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. (Author)


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    Title :

    Simulator Model Specification for the Augmentor Wing Jet STOL Research Aircraft


    Contributors:

    Publication date :

    1971


    Size :

    105 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English