首页 | 本学科首页   官方微博 | 高级检索  
     

某型飞机的结构毁伤计算与仿真实现
引用本文:潘庆军,熊腊森,杜晓伟.某型飞机的结构毁伤计算与仿真实现[J].弹箭与制导学报,2007,27(1):129-131.
作者姓名:潘庆军  熊腊森  杜晓伟
作者单位:1. 空军第一航空学院,河南,信阳,464000;华中科技大学,武汉,430074
2. 华中科技大学,武汉,430074
3. 空军第一航空学院,河南,信阳,464000
摘    要:通过对我军某型飞机的结构易损性分析和离散杆的空间分布与飞行姿态规律的分析,建立了空战对抗中,飞机结构在离散杆式战斗部打击下的毁伤计算模型。通过仿真实现,能够获得一定弹目交会条件下飞机结构的毁伤状态、损伤尺寸和损伤形态,有助于开展离散杆式战斗部威胁下的飞机结构的生存力分析及战伤模式研究。

关 键 词:易损性  离散杆  仿真  战伤模式
收稿时间:2006-05-31
修稿时间:2006-05-312006-08-31

Structure Damage Calculation and Simulation of an Aircraft
PAN Qing-jun,XIONG La-sen,DU Xiao-wei.Structure Damage Calculation and Simulation of an Aircraft[J].Journal of Projectiles Rockets Missiles and Guidance,2007,27(1):129-131.
Authors:PAN Qing-jun  XIONG La-sen  DU Xiao-wei
Affiliation:1.The First Aeronautical Institute of Air Force, Henan Xinyang 464000,China; 2.Huazhong University of Science and Technology,Wuhan 430074,China
Abstract:Through the analysis of structure vulnerability of an aircraft and space distribution and flight attitude of discrete rod, the models to calculate the damage of an aircraft affected by the discrete rod warhead under some crossing conditions are established. By simulation, survivability as well as damage dimension and form of aircraft structures is got, which helps to research the structure survivability and battle damage mode of aircraft under the threat of discrete rod warhead.
Keywords:vulnerability  discrete rod  simulation  battle damage mode
本文献已被 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号