爆炸动载下金属柱壳破片速度场分布研究OA北大核心CSTPCD
Velocity field distribution of metal cylinder fragments under explosive dynamic load
针对格尼(Gurney)公式无法描述破片速度场沿圆柱壳体轴向变化的问题,该文通过AUTODYN软件建立仿真模型,分析了长径比和壳体壁厚对破片速度场分布的影响.考虑爆炸加载下壳体断裂过程,修正了 Gurney公式.基于上述研究,将壳体长径比和相对壁厚引入指数形式的修正因子中,建立了破片速度场轴向分布模型.通过实验验证了该模型的合理性.研究结果表明:对于圆柱形战斗部,相对壁厚为常数,长径比越大,战斗部形成破片速度越接近v.;长径比为常数,壳体相对壁厚越小,战斗部形成破片速度越接近v0.将该文理论结果与Gurney理论结果以及实验结果进行对比,该文理论结果误差均在7%以内,大部分误差小于3%,与实验结果更加吻合,验证了该文建立的破片速度场轴向分布模型的合理性.该文理论模型可为杀伤战斗部破片参数精准设计提供参考.
Aiming at the problem that Gurney formula cannot reflect the axial variation of fragment velocity field along the shell,a simulation model is established by AUTODYN software to analyze the effects of aspect ratio and shell thickness on fragment velocity field distribution.The Gurney formula is modified by considering the shell fracture process under explosive loading.Based on the above research,the axial distribution model of fragment velocity field is established by introducing the shell length diameter ratio and relative wall thickness into the exponential correction factor.Finally,the rationality of the model is verified by experiments.The results show that for cylindrical warhead,the relative wall thickness is constant,and the greater the aspect ratio is,the closer the fragment formation velocity is to v0.When the aspect ratio is constant,the smaller the relative wall thickness of the shell is,the closer the fragment formation speed of the warhead is to v0.By comparing the theoretical results of this paper with the Gurney theoretical results and experimental results,the errors of the theoretical results of this paper are all within 7%,and most of the errors are less than 3%,which is more consistent with the experimental results,which verifies the rationality of the fragment velocity field axial distribution model established here.The theoretical model here can provide reference for the precise design of fragmentation parameters of kill warheads.
朱建军;霍宪旭;李伟兵
中国直升机设计研究所,江西景德镇 333000南京理工大学机械工程学院,江苏南京 210094
力学
破片速度格尼公式圆柱壳体壁厚长径比数值模拟
fragment velocityGurney formulashell wallthicknesslength diameter rationumerical simulation
《南京理工大学学报(自然科学版)》 2024 (002)
148-154,174 / 8
国家自然科学基金(12002336)
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