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)


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    Title :

    A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence


    Contributors:

    Publication date :

    1973


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English