摘要
本文叙述了具有全动翼的战术导弹出现“反操纵”气动问题,分析其原因及流态,并简要叙述解决办法。
The paper describes the aerodynamical problem of the 'anti-control' of tactical missiles with moving-wings, analyses its cause and the flow construction and gives the solution in brief.
出处
《系统工程与电子技术》
EI
CSCD
1993年第1期78-80,F003,共4页
Systems Engineering and Electronics
关键词
全动尾翼
战术导弹
气动
操纵性
Moving-wing, Tactical missile, Aerodynamics, Anti-control.
