A Laboratory Study of Subjective Annoyance Response to Sonic Booms and Aircraft Flyovers

A Laboratory Study of Subjective Annoyance Response to Sonic Booms and Aircraft Flyovers
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Publisher : Createspace Independent Publishing Platform
Total Pages : 38
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ISBN-10 : 172200441X
ISBN-13 : 9781722004415
Rating : 4/5 (1X Downloads)

Synopsis A Laboratory Study of Subjective Annoyance Response to Sonic Booms and Aircraft Flyovers by : National Aeronautics and Space Administration (NASA)

Three 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. Leatherwood, Jack D. and Sullivan, Brenda M. Langley Research Center RTOP 537-03-21-03...

NASA Technical Memorandum

NASA Technical Memorandum
Author :
Publisher :
Total Pages : 52
Release :
ISBN-10 : MINN:31951000845538Z
ISBN-13 :
Rating : 4/5 (8Z Downloads)

Synopsis NASA Technical Memorandum by :

Sonic-boom Research

Sonic-boom Research
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Publisher :
Total Pages : 52
Release :
ISBN-10 : STANFORD:36105024736196
ISBN-13 :
Rating : 4/5 (96 Downloads)

Synopsis Sonic-boom Research by : Harvey H. Hubbard

Aeronautical Engineering

Aeronautical Engineering
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Publisher :
Total Pages : 538
Release :
ISBN-10 : UOM:39015023295143
ISBN-13 :
Rating : 4/5 (43 Downloads)

Synopsis Aeronautical Engineering by :

Congressional Record

Congressional Record
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Publisher :
Total Pages : 1228
Release :
ISBN-10 : HARVARD:32044116492703
ISBN-13 :
Rating : 4/5 (03 Downloads)

Synopsis Congressional Record by : United States. Congress

The Congressional Record is the official record of the proceedings and debates of the United States Congress. It is published daily when Congress is in session. The Congressional Record began publication in 1873. Debates for sessions prior to 1873 are recorded in The Debates and Proceedings in the Congress of the United States (1789-1824), the Register of Debates in Congress (1824-1837), and the Congressional Globe (1833-1873)