北京理工大学 爆炸科学与技术国家重点实验室, 北京 100081
*邮箱: zhilingbai@bit.edu.cn;
**邮箱: duanzp@bit.edu.cn
收稿:2022-05-22,
网络出版:2023-09-06,
纸质出版:2023-08-30
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刘泓甫, 黄风雷, 白志玲, 等. 刚性弹体带攻角斜侵彻贯穿混凝土靶板的理论模型[J]. 兵工学报, 2023,44(8):2381-2390.
Hongfu LIU, Fenglei HUANG, Zhiling BAI, et al. Theoretical Model of Oblique Penetration of Rigid Projectiles into Concrete Targets at Attack Angles[J]. Acta Armamentarii, 2023, 44(8): 2381-2390.
刘泓甫, 黄风雷, 白志玲, 等. 刚性弹体带攻角斜侵彻贯穿混凝土靶板的理论模型[J]. 兵工学报, 2023,44(8):2381-2390. DOI: 10.12382/bgxb.2022.0423.
Hongfu LIU, Fenglei HUANG, Zhiling BAI, et al. Theoretical Model of Oblique Penetration of Rigid Projectiles into Concrete Targets at Attack Angles[J]. Acta Armamentarii, 2023, 44(8): 2381-2390. DOI: 10.12382/bgxb.2022.0423.
为对弹体带攻角斜侵彻贯穿混凝土靶板弹道和弹体姿态进行快速预估
在开坑阶段基于弹体表面应力分布确定弹体载荷
将攻角作用最明显的开坑阶段细分为弹头进入阶段和完全进入后的剩余开坑阶段
同时考虑斜侵彻时自由表面效应及弹靶接触区域变化对弹体受力的影响
建立弹体带攻角斜侵彻混凝土靶的开坑模型。结合弹体斜侵彻贯穿混凝土靶的姿态偏转理论模型中隧道和剪切冲塞阶段模型
构建刚性弹体带攻角斜侵彻贯穿混凝土靶板理论模型
出靶余速与偏转角计算结果与实验吻合较好。模型对给定工况的计算结果表明
在一定倾角条件下
正攻角会加剧弹体的偏转并降低弹体的侵彻能力
负攻角会抑制弹体的偏转且适当的负攻角可提高弹体的侵彻能力。
To facilitate the pre-estimation of the trajectory and attitude of rigid projectiles obliquely penetrating into concrete targets at attack angles
an theoretical model of rigid projectiles obliquely penetrating into concrete targets at attack angles is proposed to predicate the influence of attack angle on the motion state of projectiles. This paper offers a new method for calculating the projectile load at the cratering stage by its surface stress distribution
and subdivides the cratering stage into the entering stage of the projectile nose and the remaining stage after the full entry as it is considered that the attack angle has most obvious effects at the cratering stage. Moreover
the influence of free surface effect and contact area change on the stress of the projectile body is considered in the cratering model. Then the tunnel and shear plugging model in the theoretical model of attitude deflection is used to predict the whole process of a rigid projectile obliquely penetrating into a concrete target at an attack angle. The computational results of the motion state of the projectile under different penetration situations are proved to be in good agreement with the experimental data. Moreover
the results show that at an oblique angle
the positive attack angle will aggravate the deflection and reduce the penetration ability
while the negative attack angle will inhibit the deflection and the penetration ability can be improved when the negative attack angle is in the right range.
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吴普磊 , 李鹏飞 , 董平 , 等 . 攻角对弹体斜侵彻多层混凝土靶弹道偏转影响的数值模拟及试验验证 [J ] . 火炸药学报 , 2018 , 41 ( 2 ): 202 - 207 . DOI: 10.14077/j.issn.1007-7812.2018.02.017 http://doi.org/10.14077/j.issn.1007-7812.2018.02.017 为了减小炸药装药膨胀力对弹体后端盖的力学危害,采用端羟基聚丁二烯(HTPB)为黏结剂、2,4-甲苯二异氰酸酯(TDI)为固化剂、二月桂酸二丁基锡(T-12)为催化剂,成功制备了一种多孔性缓冲材料;采用力学实验机、SEM等测试方法研究了固化温度对HTPB发泡特性和缓冲材料内部结构、压缩率的影响。结果表明,固化温度对HTPB发泡体积影响显著,在30~70℃范围内,随着固化温度的增加,发泡体积从0.12cm<sup>3</sup>增至0.56 cm<sup>3</sup>;90℃固化时发泡体积从0.56 cm<sup>3</sup>减小至0.45 cm<sup>3</sup>。压缩率在70℃时达到最大值,为65%。根据不同固化温度下缓冲材料的内部结构和压缩率,确定气孔直径均匀,压缩率最大时的温度(70℃)作为缓冲材料的固化温度。
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CHEN W X , ZHANG Y Y , GUO Z K , et al . Penetration of rigid projectile into concrete target with effect of attack angle: theory and experiment [J ] . International Journal of Structural Stability and Dynamics , 2017 , 17 ( 8 ): 1750080 . DOI: 10.1142/S0219455417500808 http://doi.org/10.1142/S0219455417500808 https://www.worldscientific.com/doi/abs/10.1142/S0219455417500808 https://www.worldscientific.com/doi/abs/10.1142/S0219455417500808 The existing prediction methods of penetration depth do not take the influence of attack angle or angular velocity of projectile (i.e. effect of attack angle) into account. The main purpose of this work is to develop an approximate approach to predict the penetration depth for a rigid projectile into concrete target covered with yaw-inducing overlays. A quasi-static, elastic–plastic contact model of projectile impacting on irregular barrier is built based on Hertz’s contact theory, and the expression of effect of attack angle are also presented. The stress on projectile–target interface is derived according to spherical cavity expansion model and mechanical property of target, where reduction coefficient is introduced to consider the effect of free surface, and the penetration resistances are further obtained. Differential equations of motion for projectile arbitrarily oblique into target covered with yaw-inducing overlays are given by employing the initial conditions of projectile striking on irregular barrier. Then a simplified formula of depth-of-penetration (DOP) with effect of attack angle is presented by introducing an influence coefficient of oblique impact and an influence coefficient of yaw-inducing overlays into the depth of normal penetration. Predictions from the simplified formula are validated by comparison with ballistic experimental data for a 57[Formula: see text]mm diameter, 4.44[Formula: see text]kg, and ogive-nose, semi-armor-piercing with striking velocities between 320 and 705[Formula: see text]m/s.
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DUAN Z P , LI S R , MA Z F , et al . Attitude deflection of oblique perforation of concrete targets by a rigid projectile [J ] . Defence Technology , 2020 , 16 ( 3 ): 596 - 608 . DOI: 10.1016/j.dt.2019.09.009 http://doi.org/10.1016/j.dt.2019.09.009 A perforation model is developed to predict the attitude deflection in the oblique perforation of concrete targets by a rigid projectile, in which the inertial moment of the projectile is introduced, together with taking the attitude deflection during the shear plugging sub-stage into account, and the shape of the plug formed on the rear surface of target is also re-investigated. Moreover, a new classification of concrete targets is proposed based on the target thickness, with which the attitude deflections in different kinds of concrete targets are analyzed. It is found that the numerical results by using the new perforation model are in good agreement with the previous experimental data and simulated results. Furthermore, the variations of the attitude deflection with the initial conditions (the initial attitude angle and the initial impact velocity) are investigated. © 2019 The Authors
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