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Engineering simulation development and evaluation of the two-segment noise abatement approach conducted in the B-727-222 flight simulatorProfile modification as a means of reducing ground level noise from jet aircraft in the landing approach is evaluated. A flight simulator was modified to incorporate the cockpit hardware which would be in the prototype airplane installation. The two-segment system operational and aircraft interface logic was accurately emulated in software. Programs were developed to permit data to be recorded in real time on the line printer, a 14-channel oscillograph, and an x-y plotter. The two-segment profile and procedures which were developed are described with emphasis on operational concepts and constraints. The two-segment system operational logic and the flight simulator capabilities are described. The findings influenced the ultimate system design and aircraft interface.
Document ID
19750010123
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nylen, W. E.
(United Air Lines, Inc. Chicago, IL, United States)
Date Acquired
September 3, 2013
Publication Date
January 30, 1974
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-CR-137594
Report Number: NASA-CR-137594
Accession Number
75N18195
Funding Number(s)
CONTRACT_GRANT: NAS2-7208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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