An iterativecomputation 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。
2
The deformation quantity corresponding to the rolling press getting good shape can be got by straggling press amount and iterativecomputation.
该方法通过离散压下量，迭代计算得出板型良好的轧制压力所对应的变形量，对实际生产有指导作用。
3
This paper introduces the principle and implementation of iterativecomputation of stacking velocity and residual statics and discusses its application effects.