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
素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性
分析方法。
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素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性分析方法。
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