Maximum sideslip angles and vertical tail loads computed and compared with those obtained from two other dynamic maneuvers, rudder kick and rolling pull-out; method given for computing maximum sideslip angles when forces and moments are non-linear functions of sideslip.


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    Title :

    Sideslip angles and vertical-tail loads developed by periodic control deflections


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Lomax, H. (author)


    Publication date :

    1948


    Size :

    62 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English