摘要
为了解除直升机旋翼桨叶挥舞面载荷和摆振面载荷在测量中的耦合效应,提出了两种解耦方法:分析解耦法和物理解耦法。通过对两者的分析比较,确定两者的优缺点,为型号应用提供方法借鉴。
This paper introduced two methods for solving-couple of the flap and the lag plane in helicopter rotor blade load measurement.One was analyzing solving-couple,another was physical solving-couple.Advantage and disadvantage of the two methods were ascertained by analysis and comparing.It would be helpful to application for helicopter.
出处
《直升机技术》
2010年第4期8-10,共3页
Helicopter Technique
