研究领域

Aeroelasticity of rotorcraft, Rotor Multibody System

论文与著作

[1]     Yu Zhihao, Yang Weidong. An improved method and itsvalidation for large deflection analysis of initially twisted composite rotorblades. Chinese Journal of Applied Mechanics, 2014, 31(5): 752-757.

[2]     Yu Zhihao, Yang Weidong, Zhang Chenglin, et al.Aeroelasticity analysis of rotor multibody system based on broyden method. ActaAeronautica et Astronautica Sinica, 2012, 33(12): 2171-2182.

[3]     Yu Zhihao, Yang Weidong, Deng Jinhui. Model of rotoraeroelastic stability using dynamics of flexible multibody system. Journal ofAerospace Power, 2012, 27(5), 1122-1130

[4]     Li Ruirui, Yu Zhihao,Yang Weidong, et al. A time-domain computational method for dynamic propertiesand analysis of helicopter rotor elastomeric damper. Acta Aeronautica etAstronautica Sinica, 2015, 36(6): 1905-1914.

[5]     Liu Shiming, Yang Weidong, YUZhihao, et al. Vibratory loads prediction of rotor with trailing edgeflaps. Journal of Aerospace Power, 2016, 31(6), 1496-1503.

[6]     Li Ruirui, Yang Weidong, YuZhihao. Multiple parameters dynamic modeling and analysis of helicopterrotor multi-layer elastomeric damper. Journal of Aerospace Power,2014,29(4):844-851.

[7]     Wu Jie, Yang Weidong, Yu Zhihao.Comparison among rotor blade structural load calculation methods. Journal ofVibration and Shock, 2014, 33(7): 210-214.