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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    Titel :

    Aerodynamic analysis of gyroplane rotating-wing system


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Wheatley, J.B. (Autor:in)


    Erscheinungsdatum :

    1934


    Anmerkungen:

    6 Supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Wilford gyroplane

    Daland, E. | Engineering Index Backfile | 1938


    Hafner gyroplane

    Engineering Index Backfile | 1937


    Gyroplane Technology

    Groen, D. / AIAA / ICAS | British Library Conference Proceedings | 2003