Real-time Flutter Boundary Prediction Using Peak-Hold Method

被引:0
|
作者
Ma, Yingwen [1 ]
Zhou, Li [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Structures, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
flutter boundary prediction; flutter test; extrapolation; critical mode;
D O I
10.1117/12.2301241
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This article proposes a new method of predicting flutter boundary online. In flutter test which is under continuous wind excitation, the primary objective is to get vibration response of critical position and determine the critical mode for flutter prediction. The frequency spectrum graphs are drawn to get the peaks round the modal frequency. As the wind-tunnel test goes on, more signal data are obtained to get the relation curve between peak-reciprocal and airstream speed. Then the signal points are drawn to get the fitting curve and the flutter boundary is predicted by extrapolation. The flutter point predicted is updating until the threshold between real-time airstream speed and extrapolated speed meets the requirements.
引用
收藏
页数:8
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