In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领
，
们在设计过程最为关心的是颤振现象。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领，们在设计过程最为关心的是颤振现象。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发
了一种悬停状态下无铰旋翼桨叶气弹稳定性的
析方法。
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