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.


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    Title :

    Pitch-decoupled VTOL/FW aircraft: First flights


    Contributors:


    Publication date :

    2017-10-01


    Size :

    1335030 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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