Elementary calculation inspired by classic treatment for steady state permits determination of induced velocity and overall lift of rotor as function of collective pitch for all values of advance per turn; nature of lift response is shown to be function of rate of pitch change. Translated from Acad des Sciences -- Comptes Rendus, Sept 1 1958.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Response of rotor lift to increase in collective pitch in case of descending flight, regime of rotor being near autorotation


    Additional title:

    NASA -- Tech Translation


    Contributors:


    Publication date :

    1960


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Autogyro rotor blade for generating lift by autorotation

    FRAUNDORFER CHRISTOPH / ZOEBISCH ANDRE | European Patent Office | 2022

    Free access

    Autogyro rotor blade for generating lift by autorotation

    FRAUNDORFER CHRISTOPH / ZOEBISCH ANDRÉ | European Patent Office | 2021

    Free access

    AUTOGYRO ROTOR BLADE FOR GENERATING LIFT BY AUTOROTATION

    FRAUNDORFER CHRISTOPH / ZOBISCH ANDRE | European Patent Office | 2017

    Free access