Study of dynamic stability of helicopter with hinged rotor blades under hovering conditions; possibility of controlled stability is proved by successful flights of various helicopters, particularly of universally known Focke. From Ingenieur-Archiv Dec 1938.


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    Title :

    Dynamic stability of helicopter with hinged rotor blades


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo



    Publication date :

    1939


    Size :

    17 pages


    Remarks:

    1 Supp plate


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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