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Annoyance due to simulated blade-slap noiseThe effects of several characteristics of blade slap noise on annoyance response were studied. These characteristics or parameters were the sound pressure level of the continuous noise used to simulate helicopter broadband noise, the ratio of impulse peak to broadband noise or crest factor, the number of pressure excursions comprising an impulse event, the rise and fall time of the individual impulses, and the repetition frequency of the impulses. Analyses were conducted to determine the correlation between subjective response and various physical measures for the range of parameters studied. A small but significant improvement in the predictive ability of PNL was provided by an A-weighted crest factor correlation. No significant improvement in predictive ability was provided by a rate correction.
Document ID
19790002676
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Powell, C. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1978
Publication Information
Publication: Helicopter Acoustics, Pt. 2
Subject Category
Acoustics
Accession Number
79N10847
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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