检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
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)
机构地区:[1]海军航空大学航空作战勤务学院,山东烟台264001
出 处:《兵工自动化》2023年第10期4-7,共4页Ordnance Industry Automation
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.
关 键 词:毁伤效果评估 机场跑道 经验公式 仿真 侵彻着角
分 类 号:TJ762.21[兵器科学与技术—武器系统与运用工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.7