首页|战斗部高速侵彻混凝土靶动态响应数值模拟研究

战斗部高速侵彻混凝土靶动态响应数值模拟研究

Numerical Simulation of Dynamic Response of Warhead Penetrating Concrete Target With High Velocity

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为研究冲击载荷下侵彻战斗部动态响应特性,基于弹-靶分离方法模拟了战斗部侵彻半无限混凝土靶过程,分析了不同装药与壳体头部曲径比、速度及尺寸下战斗部的动态响应,结果表明:装药的最大过载高于壳体最大过载,且装药最大过载、变形程度与装药头部曲径比正相关,应力波导致的装药变形主要分布于头部端面、头部与圆柱段过渡处.战斗部壳体头部曲径比(CRHS)增大,壳体及装药最大过载均呈降低趋势,且二者最大过载差值逐渐缩小,CRHS=4时装药的最大塑性应变约为CRHS=2时的29%,且高应变区域明显减小.侵彻初始速度主要影响过载幅值,初始速度越高,战斗部壳体和装药的过载、塑性变形程度越大.而对于不同尺寸的战斗部而言,在不考虑混凝土骨料尺寸、应变率等因素的影响下,战斗部的最大过载、侵彻深度、应力幅值等参量满足相似律,但装药变形程度不符合,战斗部尺寸越大,装药塑性变形越严重.
To investigate the dynamic response characteristics of penetration warhead under impact load,the simulation of warhead penetrating into a semi-infinite concrete target was conducted using the projectile-target separation method. The dynamic response of the warhead under different charge and shell head-curve-ratios,velocities,and sizes was analyzed. The results indicate that the deceleration peak of charge is higher than that of warhead shell. The deceleration peaks and deformation of the charge are positively correlated with the head curve ratio of charge. The deformation of the charge caused by stress wave is primarily concentrated on its end face and at the transition between the head and cylinder section. Increasing the head curve ratio(CRHS)of the warhead shell reduces deceleration peaks for both the shell and charge,as well as their maximum overload difference. Specifically,the maximum plastic strain of the charge at CRHS=4 is about 29% of that at CRHS=2,with a significant reduction in high strain area. The initial velocity of penetration mainly affects the overload amplitude. Furthermore,an increase in initial velocity results in higher overload and plastic deformation for both the shell and charge. Overload,penetration depth and stress amplitude adhere to similarity laws for different warhead-sizes,without considering factors such as concrete aggregate size and strain rate. However,larger warhead size results in more severe plastic-deformation of charge.

penetrating warheaddynamic responseprojectile-target separation methodnumerical calculation

盛强、孟繁霖、张先锋、刘闯

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南京理工大学 机械工程学院,江苏 南京210094

北京航天长征飞行器研究所,北京100074

侵彻战斗部 动态响应 弹-靶分离方法 数值计算

国家自然科学基金国家自然科学基金

1220220512141202

2024

弹道学报
中国兵工学会

弹道学报

CSTPCD北大核心
影响因子:0.483
ISSN:1004-499X
年,卷(期):2024.36(3)
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