摘要
本文以高速歼击机为例描述了飞机气动导数相关性飞行试验研究的方法,并对试飞获得的结果进行了分析.
In this paper, a method of flight test research on corelation of airplane aerodynamic derivatives is described and the results of flight test are analysed. A high speed fighter was used in the flight test research.
出处
《飞行力学》
CSCD
北大核心
1990年第3期67-76,共10页
Flight Dynamics
