Research of the incipient fault detection method for an airfoil based on near flutter analysis
暂无分享,去创建一个
Zhen Yu | Lijun Liu | Chunhui Zhu | Nanjie Xie | Chunhui Zhu | Lijun Liu | Zhenlin Yu | Nanjie Xie
[1] Yuan-Cheng Fung,et al. An introduction to the theory of aeroelasticity , 1955 .
[2] Robert M. Bennett,et al. NACA 0012 benchmark model experimental flutter results with unsteady pressure distributions , 1992 .
[3] R Waszak Martin. Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression , 1996 .
[4] Eli Livne,et al. Future of Airplane Aeroelasticity , 2003 .
[5] Wan Xiao. DAMAGE DETECTION OF COMPOSITE WING BY USING MODAL STRAIN ENERGY , 2005 .
[6] Liu Xiao-xiong,et al. Method of dynamic flight envelop assessment for aircraft wing damages , 2013 .