System consists of freely rotating rotor in which opposite blades are rigidly connected and allowed to rotate freely about their span axis; equations for lift, lift-drag ratio, angle of attack, feathering angles, and rolling and pitching moments of gyroplane rotor in terms of its basic parameters; investigation discloses that aerodynamic principles of gyroplane are sound.


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    Title :

    Aerodynamic analysis of gyroplane rotating-wing system


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1934


    Remarks:

    6 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Wilford gyroplane

    Daland, E. | Engineering Index Backfile | 1938


    Hafner gyroplane

    Engineering Index Backfile | 1937


    GYROPLANE

    KRASNOBORODKO VLADIMIR VSEVOLODOVICH | European Patent Office | 2018

    Free access