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Guijuan Wang, Huarong Chen, Rui Zhou, Yadong Wu, Wei Gao, Jing Liao and Fupan Wang
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Renguo Yang, Yadong Gao, Huaming Wang and Xianping Ni
In order to further reduce the vibration level of helicopters, the active vibration control technology of helicopters has been extensively studied. Among them, individual blade control (IBC) independently applies high-order harmonics to each blade with a...
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Yadong Gao, Xinyu Yu, Likun Chen and Dawei Huang
Accurately identifying the peak value of impact load acting on the helicopter structure during weapon launch is of great significance to the design and finalization of weapon pylons. Firstly, a method of standardized preprocessing load signal is proposed...
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Yadong Gao and Yang Xu
Variable diameter rotor can improve the flight performance of the aircraft both in hovering and forward flying and a duct can improve the rotor performance further both in force and efficiency. In previous studies, those two parts are always studied in t...
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Zhengying Cui, Shigeru Morita, Bingzhong Fu, Yuan Huang, Ping Sun, Yadong Gao, Yuan Xu, Chunfeng Dong, Ping Lu, Quanming Wang, Xuantong Ding, Qingwei Yang, and Xuru Duan
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