摘要
本文建立了任意风场中带有机动襟翼的飞机的纵向小扰动模型,研究了在下击暴流中,机动襟翼对飞机动态特性的影响,以及接通或断开机动襟翼控制系统的瞬间飞机的稳定性。所得结果对带机动襟翼的飞机的设计有一定参考价值。
This paper sets up a small disturbed longitudinal model of an aircraft with maneuver flaps in any wind field and studies the influence of maneuver flaps on the dynamic properties in downburst. The stability of aircraft is also considered while the flap control systems are switched on or cut off abruptly in downburst. The results given in this paper are useful in designing aircrafts with maneuver flaps.
出处
《飞行力学》
CSCD
北大核心
1991年第2期39-47,共9页
Flight Dynamics
关键词
飞机
机动襟翼
稳定性
动态特性
aircraft
maneuver flap
stability
dynamic property
downburst.
