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    Title :

    Response of a helicopter rotor to an increase in collective pitch for the case of vertical flight


    Additional title:

    Réponse d'un rotor d'hélicoptère a une augmentation du pas général dans le cas du vol vertical <engl.>


    Contributors:

    Publication date :

    1961


    Size :

    20 S., [2] Bl


    Remarks:

    Ill., graph. Darst
    Übers. aus: Technique et science aéronautiques ; 1959,3
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Response of helicopter rotor to increase in collective pitch for case of vertical flight

    Rebont, J. / Valensi, J. / Soulez-Lariviere, J. | Engineering Index Backfile | 1961



    ASSISTED COLLECTIVE PITCH CONTROL SYSTEM FOR A HELICOPTER ROTOR

    LAMANNA ROBERTO | European Patent Office | 2023

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

    Rebont, J. / Soulez-Lariviere, J. / Valensi, J. | Engineering Index Backfile | 1960