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
2017-10-01
1335030 byte
Conference paper
Electronic Resource
English
Helicopter, first of VTOL aircraft
Engineering Index Backfile | 1961
|SAE Technical Papers | 1961
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