摘要
讨论了对非比例阻尼振动系统作小修改时,其复频率和复振型的摄动分析方法。当振动系统的质量矩阵、刚度矩阵和阻尼矩阵有较小修改时,不重复求解大型复广义特征问题,在已知初始系统复模态参数的基础上进行复模态坐标变换,用矩阵摄动法给出修改系统的频率、阻尼比和复振型。算例表明,将这种方法用于非比例阻尼振动系统的动力修改,计算简单,费用经济,精度较高,因此是一种行之有效的分析方法。
A perturbation method for analyzing the complex frequencies and modes of non-pro-portional damped vibration systems is presented.When the mass,stiffness and damping matrices of the original system vary a little,carrying out the complex modal coordinate transformation based on the original known complex modes and using the matrix perturbation method,the fre-quencies,damping ratios and complex modes of the updated system can be obtained without re-solving a new large generalized complex eigenvalue problem.The numerical example shows that the present method is simple,economic and highly accurate.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第12期1486-1489,共4页
Acta Aeronautica et Astronautica Sinica
关键词
结构动力学
振动分析
摄动方法
飞机
structural dynamics,vibration analysis method,vibration characteristics,perturbation method