption continuously dissipates the kinetic energy of projectile. Within a velocity range of 600 m/s∼1400 m/s, the protection coefficient of 2DP is 8.11 % to 48.64 % higher than that of 2DN.
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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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