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A laboratory study of subjective annoyance response to sonic booms and aircraft flyoversThree experiments were conducted to determine subjective equivalence of aircraft subsonic flyover noise and sonic booms. Two of the experiments were conducted in a loudspeaker-driven sonic boom simulator, and the third in a large room containing conventional loudspeakers. The sound generation system of the boom simulator had a frequency response extending to very low frequencies (about 1 Hz) whereas the large room loudspeakers were limited to about 20 Hz. Subjective equivalence between booms and flyovers was quantified in terms of the difference between the noise level of a boom and that of a flyover when the two were judged equally annoying. Noise levels were quantified in terms of the following noise descriptors: Perceived Level (PL), Perceived Noise Level (PNL), C-weighted sound exposure level (SELC), and A-weighted sound exposure level (SELA). Results from the present study were compared, where possible, to similar results obtained in other studies. Results showed that noise level differences depended upon the descriptor used, specific boom and aircraft noise events being compared and, except for the PNL descriptor, varied between the simulator and large room. Comparison of noise level differences obtained in the present study with those of other studies indicated good agreement across studies only for the PNL and SELA descriptors. Comparison of the present results with assessments of community response to high-energy impulsive sounds made by Working Group 84 of the National Research Council's Committee on Hearing, Bioacoustics, and Biomechanics (CHABA) showed good agreement when boom/flyover noise level differences were based on SELA. However, noise level differences obtained by CHABA using SELA for aircraft flyovers and SELC for booms were not in agreement with results obtained in the present study.
Document ID
19940029104
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Leatherwood, Jack D.
(NASA Langley Research Center Hampton, VA, United States)
Sullivan, Brenda M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Subject Category
Acoustics
Report/Patent Number
NASA-TM-109113
NAS 1.15:109113
Report Number: NASA-TM-109113
Report Number: NAS 1.15:109113
Accession Number
94N33610
Funding Number(s)
PROJECT: RTOP 537-03-21-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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