Study of transition following power failure while hovering; effects of hinging blades, of blade moment of inertia and of rapidity of pitch reduction after power failure investigated.


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    Title :

    Analysis of transition of helicopter from hovering to steady autorotative vertical descent


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Nikolsky, A.A. (author) / Seckel, E. (author)


    Publication date :

    1949


    Size :

    29 pages


    Remarks:

    Diagrs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :