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Acoustic design criteria and validationThe tools currently available for acoustic design risk reduction and problem solving are limited in accuracy and do not encompass all design parameters. Assuming available technology, designing helicopters to confidently meet noise limits as were proposed by the FAA and were now adopted by ICAO will result in significant design compromises.
Document ID
19840021594
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Arcidiacono, P.
(Sikorsky Aircraft Stratford, CT, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1982
Publication Information
Publication: NASA. Langley Research Center Rotorcraft Noise
Subject Category
Acoustics
Accession Number
84N29663
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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