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A simulator study to determine pilot opinion of the trim changes with power for deflected slipstream STOL airplanesPowered trim changes affecting pilot during simulated landing for short take off and landing aircraft
Document ID
19660007261
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Drinkwater, F. J., III (NASA Ames Research Center Moffett Field, CA, United States)
Vomaske, R. F. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Biotechnology
Report/Patent Number
NASA-TN-D-3246
Report Number: NASA-TN-D-3246
Accession Number
66N16550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT SIMULATION
AIRCRAFT LANDING
PILOT PERFORMANCE
AIRCRAFT PERFORMANCE
STOL AIRCRAFT

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