Nonlinear flutter study of high-aspect-ratio cantilever plate in subsonic flow

来源 :The 5th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：lycwmy01011

【摘要】

：

Flutter is self-excited oscillation of a flight vehicle when exposed to airflow.Analysis of nonlinear flutter of the cantilever plate requires an explicit expression of the aerodynamic force of the ca

【作者】

：

Minghui Yao Li Ma Kai Lou Wei Zhang

【机构】

：

College of Mechanical Engineering, Beijing University of Technology, Beijing, China

【出处】

：

The 5th International Conference on Dynamics, Vibration and

【发表日期】

：

2018年11期

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Nonlinear flutter study of high-aspect-ratio cantilever plate in subsonic flow

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