An iterative computation method for nonlinear forced vibration equation on helicopter blade aerodynamic load is given.

介绍用迭代方法求解直升机桨叶气动载荷中的非线性强迫振动方程。

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An iterative computation method for nonlinear forced vibration equation on helicopter blade aerodynamic load is given.

介绍用迭代方法求解直升机桨叶气动载荷中的非线性强迫振动方程。

youdao