摘要
概要介绍了现代飞机失速/尾旋研究的途径、失速/过失速/尾旋试飞验证的目的、试验方法和测试要求。较详细地介绍了现代飞机失速/过失速/尾旋试飞验证的程序和步骤,对装有迎角限制器飞机的特殊要求,应急改出尾旋装置的安装使用以及与安全有关的一些注意事项。
In this paper,the approach to research the stall/post-tall/spin for modernaircraft,the aims of the stall/post──stall/spin flight test demonstration,test method and therequirements on the measurement are introduced briefly. The procedure of flight testdemonstration of the stall/post-stall/spin for today’s aircraft,the expectal requirements foraircrafts that employ AOA limiter , the installation and employment of the emergency anti──spin device and some safety problems are described in detail.
出处
《飞行力学》
CSCD
北大核心
1995年第3期9-17,共9页
Flight Dynamics
关键词
失速
过失速
尾旋
飞行试验
飞机
Stall/post-stall/spin Departure/spin sensitivity Flight test