The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular attention is given to the following: control system; conversion system; and propulsion system. Flight test results are also reported.


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    Title :

    The XV-15 tilt rotor research aircraft


    Contributors:

    Publication date :

    1980-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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