Hostname: page-component-848d4c4894-ttngx Total loading time: 0 Render date: 2024-06-09T09:37:58.270Z Has data issue: false hasContentIssue false

A Subjective Experiment with Helicopter Noises

Published online by Cambridge University Press:  04 July 2016

D. W. Robinson
Affiliation:
Applied Physics Division, National Physical Laboratory
J. M. Bowsher
Affiliation:
Applied Physics Division, National Physical Laboratory

Extract

Following upon an experiment on the subjective effects of jet engine noise we have recently undertaken a similar experiment, this time on the subjective aspects of helicopter noise. The purpose of the earlier experiment was to determine the reliability of various methods of rating based on spectrum analysis, so far as comparisons between jet- and piston-engined aircraft are concerned. The main objective of the present experiment was to find if these methods are applicable to the pulsating types of noise characteristic of helicopters.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1961

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Copeland, W. C, Davidson, I. M., Hargest, T. J. and Robinson, D. W. (1960). Journal of the Royal Aeronautical Society, Vol. 64, p. 33, 1960.Google Scholar
2.Stevens, S. S. (1956). J. acoust. Soc. Amer., Vol. 28, p. 807, 1956.Google Scholar
3.Zwicker, K. E. (1959). Frequenz, Vol 13, p. 234, 1959.Google Scholar
4.Kryter, K. D. (1959). J. Acoust. Soc. Amer., Vol. 31, p. 1415, 1959.Google Scholar
5.Recommendations for Sound Level Meters. International Electrotechnical Commission, Publication 123, Geneva, 1961Google Scholar
6.Crosse, G. W., Davidson, I. M., Hargest, T. J. and Porter, M. J. (1960). Journal of the Royal Aeronautical Society, Vol. 64 p. 629, 1960.Google Scholar