摘要
论述了反坦克导弹、制导航弹、末制导炮弹、制导火箭等制导兵器常用的气动布局和特点;分析了制导兵器的新型气动布局及特点;论述了制导兵器的发展趋势是远射程、高机动、高精度、大威力和高隐身;指出了制导兵器发展中必须研究解决的关键气动力技术问题.
Aerodynamic configurations in general use and aerodynamic characteristics of guided weapons, e.g. of antitank missiles, guided bombs, terminally guided projectiles, guided rockets etc., are summarized. Some new aerodynamic configurations of guided weapons and correspond-ing characteristics are analyzed. It is shown that the trends of development in guided weapons are toward long range, high maneuverability, high accuracy, high power and high stealthy. The key aerodynamic techniques to be predetermined during the development of guided weapons are pointed out and discussed.
出处
《北京理工大学学报》
EI
CAS
CSCD
北大核心
2003年第6期665-670,共6页
Transactions of Beijing Institute of Technology
基金
国家部委预研项目(4013130302)
关键词
制导兵器
气动布局
气动特性
滑翔增程
气动弹性
锥形运动
guided weapons
aerodynamic configuration
aerodynamic characteristics
extended gliding range
aeroelasticity
conical motion
