A method for reducing the aerodynamic drag SYSTEM freewheeling rotor-wing rotary-wing aircraft at high speed FLIGHT

摘要

A method of reducing the drag system freewheeling rotor-wing rotorcraft at high flight speeds is to reduce profile drag freewheeling rotor due to redistribution of a lifting force to the wing having smaller core resistance, characterized in that the adjusted minimum chastototu rotation freewheeling rotor by reducing its overall pitch.