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Simulator model specification for the augmentor wing jet STOL research aircraftThe 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.
Document ID
19720014363
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rumsey, P. C. (Boeing Co. Renton, WA, United States)
Spitzer, R. E. (Boeing Co. Renton, WA, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-CR-114434
D6-26065TN
Report Number: NASA-CR-114434
Report Number: D6-26065TN
Accession Number
72N22013
Funding Number(s)
CONTRACT_GRANT: NAS2-6025
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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