1. 北京理工大学 爆炸科学与安全防护全国重点实验室, 北京 100081
2. 北京理工大学重庆创新中心, 重庆 401120
3. 北京理工大学长三角研究院(嘉兴), 浙江 嘉兴 314019
* liuyan@bit.edu.cn
收稿:2024-11-19,
网络出版:2025-09-24,
纸质出版:2025-09-30
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时振清, 刘彦, 王晓锋, 等. 类椭圆截面弹侵彻有限厚混凝土靶板弹道特性[J]. 兵工学报, 2025,46(9):241051.
Zhenqing SHI, Yan LIU, Xiaofeng WANG, et al. Ballistic Characteristics of Quasi-elliptical Cross-section Projectile Penetrating into Finite-thick Concrete Target[J]. Acta Armamentarii, 2025, 46(9): 241051.
时振清, 刘彦, 王晓锋, 等. 类椭圆截面弹侵彻有限厚混凝土靶板弹道特性[J]. 兵工学报, 2025,46(9):241051. DOI: 10.12382/bgxb.2024.1051.
Zhenqing SHI, Yan LIU, Xiaofeng WANG, et al. Ballistic Characteristics of Quasi-elliptical Cross-section Projectile Penetrating into Finite-thick Concrete Target[J]. Acta Armamentarii, 2025, 46(9): 241051. DOI: 10.12382/bgxb.2024.1051.
为探索类椭圆截面弹体侵彻有限厚混凝土靶板的弹道特性
开展了类椭圆截面弹体正、斜侵彻不同厚度混凝土靶实验。结合有限元-光滑粒子伽辽金数值模拟方法
研究类椭圆截面弹体不同侵彻阶段纵向加速度和弹道偏转角度的变化趋势
分析着靶速度、靶板厚度、着靶倾角、滚转角和攻角等因素对弹道偏转的影响规律。研究结果表明:类椭圆截面弹体正侵彻有限厚靶板时
弹道会向小端侧偏转
且随着靶板厚度的增加
弹道偏转角随之增大;通过数值模拟分析发现弹道偏转主要发生在隧道阶段和冲塞阶段
开坑阶段造成的偏转仅为最终偏转角度的1.4%;存在一个临界着靶速度
使高于此速度下的正侵彻弹道偏转角随着侵彻速度增加而减小
低于此速度时变化规律相反
临界速度随靶厚增加呈现先上升、再下降至稳定值的非单调变化规律;弹体以同一倾角斜侵彻时
随着攻角的增加(-6°~ 6°)
弹道由向下偏转变为向上偏转
当攻角为2°时
在0°~ 30°着靶倾角范围内
具有良好的弹道稳定性;在
Oxz
平面上
弹体姿态的稳定性随滚转角的增大总体上呈先减弱、后增强的趋势
当滚转角小于150°
弹体结束与靶体作用后
弹体呈现负攻角。
To investigate the ballistic characteristics of a quasi-elliptical cross-section projectile penetrating into finite-thick concrete target
the tests are made on the normal and oblique penetrations of quasi-elliptical cross-section projectiles into the concrete targets with different thicknesses.The variation trends of the longitudinal acceleration and trajectory deflection angle of projectile during different penetrating stages are analyzed through the numerical simulation using the finite element method-smooth particle Galerkin (FEM-SPG) algorithm.The effects of impa
ct velocity
target plate thickness
oblique angle
rolling angle and angle of attack on the trajectory deflection are discussed.The research results show that the trajectory deflects toward the flatter surface and the deflection mainly occurs in the tunnel stage and the plugging stage when a quasi-elliptical cross-section projectile penetrates into a target plate with finite thickness.As the thickness of the target plate increases
the trajectory deflection angle increases.The deflection caused at the cratering stage is only 1.4% of the final deflection angle in numerical simulation.There is a critical impact speed
which makes the deflection angle of the normal penetration trajectory decrease with the increase of the penetration speed above this target impact speed
while below this critical value
an inverse relationship is observed.Furthermore
the critical speed demonstrates non-monotonic dependence on target thickness
exhibiting an initial increase followed by progressive reduction until stabilization occurs.The trajectory changes from downward deflection to upward deflection with the increase in the angle of attack (-6°-6°) when the projectile penetrates into a target at the same oblique angle.The trajectory has excellent stability within the range of 0°-30° oblique angle at 2° angle of attack.The attitude stability of the projectile generally weakens first and then increases with the increase of the rolling angle on
Oxz
plane.When the rolling angle is less than 150°
the projectile shows a negative angle of attack after it ends interacting with the target.
