Theoretical analysis, considering unsteady effects, shows that response to collective pitch while in descending flight is largely dependent upon rapidity of control application; experimental tests confirm results. Translation from Technique et Science Aeronautiques n 3 May-June 1959 p 177-83.


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    Title :

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


    Additional title:

    NASA -- Tech Translation


    Contributors:


    Publication date :

    1961


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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

    Rebont, Jean / Valensi, Jacques / Soulez-Larivière, Jean | TIBKAT | 1961




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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