相关期刊:《Transactions of Nanjing University of Aeronautics and Astronautics》《Journal of Computer and Communications》《Chinese Journal of Aeronautics》《Science China(Technological Sciences)》更多>>
The aerodynamics, dynamic responses and aeroelasticity of tiltrotor aircraft in the tilting of rotor i.e. in conversion flight are extraordinarily complicated. The traditional quasi-steady assumption model can not ref...