Dynamic yawing effects on vertical tail loads are considered by a theory of flat yawing maneuvers. A comparison is shown between computed loads and the loads measured in flight in a fighter airplane. The dynamic effects were investigated on a large flying boat for both an abrupt rudder deflection and a sinusoidal rudder deflection. Only a moderate amount of control deflection was found to be necessary to attain the ultimate design load on the tail. In order 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 the vertical tail by the theory of flat yawing maneuvers


    Beteiligte:
    Boshar, John (Autor:in) / Davis, Philip (Autor:in)

    Erscheinungsdatum :

    1946-06-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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

    Boshar, J. / Davis, P. | Engineering Index Backfile | 1946


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

    Boshar, J. / Davis, P. | Engineering Index Backfile | 1946



    Yawing Maneuvers

    Lomax, Ted L. | AIAA | 1996


    Analysis of vertical-tail loads in rolling pull-out maneuvers

    Gilruth, R.R. | Engineering Index Backfile | 1944