The helicopter blades aeroelastic stability optimization
直升机气弹稳定性优化，王红州，刘勇，推导旋翼气弹运动方程，给出稳定性条件。以安装角、预锥角及单元质量为设计变量，以稳定性系数和频率分布为约束，进行桨叶最小质
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