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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Lomax, H. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    62 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch






    Sideslip angles and vertical-tail loads in rolling pull-out maneuvers.

    White, Maurice D / Lomax, Harvard / Turner, Howard L | NTRS | 1947


    Sideslip angles and vertical-tail loads in rolling pull-out maneuvers

    White, M.D. / Lomax, H. / Turner, H.L. | Engineering Index Backfile | 1947


    Sideslip angles and vertical-tail loads in rolling pull-out maneuvers

    White, Maurice D. / Lomax, Harvard / Turner, Howard L. | TIBKAT | 1946