flutter-clear aircraft 不易颤振的飞机
After reviewing the application of system identification to aircraft flutter research, three methods of system identification are presented in this paper.
本文在简要综述了系统识别技术在飞机颤振研究中的应用后，介绍了三种系统识别方法。
Design of flutter model from aircraft metal structure to composite structure can be achieved by equation of stiffness, yet it may cost much time for general design method.
金属飞机结构到复合材料结构的颤振模型设计，要求采用刚度等代法来完成，然而一般的设计方法通常需要消耗大量时间。
Combining dynamic design of wing flutter model for a giant transport aircraft, a numerical example of engineering application is presented.
结合某大型飞机机翼颤振吹风模型的动力设计，本文给出了工程应用的具体数值例子。
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