NASA NTRS · 19720014363
Simulator model specification for the augmentor wing jet STOL research aircraft
Abstract
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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Rumsey, P. C., Spitzer, R. E.. 1971-12-01. Simulator model specification for the augmentor wing jet STOL research aircraft. https://ntrs.nasa.gov/citations/19720014363
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