In the following report, we will first draw some conclusions of purely theoretical interest, from the general equations of motion. At the end, we will consider the motion of an airplane, with the engine dead and with the assumption that the angle of attack remains constant. Thus we arrive at a simple result, which can be rendered practically utilizable for determining the trajectory of an airplane descending at a constant steering angle.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Differential equations in airplane mechanics


    Beteiligte:
    Carleman, M T (Autor:in)

    Erscheinungsdatum :

    01.03.1922


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Structural Mechanics of the Airplane

    A. A. Umanskii | NTIS | 1965


    Airplane engines and differential coupling

    Le Bidolec, A. | Engineering Index Backfile | 1923


    Analytical Approximation for the Mechanics of Airplane Spin

    W. F. Phillips / E. A. Anderson | AIAA | 2002