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展了一种悬停
态下无铰旋翼桨叶气弹稳定性的分析方法。
叶片;子叶片;叶片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展了一种悬停态下无铰旋翼桨叶气弹稳定性的分析方法。
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