A novel Pitch-Decoupled Tilt Rotor aircraft is introduced that dramatically deviates from all tilt rotor systems developed to date. This new design does not require a complex transition algorithm and is continuously stable and operable in all its rotor pitch configurations.
Pitch-decoupled VTOL/FW aircraft: First flights
01.10.2017
1335030 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch