It is shown by calculation of preceding note that effect on lift of rotor due to increase in effective collective pitch, while in course of steady descending vertical flight near autorotative regime, depends essentially upon speed of pitch change; experiment confirms result. Translated from Acad des Sciences -- Comptes Rendus Sept 8 1958.


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    Title :

    Wind-tunnel study of response in lift of rotor to increase in collective pitch in case of vertical flight near autorotative regime


    Additional title:

    NASA -- Tech Translation


    Contributors:


    Publication date :

    1960


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :