Airworthiness compliance validating technique for wind tunnel test of a civil aircraft low speed flutter model

被引：0
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作者：
Liang, Ji [1 ]
Yang, Fei [1 ]
Yang, Zhi-Chun [1 ]
机构：
[1] Stress Department, Shanghai Aircraft Design and Research Institute of COMAC, Shanghai 200232, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2013年 / 32卷 / 12期
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