摘要
以某飞翼飞机为例,讨论了典型飞翼飞机的基本操稳特性和动态特性。并对飞翼布局飞机和常规布局飞机的主要气动导数作了对比研究,简要说明了二者在操稳特性上的不同之处及其产生的原因,为控制增稳系统的设计提供了依据。
A flying wing aircraft has many very different characteristics on stability and manoeuvrability compared to a traditional aircraft. This paper takes the flying wing aircraft FWX1 as an example to explain the stability and manoeuvrability of a flying wing aircraft, which is the base for control and stability augmentation system design.
出处
《飞行力学》
CSCD
北大核心
2006年第3期17-21,共5页
Flight Dynamics
关键词
飞翼
无尾飞机
操稳特性
flying wing
tailless aircraft
stability and manoeuvrability
