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头部受冲击的锥形弹体结构动力响应研究

STUDY ON THE DYNAMIC RESPONSE OF A CONICAL PROJECTILE SUBJECTED TO IMPACT LOADING AT ITS NOSE

  • 摘要: 近年来, 高超声速武器凭借其打击速度和毁伤效能的优势得到了迅速发展. 为提高武器平台的空间利用率, 采用与平台共形的变截面战斗部成为重要的发展趋势. 然而, 战斗部外形的复杂化和速度的提高导致其载荷环境更加严酷, 结构强度问题突出. 为探究变截面弹体在非正侵彻条件下的结构动力响应规律, 文章基于空间自由梁和结构塑性理论, 建立了头部受冲击载荷作用的锥形弹体结构动力响应模型和轴力-弯矩耦合作用下的结构失效函数, 并借助Abaqus/Explicit非线性数值程序对典型锥形弹体的动力响应进行了仿真, 验证了理论模型的合理性和准确性. 在此基础上, 分析了弹体头部形状系数、锥度、径厚比和长径比等因素对弹体内力分布和失效位置的影响规律. 结果表明, 理论模型能够较准确地预测变截面弹体的内力分布规律; 头部集中质量降低了弹体的内力幅值, 但不影响其分布规律. 在冲击载荷、头部直径及其他无量纲参数相同的条件下, 弹体锥度越大, 危险位置越靠近弹体头部, 而长径比或径厚比增大会使弹体更易发生结构失效.

     

    Abstract: In recent years, hypersonic weapons have developed rapidly due to their advantages in attack speed and damage ability. In order to improve the space utilization of the platform, the adoption of variable cross-sectional warheads that have the same shape as the platform becomes an important developing trend. However, the increase in structural shape complexity and velocity results in extreme dynamic loading conditions, which lead to serious structural strength issues for warheads. To investigate the dynamic response of variable cross-sectional projectiles in oblique penetration scenarios, based on the free-free beam and structural plasticity theories, a dynamic response model and structural failure function with the coupling of axial force and bending moment considered were established for the conical projectile subjected to impact loading at its nose. Then, by means of Abaqus/Explicit nonlinear finite element analysis software, the dynamic responses of typical conical projectiles under different impact loadings at the nose were numerically simulated, and the rationality and accuracy of the proposed dynamic response model were verified. Based on the theoretical models, the influences of the structural parameters of projectiles, such as the shape coefficient of the projectile head, semi-conic angle, diameter-to-thickness ratio, as well as the length-to-diameter ratio were analyzed. The results showed that the theoretical model could predict the internal force distribution and failure locations of the conical projectiles very well. The nose mass of the projectile could decrease the magnitude of the internal forces, but does not change their non-dimensional distribution. When the impact loading, the diameter at the front part of the projectile, as well as the other nondimensional parameters keep constant, the increase of the semi-conic angle of the projectile induces a shift of the critical failure section toward the head, and the increase of the length-to-diameter ratio or diameter-to-thickness ratio makes the projectile more prone to structural failure.

     

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