The dynamics of a highly maneuverable subsonic aircraft during multiple roll around the length axis were investigated with a 6 deg of freedom computer program. The nonlinear dependencies on the aerodynamic forces and moments are taken into account. The effect of the dynamic derivation of lateral motion on the overall motion is shown. The relationship between the position of the overall rotation vector and the velocity vector is represented.


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    Titel :

    Investigation of Flight Dynamics During Roll Untersuchung der Flugdynamik Beim Rollen


    Beteiligte:
    H. D. Finck (Autor:in) / G. Sachs (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch