摘要
阐述了襟翼涡流发生器、主翼后缘偏折技术、Zhu’s襟翼、自激励运动襟翼、零质量射流、等离子体技术以及动力增升等各类主动控制技术的工作原理及其增升效果分析和具体应用情况.结果表明,这些流动控制新技术对于进一步提高民用飞机的增升效果具有巨大的潜力.
In this paper, many kinds of flow control is introduced from the working principle, lift enhancing efficiency and the application. The flow control includes vortex generators on flap, spoiler deflection, ZHU＇s flap, self-activated movable flap, zero mass actuation, plasma actuators, dynamical lift enhancing, and so on. The analysis results indicate that, these flow control technique has great potential for improving the lift enhancing efficiency of civil aircraft.
出处
《上海交通大学学报》
EI
CAS
CSCD
北大核心
2014年第2期214-221,共8页
Journal of Shanghai Jiaotong University
关键词
民用飞机
增升装置
流动控制
涡流发生器
civil aircraft
high lift device
flow control
vortex generator
