摘要
针对相同速度下不同着角对于侵彻爆炸坑半径的影响,分析空地导弹着角与机场跑道毁伤弹坑半径之间的关系。对空地导弹侵彻段深度及爆炸坑半径进行预期,讨论着角对侵彻深度带来的影响,结合经验公式给出着角与爆炸坑之间的计算公式。结果表明:该分析能更好地体现单一影响因素在侵彻段对于毁伤效果的影响,为下一步作战筹划提供参考。
Aiming at the influence of different impact angles on the radius of penetration explosion crater under the same velocity,the relationship between the impact angle of air-to-ground missile and the radius of damage crater on airport runway is analyzed.The penetration depth and crater radius of the air-to-ground missile were predicted,and the influence of the impact angle on the penetration depth was discussed.Combined with the empirical formula,the calculation formula between the impact angle and crater was given.The results show that the analysis better reflects the impact of a single factor on the damage effect in the penetration phase,and provides a reference for the next operational planning.
作者
李健宁
张毅
张指辉
Li Jianning;ZhangYi;Zhang Zhihui(College of Aviation Combat Service,Naval Aviation University,Yantai 264001,China)
出处
《兵工自动化》
2023年第10期4-7,共4页
Ordnance Industry Automation
关键词
毁伤效果评估
机场跑道
经验公式
仿真
侵彻着角
damage effect evaluation
airport runway
empirical formula
simulation
penetration angle