Some key issues of aircraft T-Tail flutter calculation

被引：0
|
作者：
Yang, Fei [1 ]
Yang, Zhi-Chun [2 ]
机构：
[1] Strength Department, Shanghai Aircraft Design and Research Institute, Shanghai 200232, China
[2] School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2011年 / 30卷 / 05期
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摘要：
13
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页码：136 / 139
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