In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
气动弹性领域中,人们过程中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.
采用伽金加权余数有限元素法发展了一种悬下无铰旋翼桨叶气弹稳定性的分析方法。
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This phenomenon is called aeroelastic flutter.
现称弹性颤振。
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