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The Influence of Added Narrow Band Noises and Tones on the Subjective Response to Shaped “White” Noise

Published online by Cambridge University Press:  04 July 2016

T. J. Hargest  and
R. A. Pinker
T. J. Hargest
Affiliation:
National Gas Turbine Establishment
R. A. Pinker
Affiliation:
National Gas Turbine Establishment
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Extract

Experiments on the influence of added narrow band sounds on the subjective assessment of noise were conducted at the NGTE 1966 Open Week and at the 1966 SBAC Show, with over two thousand people participating. The results clarify the apparently conflicting observations of earlier workers and show definitely that the presence of a narrow band content can significantly influence the degree of disturbance caused by noise of the type generated by aircraft near an airport.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 71 , Issue 678 , June 1967 , pp. 428 - 430
Copyright
Copyright © Royal Aeronautical Society 1967

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References

1.Copeland, W. C. T., et al.A Controlled Experiment on the Subjective Effects of Jet Engine Noise. JRAeSoc, Vol. 64, p 33, January 1960.Google Scholar
2.Kryter, K. D. and Pearsons, K. S.Judged Noisiness of a Band of Random Noise Containing an Audible Pure Tone. JASA, Vol. 38, p 106, July 1965.CrossRefGoogle ScholarPubMed
3.Little, J. W.Human Response to Jet Engine Noises. Noise Control 7, No. 3, p 11–13, 1961.CrossRefGoogle Scholar
4.Bowsher, J. M. Private Communication from the National Physical Laboratory, England.Google Scholar
5.Anon. Proposed FAA Maximum Allowable Noise Levels to be Required for Certification of Future Aircraft (Table I). Federal Aviation Agency, 26th August 1966.Google Scholar
6.Rayleigh, Lord. Theory of Sound. Vol. 1, p 8, Second Edition, Macmillan, 1944.Google Scholar
7.Rüedi, L. and Furrer, W.Physics and Physiology of Acoustic Trauma. JASA, Vol. 18, p 409, October 1946.CrossRefGoogle Scholar