The response to vertical turbulence in cruise of the HTR XV-15 design is studied using simulation techniques. This design is a modified version of the XV-15 with a hingeless fiberglass soft-in-plane rotor system. The parameters of a gust alleviation system are determined and the performance of the system is evaluated over a range of cruise velocities and altitudes.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Simulation Study of Gust Alleviation in a Tilt Rotor Aircraft, Volume 1


    Contributors:

    Publication date :

    1977


    Size :

    174 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English