T尾结构振动的模态局部化判据研究

用峰值振幅比定义局部化度,用平尾刚度与垂尾刚度的比值定义耦合度.基于T尾结构的质量失调模型,从模态峰值振幅比、失调耦合比、常规摄动和近频摄动4个角度,提出4个不同的局部化判据来预测T尾结构模态局部化的发生.对一个T尾结构模型局部化振动的数值分析结果表明:(1)T尾结构系统一般具有弱耦合性,小量的失调就可以使T尾结构发生模态局部化;(2)T尾结构一旦发生模态局部化,不但使对称一弯模态和反对称一弯模态的振型发生较大改变,而且其模态频率也将改变,模态频率的改变在失调量的正负区间内具有唯一性;(3)算例验证了4个模态局部化判据的可行性和有效性,为T尾结构的模态局部化分析和设计提供了依据.

MODE LOCALIZATION PREDICTION CRITERION FOR T-TAIL STRUCTURE

Mode localization is often an unexpected dynamic phenomenon in weakly-coupled symmetric structure, and it arises from small imperfections(less than 5%) which perturb the symmetry.Such imperfections typically result from random manufacturing or assembly imprecision.Mode localization prediction is an important problem in T-Tail structure design because some drastic localized vibration phenomena occur during ground vibration test of T-Tail aircraft.Mode localization is dependent not only on mistuning,but also ...