摘要
介绍了动力三角翼飞行器的总体布局特征及有关气动力设计技术,着重论述了该类飞行器实现飞行稳定性和操纵性的原理,并以某型动力三角翼飞行器的气动力数据为例进行了说明,最后总结出了该类飞行器可行的气动力设计和试验方法。
This paper introduces the general layout characteristics and corresponding aerodynamic design technology for the trike, and put much effort to instruct the trike＇s stability and control principles with the help of a set of aerodynamic data for a trike. Finally, the applicable aerodynamic design and test methods for the trike are pointed out in this paper.
出处
《飞行力学》
CSCD
北大核心
2006年第3期9-12,共4页
Flight Dynamics
