摘要
介绍了无尾飞机布局方向控制特性风洞试验研究的主要结果。在两种典型布局上研究了扰流板、开裂副翼、机头边条、活动和偏转翼梢及舵面的方向控制特性。认为机头边条、开裂副翼、活动(偏转)翼梢及其舵面组合是一种极具潜力的方向控制方案,可供无尾飞机布局参考。
In this paper are presented the major wind tunnel test results for the direction control of the tailless aircraft configuration.Some unusual control surfaces such as spoiler,clam-shell aileron,body-nose strake,movable wing-tip are investigated on two typical configurations.It is considered that the body-nose strake,clam-shell aileron and movable wing-tip are the potential control device for the tailless aircraft direction control.The data can be referred to the tailless aircraft configuration.
出处
《流体力学实验与测量》
CSCD
北大核心
2003年第4期1-9,共9页
Experiments and Measurements in Fluid Mechanics
基金
国家重点实验室基金项目(00JS33.3.1KG2901)
关键词
方向控制
无尾飞机
风洞试验
扰流板
副翼
机头边条
翼梢
舵面
布局
direction control
wind tunnel test
spoiler
cham-shell aileron
body-nose strake
movable wing-tip
