It has been shown by the calculations of a preceding note that the effect on the lift of a rotor due to an increase in the effective collective pitch, while in the course of steady descending vertical flight near the autorotative regime, depends essentially upon the speed of the pitch change. Experiment confirms the result.


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    Title :

    Wind-Tunnel Study of the Response in Lift of a Rotor to an Increase in Collective Pitch in the Case of Vertical Flight Near the Autorotative Regime


    Contributors:

    Publication date :

    1960


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English