A six degree of freedom flight simulation model was developed for digital computers to investigate the response of aircraft to a pair of trailing vortices. The model was used to simulate the flight of a light, two-seat training aircraft and a twin-engined commercial transport into the vortices shed by medium weight and heavy weight aircraft. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence


    Beteiligte:
    R. C. H. Parkinson (Autor:in) / D. W. Kelly (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    52 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch