Tests of three airplanes conducted to develop elevators that would provide stick forces in steady turns within limits required by Army and Navy specifications; it is concluded that requirements for stick forces in steady turns and damping of control-free longitudinal oscillation are not adequate to assure satisfactory elevator control in all cases.


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    Title :

    Investigation of additional requirements for satisfactory elevator control characteristics


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1946


    Size :

    9 pages


    Remarks:

    Supp sheets, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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