aeroelastic

In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.

在动性领域中，人们在设计过程中最为关心的是颤振现。

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.

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稳定性的分析方法。