Comparison shown between computed loads and loads measured in flight on fighter airplane; dynamic effects investigated on large flying boat for both abrupt rudder deflection and sinusoidal rudder deflection; to take into account dynamic effects in design, specifications of yawing maneuverability or control movement are needed.


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    Titel :

    Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Boshar, J. (Autor:in) / Davis, P. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    12 pages


    Anmerkungen:

    Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch