semi-active flutter suppression 半主动抑制
active flutter suppression system 颤振主动抑制系统
flutter active suppression 颤振主动抑制
At the end of this paper are some problems which must be solved for the realization of active flutter suppression.
最后，提出了为实现主动颤振抑制必须解决的一些问题。
A flutter analysis based on root locus method is programmed. It can be applied to a wing equipped with an active flutter suppression system.
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。
The phenomena "limit cycle" occurred in wind tunnel test for active flutter suppression of a wing model are numerically explained using Harmonic Balance Method.
本文采用谐波平衡法，定量地解释了机翼颤振主动抑制风洞试验中出现的极限环现象。
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