董恒 , 黄风雷 , 武海军 , 等 . 异形弹体高速侵彻/穿甲机理研究进展 [J ] . 兵工学报 , 2024 , 45 ( 9 ): 2863 - 2887 . DOI: 10.12382/bgxb.2024.0040 http://doi.org/10.12382/bgxb.2024.0040 为支撑超高声速武器终点毁伤效应评估,满足异形弹体侵彻力学理论发展需求,异形弹体侵彻机理是当前亟需研究的关键基础科学问题。对异形弹体侵彻行为、弹靶作用机制、弹道稳定性与结构响应研究现状进行全面综述,对现有研究工作进行梳理与总结,搭建异形弹体侵彻问题研究的基本框架;以异形弹体侵彻/穿甲过程中出现的新质弹靶作用现象、机理为脉络,突出异形弹体结构对载荷环境表征、弹道及结构稳定性控制等方面带来的新挑战,并提出了异形弹体未来研究的3个建议,供相关研究者参考。
DONG H , HUANG F L , WU H J , et al. Penetration and perforation mechanism of high-speed non-circular projectiles a-state-of-the-art review [J ] . Acta Armamentarii , 2024 , 45 ( 9 ): 2863 - 2887 . (in Chinese) DOI: 10.12382/bgxb.2024.0040 http://doi.org/10.12382/bgxb.2024.0040 To support the theoretical design of the hypersonic missile’s terminal effect and meet the development demand of penetration mechanics theory of non-circular projectiles, the penetration mechanism of non-circular projectilesis a key scientific problem required to be solved. A comprehensive review is conducted on the penetration behavior, penetration mechanism, ballistic stability, and structural response of non-circular projectiles.It is a review and summary of the existing research work, aiming to establish a basic framework for researching the penetration problem of non-circular projectiles.Moreover, the new phenomena and mechanisms introduced by the structural changes of non-circular projectiles are highlighted. Three suggestions for the future research of the non-circular projectiles are put forward for the reference of relevant researchers.
邓希旻 , 武海军 , 董恒 , 等 . 椭圆截面截锥弹体的高速穿甲特性及阻力模型 [J ] . 爆炸与冲击 , 2023 , 43 ( 9 ): 104 - 120 .
DENG X M , WU H J , DONG H , et al. A study of high-velocity penetration characteristics and resistance model of elliptical cross-section truncated ogive projectile [J ] . Explosion and Shock Waves , 2023 , 43 ( 9 ): 104 - 120 . (in Chinese)
田泽 , 王浩 , 武海军 , 等 . 椭圆变截面弹体斜贯穿薄靶姿态偏转机理 [J ] . 兵工学报 , 2022 , 43 ( 7 ): 1537 - 1552 . DOI: 10.12382/bgxb.2021.0367 http://doi.org/10.12382/bgxb.2021.0367 随着新型武器平台的发展,具有良好平台适应性、高升阻比及隐身性能等特点的异形截面(椭圆形及变截面椭圆形)战斗部开始受到广泛关注。为探究椭圆变截面弹体斜贯穿薄靶机理与姿态偏转规律,对3种不同截面(圆形、椭圆形、变截面椭圆形)弹体斜贯穿双层945舰船薄钢板实验过程及结果进行整理与分析,根据椭圆变截面弹体贯穿过程、靶板破坏失效模式与弹体受力特征,将贯穿过程分为弹体头部压入阶段、弹体头部贯穿阶段、过渡阶段与弹身贯穿阶段。基于能量守恒、虚功原理分阶段分析弹体受力特征,建立弹体姿态偏转理论模型。通过对已有实验和数值模拟结果与理论模型所得结果进行对比,验证理论模型的可靠性。采用该理论模型着重讨论弹体撞击速度、初始倾角、质心位置、弹体翻滚角及椭圆截面长短轴之比等参数对椭圆变截面弹体姿态偏转的影响。结果表明:随着椭圆变截面弹体初始撞击速度的增加,弹体姿态偏转角度呈现指数型减小趋势;随着椭圆变截面弹体初始倾角的增大,弹体姿态偏转量增大;随着椭圆变截面弹体质心位置的后置,弹体姿态偏转角度增大;椭圆变截面弹体以不同的翻滚角撞击靶板时,弹体姿态偏转角度不同,γ<sub>pt</sub>=0°较γ<sub>pt</sub>=90°时弹体姿态偏转角度更大;当γ<sub>pt</sub>=0°时,椭圆变截面弹体椭圆截面长短轴之比增大,弹体姿态偏转角度随之增大;当γ<sub>pt</sub>=90°时,规律则相反。
TIAN Z , WANG H , WU H J , et al. Attitude deflection mechanism of projectiles with variable elliptical cross-sections obliquely perforating thin targets [J ] . Acta Armamentarii , 2022 , 43 ( 7 ): 1537 - 1552 . (in Chinese) DOI: 10.12382/bgxb.2021.0367 http://doi.org/10.12382/bgxb.2021.0367 With the development of new weapon platforms, warheads with novel cross-sections (elliptical and variable elliptical cross-sections) have drawn wide attention due to high platform adaptability, lift-drag ratio, and stealth performance. This study investigates the oblique penetration mechanism and the attitude deflection of projectiles with variable elliptical cross-sections by examining projectiles with three types of cross-sections (circle,elliptic,and tapered elliptic) obliquely penetrating a double-layer thin steel plate through experiments. Based on the failure mode of the target plate and the mechanic characteristics of the projectile body, the penetration process is divided into four stages, namely press-in of the projectile nose, penetration of the nose, transition, and penetration of the projectile body. The mechanic characteristics of each projectile at each stage are also analyzed based on the law of energy conservation and virtual work principle. A theoretical model is constructed for the projectile's attitude deflection. The theoretical model is validated through comparing the experimental and simulation results. The model is used to study how the attitude deflection of projectiles with variable elliptical cross-sections is affected by different parameters, including impact velocity, initial oblique angle, centroid position, roll angle, and the long to short axis ratio of the elliptical cross-sections. The results show that as the impact velocity of the projectile increases, the attitude deflection angle decreases exponentially; the deflection increases as the initial oblique angle increases; the deflection increases as the centroid moves away from the projectile nose; the deflection angles vary when the projectile hits the target from different rolling angles; the deflection at γ<sub>pt</sub>=0° is greater than that when γ<sub>pt</sub>=90°; as the long to short axis ratio increases, the deflection increases when γ<sub>pt</sub>=0°, yet it decreases when γ<sub>pt</sub>=90°.
