计算机与数字工程2011，Vol.39Issue(8)：4-7,4.
破片对飞机壁板冲击损伤仿真研究
Study on Simulation of Fragment Impact Integral Panel of an Aircraft
陈国乐 1李海兵 2康建设 1刘夺3
作者信息
- 1. 军械工程学院装备指挥管理系 石家庄050003
- 2. 成都军区空军95633部队 成都550031
- 3. 沈阳军区空军93363部队 公主岭136100
- 折叠
摘要
Abstract
The objective of this paper is to simulation of basing on Aircraft Battle Damage Assessment and RepairCAB-DR) for resource required. It focuses on develop a simulation of penetration condition totally for fragments. It is simulated a three-dimensional finite element model to get K file, and obtain results via ANSYS/LS-DYNA, get damage of effective from velocity of discrete rod and thickness of target, compare data from simulation with equation to damage of integral panel. Results are presented in terms of images of damages as well as area removed. These results are consistent with the former. The results can be used in a rapid assessment of a battle-damaged aircraft repair and as a reference for the usual repair of aircraft.关键词
离散杆/飞机整体壁板/ANSYS/LS-DYNA/损伤/侵彻Key words
discrete rod/integral panel/ANSYS/LS-DYNA/damage/penetration分类
军事科技引用本文复制引用
陈国乐,李海兵,康建设,刘夺..破片对飞机壁板冲击损伤仿真研究[J].计算机与数字工程,2011,39(8):4-7,4.
