Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The influence of unsteady aoerodynamic effects on the coupled free vibrations of rotor flapping body pitch and roll in Hover


    Contributors:


    Publication date :

    1996



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik
    Local classification TIB:    770/7040




    Modified Unsteady Vortex-Lattice Method to Study Flapping Wings in Hover Flight

    Roccia, Bruno A. / Preidikman, Sergio / Massa, Julio C. et al. | AIAA | 2013


    Hover-Capable Flapping-Wing Aircraft

    BENEDICT MOBLE / COLEMAN DAVID A | European Patent Office | 2020

    Free access

    HOVER-CAPABLE FLAPPING-WING AIRCRAFT

    BENEDICT MOBLE / COLEMAN DAVID | European Patent Office | 2019

    Free access