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作 者:屈可朋[1] 吴翰林 郭洪福 肖玮[1] 胡雪垚 QU Kepeng;WU Hanlin;GUO Hongfu;XIAO Wei;HU Xueyao(Xi'an Modern Chemistry Research Institute,Xi'an 710065,China)
出 处:《弹道学报》2022年第1期45-50,共6页Journal of Ballistics
基 金:基础性科研院所稳定支持科研项目。
摘 要:为优化弹体头部外形,减小侵彻过程头部侵蚀对弹道偏转的影响,进而提升弹体斜侵彻多层靶弹道稳定性,设计了一种复合式侵彻体,利用ANSYS/LS-DYNA,计算了复合式侵彻体以500~800 m/s速度侵彻3层间隔钢靶的弹道偏转情况,对比了复合式与整体式侵彻体弹道偏移量,探讨了帽罩材质对复合式侵彻体弹道的影响机制,并进行了实验验证。结果表明:在500~800 m/s速度范围内,复合式侵彻体侵彻各层及最终弹道偏移量均明显小于整体式侵彻体,随着侵彻速度由500 m/s增加至800 m/s,弹道稳定性分别提升54%、50%、60%和32%;在500 m/s侵彻速度下,35CrMnSiA帽罩复合式侵彻体弹道偏移总量略小于93WNiFe帽罩复合侵彻体,当速度增大至800 m/s时,93WNiFe帽罩复合式侵彻体的弹道最终偏移量小于35CrMnSiA帽罩复合式侵彻体。In order to optimize the shape design of the projectile head,reduce the impact of head erosion on ballistic deflection during penetration,and then improve the ballistic stability of the projectile oblique penetration into multi-layer targets,a composite penetrator was designed.The ballistic deflection of the composite penetrator penetrating three-layer spaced steel target at the velocity of 500-800 m/s was calculated by ANSYS/LS-DYNA.The ballistic offset of the composite penetrator and the integral penetrator was compared,and the influence mechanism of the cap material on the trajectory of the composite penetrator was discussed.Experimental verification was carried out.The results show that in the velocity range of 500-800 m/s,the penetration of each layer and the final ballistic offset of the composite penetrator are significantly smaller than those of the integral penetrator.With the penetration velocity increasing from 500 m/s to 800 m/s,the ballistic stability increases by 54%,50%,60%and 32%respectively.At the penetration speed of 500 m/s,the total ballistic offset of 35CrMnSiA cap composite penetrator is slightly less than that of 93WNiFe cap composite penetrator.When the speed increases to 800 m/s,the final ballistic offset of 93WNiFe cap composite penetrator is less than that of 35CrMnSiA cap composite penetrator.
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