Hostname: page-component-848d4c4894-mwx4w Total loading time: 0 Render date: 2024-06-20T00:24:15.632Z Has data issue: false hasContentIssue false

Recent developments in noise research at the National Gas Turbine Establishment

Published online by Cambridge University Press:  04 July 2016

F. W. Armstrong*
Affiliation:
Acoustic Aerodynamics Department, National Gas Turbine Establishment

Extract

The noise nuisance caused to communities around airports is one of the greatest problems besetting present-day civil aviation. Considerable effort is being expended to meet the challenge of lessening the nuisance without impairing the continued development of air transport. Governments, operators, manufacturers and research institutions are all playing a part. In addition to local regulations designed to control noise near specific airports, legislation based on international agreements has for some years required new types of subsonic jet airliner to be certificated as meeting given noise levels. Currently, the successful development of “hushkits” is enabling many older types to be brought within these levels. At the same time, it appears likely that still more stringent limits will be set for new types as the future unfolds.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1975 

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. Lloyd, P. Some aspects of engine noise. Journal of Royal Aeronautical Society, Vol 63, September 1959.Google Scholar
2. Kilpatrick, D. A. and Reid, D. T. Transonic compressor noise. The effect of inlet guide vane/rotor spacing. ARC R&M No 3412, 1964.Google Scholar
3. Philpot, M. G. The buzz saw noise generated by a high duty transonic compressor. ASME Paper 70-GT-54, 1970.Google Scholar
4. Philpot, M. G. The attenuation of forward arc fan tone noise due to rotor blade blockage effects. NGTE Report No R332, 1974.Google Scholar
5. Copeland, W. C, Davidson, I. M., Hargest, T.J. and Robinson, D. W. A controlled experiment on the subjective effects of jet engine noise.Journal of Royal Aeronautical Society, Vol 64, January 1960.Google Scholar
6. Crosse, G. W., Davidson, I. M., Hargest, T. J. and Porter, M. J. A controlled experiment on the perception of helicopter rotor noise. Journal of Royal Aeronautical Society, Vol 64, October 1960.Google Scholar
7. Hargest, T. J. Noise of VTOL aircraft. Journal of Sound and Vibration, 1966, 4 (3).Google Scholar
8. Hargest, T. J. and Pinker, R. A. The influence of added narrow band noise and tones in the subjective response to shaped white noise. The Aeronautical Journal of Royal Aero nautical Society, Vol 71, June 1967.Google Scholar
9. Martlew, D. L. Noise associated with shock waves in super sonic jets. AGARD CP 42.Google Scholar
10. Davidson, I. M. and Hargest, T. J. Helicopter noise. Journal of Royal Aeronautical Society, Vol 69, May 1965.Google Scholar
11. Davidson, I. M. The United Kingdom aircraft engine noise research programme. Paper to International Conference on Reduction of Noise and Disturbance caused by Civil Aircraft, London, November 1966.Google Scholar
12. Ahuja, K. K. Correlation and prediction of jet noise. Journal of Sound and Vibration, 1973, 29 (2).Google Scholar
13. Hoch, R. G., Duponchel, J. P., Cocking, B. J. and Bryce, W. D. Studies of the influence of density on jet noise. Journal of Sound and Vibration, 1973, 28 (4).Google Scholar
14 Cocking, B. J. The effect of temperature on subsonic jet noise. NGTE Report No R331, 1974.Google Scholar
15. Cocking, B. J. An experimental study of co-axial jet noise. NGTE Report No R333, 1974.Google Scholar
16. Holbeche, T. A. and Williams, J. Acoustic considerations for noise experiments at model scale in subsonic wind tunnels. RAE Technical Report 72155, September 1972. (Also AGARD Report 601, Paper 8).Google Scholar
17. Cocking, B. J. and Bryce, W. D. An investigation of the noise of cold air jets under simulated flight conditions. NGTE Report No R334, 1974.Google Scholar
18. Cocking, B. J. and Bryce, W. D. Prediction methods for subsonic jet noise in flight based on some recent wind-tunnel results. Unpublished work at NGTE, 1974.Google Scholar
19. Von Glahn, U.,Groesbeck, D.and Goodykoontz, J. Velocity decay and acoustic characteristics of various nozzle geometries in forward flight. AIAA Paper No 73-629, July 1973.Google Scholar
20. Stevens, R. C. K. and Bryce, W. D. An investigation of the noise from a scale model of an engine exhaust system. Un published work at NGTE, 1974.Google Scholar
21. Flintoff, J. L. The Ansty Noise Facility—its design, instru mentation and future commitments. The Aeronautical Journal of Royal Aeronautical Society, Vol 75, June 1971.Google Scholar
22. Amiet, R. Transmission and reflection of sound by a blade row. AIAA Paper No 71-181, January 1971.Google Scholar
23. Crick, K. A. and Martlew, D. L. Experiments on Hartmann noise generators. Unpublished work at NGTE, 1974.Google Scholar