A nomogram is developed which renders it possible by drawing a few lines, to determine: the location of the center of gravity for zero wing and tail moments; the longitudinal dihedral angle; the tail coefficient F(sub h) iota/F(sub t). Moreover there is no difficulty in determining the magnitude of the restoring moment or of the unstable moment.


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    Titel :

    The balance of moments and the static longitudinal stability of airplanes


    Beteiligte:
    Muller, Horst (Autor:in)

    Erscheinungsdatum :

    01.12.1929


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Equalization of moments and static longitudinal stability of airplanes

    Mueller, H. | Engineering Index Backfile | 1929


    Static longitudinal stability of "Ente" airplanes

    Kiel, Heinrich Georg | NTRS | 1931


    Static longitudinal stability of "Ente" airplanes

    Kiel, Heinrich Georg | TIBKAT | 1931


    Static longitudinal stability of "Ente" airplanes

    Kiel, H.G. | Engineering Index Backfile | 1930