Hostname: page-component-cd9895bd7-dk4vv Total loading time: 0 Render date: 2024-12-27T14:26:57.508Z Has data issue: false hasContentIssue false

A Comparative Study of the Noise from Turbo-Jet and Reciprocating Aircraft Engines in Flight

Published online by Cambridge University Press:  28 July 2016

Summary

Sources of noise in aircraft are discussed briefly with particular reference to the introduction of the turbo-jet engine.

An account is given of a particular investigation made in a Lancastrian aircraft fitted with both turbo-jet and reciprocating engines. The equipment by which the noise spectrum was analysed over, an extended frequency band is described.

The results are examined and the effects of the two types of engine on the noise spectrum are compared, under different representative conditions, in the forward and rear sections of the fuselage.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1950

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. Air Service Training Ltd. Technical Report, ST/Tech./EX/9, p. 6, November 1947.Google Scholar
2. Beranek, L. L. et al. O.S.R.D. Report No. 1543, 1944.Google Scholar
3. Chavasse, P. and Lehmann, R. Report 12/154, 3eme Congress National de l'Aviation Française, April 1947.Google Scholar
4. Dickson, E. D. D. Report R.A.F., A.R.C. 18, March 1948.Google Scholar
5. Fleming, N. The Silencing of Aircraft, Journal R.Ae.S., 50, September 1946.Google Scholar
6. Francke, E. Technical Report 4, Helmholz Institute, Berlin, April 1945.Google Scholar
7. Gardiner, G. C. I. and Mullin, J. The Design of Propellers, Journal R.Ae.S., August 1949.Google Scholar
8. Makinson, W. and Badcoe, S. R. R.A.E. Technical Note No. Rad. 431, June 1948.Google Scholar
9. Rudmose, H. Wayne, and Beranek, L. L. Noise Reduction in Aircraft, Journal of the Aeronautical Sciences, February 1947.Google Scholar