The configuration and simulation studies of a C-8A (De Havilland Buffalo) aircraft are described. The modifications to STOL configuration consisted of augmentor-wing jet flaps, blown and drooped ailerons, and leading edge slats. The total simulator model includes a number of component parts for producing realistic visual, aural, tactile, vestibular, and kinesthetic cues for the pilot to assess the predicted behavior of the real airplane.


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    Titel :

    Simulator model specification for the augmentor wing jet STOL research aircraft


    Beteiligte:
    Rumsey, P. C. (Autor:in) / Spitzer, R. E. (Autor:in)

    Erscheinungsdatum :

    01.12.1971


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :