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Sound Quality Metric Indicators of Rotorcraft Noise Annoyance Using Multilevel Regression AnalysisAlthough every helicopter in operation has to go through a noise certification process, annoyance due to helicopters still persists within various communities. This implies that certification metrics do not capture the full range of human response and that predicted reactions could be supplemented with other information, which could be acoustic or non-acoustic in nature. The rotorcraft sound quality metric (RoQM) psychoacoustic experiment was designed to determine the relative importance of sound quality metrics (SQMs), such as sharpness, tonality, loudness, fluctuation strength and impulsiveness, on human annoyance to rotorcraft sounds. Starting from a baseline helicopter recording, SQMs were varied synthetically and presented to subjects who responded with an annoyance rating. The RoQM test took place in 2017 at the NASA Langley Research Center in the Exterior Effects Room. A total of 105 sounds were played to 40 subjects. The relationship between helicopter noise sound quality and annoyance is modeled using multilevel regression in this work, which takes into account the variability of responses across subjects. Previous analyses did not consider such a grouping of the data.
Document ID
20200003210
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Matthew Boucher
(Langley Research Center Hampton, Virginia, United States)
Siddhartha Krishnamurthy
(Langley Research Center Hampton, Virginia, United States)
Andrew Christian
(Langley Research Center Hampton, Virginia, United States)
Stephen A Rizzi
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 7, 2020
Publication Date
April 23, 2019
Publication Information
Publication: Journal of the Acoustical Society of America
Publisher: Acoustical Society of America
Volume: 145
Issue: 3
Issue Publication Date: March 1, 2019
ISSN: 0001-4966
Subject Category
Acoustics
Report/Patent Number
NF1676L-35613
Funding Number(s)
WBS: 664817.02.07.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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