System claimed to be aerodynamically sound in principle; hovering flight, vertical ascent, and reasonable forward speed obtained without excessive expenditure of power; cyclogiro rotor will autorotate in gliding descent.


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    Title :

    Simplified aerodynamic analysis of cyclogiro rotating-wing system


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1933


    Size :

    13 pages


    Remarks:

    15 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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    Free access