A flutter analysis based on root locus method is programmed. It can be applied to a wing equipped with an active fluttersuppressionsystem.
本文编制了可用于分析带有颤振主动抑制系统的机翼的根轨迹法程序。
2
The test results show that a change in two parameters-the gain and the phase Angle of the feedback control-will have an effect on the stability of the active fluttersuppressionsystem.