蒋腾 , 武海军 , 邓希旻 , 等 . 变截面弹体斜侵彻两层间隔钢靶弹道特性 [J ] . 兵工学报 , 2025 , 46 ( 2 ): 240019 . DOI: 10.12382/bgxb.2024.0019 http://doi.org/10.12382/bgxb.2024.0019 为研究变截面弹体斜侵彻两层间隔钢靶时结构特征对弹道特性的影响规律,开展椭圆等截面、椭圆变截面弹体在1020m/s初速、5°着角条件下斜侵彻两层间隔钢靶实验,结合数值模拟对比圆等截面、椭圆等截面、圆变截面和椭圆变截面弹体在斜侵彻钢靶过程中的弹道轨迹、速度、偏转角、纵向位移和纵向加速度的变化情况,揭示变截面弹体结构特征影响弹道稳定性的物理机制。研究结果表明:当弹体初始撞击速度较大、弹肩处横截面面积一致及变截面角度在0°~2.5°范围内时,不同横截面形状和变截面角度弹体在斜侵彻两层间隔钢靶过程中的速度变化差异很小;对于变截面弹体,可以通过改变变截面结构特征找到一个使得弹体贯穿首层靶板后纵向位移基本为零的临界变截面角度;不同横截面形状的变截面弹体受变截面角度对贯穿钢靶后纵向运动、姿态偏转的敏感程度不同,横截面形状的长短轴之比越大,变截面角度对偏转角速度的影响越大;变截面角度会影响弹体穿靶过程中的受力方向,可能导致弹体受力出现反转现象。相关研究对变截面弹体结构特征参数的优化、变截面弹体斜侵彻两层间隔钢靶弹道特性预测具有较好的指导价值。
JIANG T , WU H J , DENG X M , et al. Ballistic characteristics of variable section projectile obliquely penetrating two-layer spacer steel targets [J ] . Acta Armamentarii , 2025 , 46 ( 2 ): 240019 . (in Chinese) DOI: 10.12382/bgxb.2024.0019 http://doi.org/10.12382/bgxb.2024.0019 The influence of the structural characteristics of variable cross-section projectile on the ballistic characteristics during obliquely penetrating the two-layer spaced steel targets is studied.The elliptical and variable cross-section projectiles obliquely penetrate a two-layer spaced steel target at an initial velocity of 1020m/s and an impact angle of 5° in the experiments.The trajectories,velocities,deflection angles,longitudinal displacements and longitudinal accelerations of circular and elliptical equal cross-section projectiles,and circular-and elliptical-variable cross-section projectiles during obliquely penetrating the steel target are compared by numerical simulations,and the physical mechanism of which the structural characteristics of variable cross-sectional projectile affect the stability of its trajectory is revealed.The results indicate that,when the initial impact velocity of projectile is high,the cross-sectional area at the shoulder of projectile remains consistent,and the variable cross-sectional angle is within the range of 0° to 2.5°,the velocity variations of projectiles with different cross-sectional shapes and variable cross-sectional angles during obliquely penetrating two-layer spaced steel targets are very small.For the variable cross-section projectile,a critical variable cross-section angle can be found by changing the structural characteristics of variable cross-section projectile,which makes the longitudinal displacement of the projectile penetrating the first-layer target plate basically zero.Different cross-sectional shapes of variable cross-sectional projectiles have different sensitivities to longitudinal motion and attitude deflection after penetrating the steel target at variable cross-sectional angles.The greater the ratio of long axis to minor axis of cross-sectional shape is,the greater the influence of variable cross-sectional angle on the deflection angular velocity is.Variable cross-section angle has an affect the force direction of the projectile during the process of penetrating the target,which may lead to the reversal of force on the projectile.The relevant studies have good guiding value for the optimization of structural characteristic parameters of variable cross-sectional projectile and the prediction of trajectory characteristics of variable cross-sectional projectiles during obliquely penetrating two-layer spaced steel targets.
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