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Effects of helicopter noise and vibration on pilot performance (as measured in a fixed-base flight simulator)The effects of noise and vibration on pilot performance are described. Pilot subjects were required to fly VTOL commercial IFR schedules using the computer simulation facilities. The routes flown simulated closely metropolitan routes flown currently by a helicopter airline. The duration of simulator flights ranged from 3 to 8 hours. Subjects were exposed to noise sound pressure levels ranging from 74dB (ambient) to 100dB and 17 Hz vibration stimuli ranging from .1 g to .3 g measured at the floor directly beneath the pilot's seat. Despite subject reports of extreme fatigue in these long flights, performance did not degrade. A curve of performance shows a slow improvement for the first three hours of exposure and a slight loss in performance during the remainder of the flight. As environmental stress conditions (noise, vibration, and time in the simulator) increased, subject performance improved. Within the limits of this study, the higher the stress the better the performance.
Document ID
19740002865
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stave, A. M.
(United Aircraft Corp. Stratford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
December 7, 1973
Subject Category
Biotechnology
Report/Patent Number
NASA-CR-132347
Report Number: NASA-CR-132347
Accession Number
74N10978
Funding Number(s)
CONTRACT_GRANT: NAS1-11222
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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