摘要
为获取飞机在导弹打击后的毁伤状态及战伤数据,指导军队战时战伤抢修和战场备件筹措,有效恢复作战能力,本文建立某型主战飞机的易损性模型、结构件模型及相关计算模型,分析了飞机在破片型战斗部打击下的生存力及损伤情况。计算结果实施了地面实弹打击试验及战伤抢修训练,为战伤飞机进行战伤模式分析、战伤评估和抢修方案的制定提供了重要依据,提高了飞机持续作战能力。
To obtain the injuring state and analysis data of the battle damage aircraft under the threat of the enemy guided missile, and guide the aircraft battle damage repair (ABDR) and the raise of battle field spare part, the vulnerability, structure and relevant calculating models are established and the aircraft survivability and battle damage under the attacks of the fragment warhead are analyzed. The simulation data guide the ground ball firing experiment and ABDR training for air force, thus it is helpful to analyze the battle damage mode, battle damage assessment, and repair projects, thus improving the persistent battle ability of the aircraft.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
2008年第2期205-208,共4页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
计算
导弹
飞机战伤抢修
易损性
破片杀伤战斗部
calculations
missiles
aircraft battle damage repair (ABDR)
vulnerability
fragmentation kill warhead