A theoretical investigation has been made to determine the effect of nonlinear stability derivatives on the lateral stability of an airplane. Motions were calculated on the assumption that the directional-stability and the damping-in-yawing derivatives are functions of the angle of sideslip. The application of the Laplace transform to the calculation of an airplane motion when certain types of nonlinear derivatives are present is described in detail. The types of nonlinearities assumed correspond to the condition in which the values of the directional-stability and damping-in-yawing derivatives are zero for small angle of sideslip.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane


    Beteiligte:

    Erscheinungsdatum :

    01.01.1951


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch