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Noise research

Part of: Sustainable Aerospace

Published online by Cambridge University Press:  04 July 2016

I. C. Cheeseman
I. C. Cheeseman*
Affiliation:
Southampton University
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Extract

The development of the jet engine produced jet noise problems. Most of the understanding of jet noise was and is performed in universities. The fundamental and quite exceptional work of Lighthill was followed by that of Curie. Powell and Ffowcs Williams at Southampton in the early 1950s and was paralleled by experimental investigations on noise suppression by for example. Lilley at Cranfield. This university work was used to form the basis of a programme of research into jet engine noise at Ministry of Aviation establishments with considerable university inputs which established a commanding lead for the United Kingdom in the understanding of jet noise.

The formation of the Institute of Sound and Vibration Research at the University of Southampton under the inspiration of Professor E. J. Richards was a step which placed university research at a different level to that usually observed in the United Kingdom by concentrating in one place some 40-50 people all devoted to research and postgraduate education.

Type
Universities — Have They a Role in Aeronautical Research?
Information
The Aeronautical Journal , Volume 87 , Issue 866 , July 1983 , pp. 210 - 218
Copyright
Copyright © Royal Aeronautical Society 1983 

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References

1. Tester, B. J. and Fisher, M. J. Engine noise source breakdown. Theory, Simulation and Results. AIAA 7th Aeroacoustic Conference, Palo Alto, 1981, Paper 81-2049.Google Scholar
2. Ffowcs-Williams, J. E. The silent noise of a gas turbine. DSPectrum: British Science News No. 174/1, 1981, 9–11.Google Scholar
3. Ross, C. F. An algorithm for designing a broadband active sound control system. J. of Sound and Vibration, 1982, 80, 3, 373–380.Google Scholar
4. Ross, C. F. A demonstration of active control of broadband sound.J. of Sound and Vibration, 1981, 74, 3, 411–417.Google Scholar
5. Ross, C. F. An adaptive digital filter for broadband active sound control. J. of Sound and Vibration, 1982, 80, 3, 381–388.Google Scholar
6. Swinbanks, M. A. The active control of sound propagation in long ducts. J. of Sound and Vibration, 1973, 27, 3, 411–436.Google Scholar
7. Tadghighi, H. and Cheeseman, I. C. A study of helicopter rotornoise, with special reference to tail ratios using an acoustic windtunnel. Vertica, 1983, 7, 9–32.Google Scholar
8. Williams, J. and Law, M. R. P. Helicopter flight-path and acoustic signal repeatability for noise-diagnosis and noise certification. RAE Tech. Memo., Aero, Sept. 1973.Google Scholar
9. Done, G. T. S. and Hughes, A. D. The response of a vibrating structure as a function of structural parameters. J. Sound and Vibration, 1975, 38, 2, 255–266.Google Scholar
10. Done, G. T. S. and Hughes, A. D. Reducing vibration by structural modification. Proc. 1st European Rotorcraft and Powered Lift Forum, Southampton, England. 22-24 Sept. 1975, Vertica, 1976, 1, 1, 31–38.Google Scholar
11. Done, G.T.S., Hughes, A. D. and Webby, J. The response of a vibrating structure as a function of structural parameters — application and experiment. J. Sound and Vibration. November 1976, 49, 2, 149–159.Google Scholar
12. Done, G. T. S. and Rangacharyulu, M. A. V. A survey of structural optimisation under dynamic constraints. Shock and Vibration Digest, December 1979, 11, 12, 15–25.Google Scholar
13. Done, G. T. S. and Rangacharyulu, M. A. V. Use of optimisation in helicopter vibration control by structural modification. Proc. 5th European Rotorcraft and Powered Lift Aircraft Forum, Amsterdam, The Netherlands. 4-7 September 1979.Google Scholar
14. Done, G. T. S. Use of optimisation in helicopter vibration control by structural modification. Paper No. 27, AHS specialists meeting on helicopter vibration, Hartford, Connecticut, Nov. 1981.Google Scholar
15. Done, G. T. S. and Gibbons, M. P. Automatic generation of helicopter rotor aeroelastic equations of motion. Paper No. 3.3, 8th European Rotorcraft Forum, Aix-en-Provence, Sept. 1982.Google Scholar
16. Elder, R. L., Forster, C. P. and Gill, M. E. Initial findings during studies of the flow with a high speed impeller using a transit anemometer. 4th International Conference, Photon Correlation Techniques in Fluid Mechanics, 1980, Stanford University.Google Scholar
17. Langdon, P. J. Lasers help improve diesel economy. High Speed Diesel Report, September/October 1982.Google Scholar
18. Adkins, R. C. A simple method for designing optimum annula diffusers. 1983. ASME 83-GT-42.Google Scholar
19. Adkins, R. C. and Binks, D. A configuration to improve the aerodynamics and scope of can-annular combustors. 1983. ASME83-GT-37.Google Scholar
20. Adkins, R. C. and Yost, J. O. The hybrid diffuser. 1980. ASME 80-GT-136.Google Scholar
21. Fishenden, C. R. and Stevens, S. J. The performance of annula combustor-dump diffusers. Journal of Aircraft, Jan. 1977, 14.Google Scholar
22. Stevens, S. J. Nayak, U. S. L. Robinson, P. J. and Scrivener, C. T. The influence of compressor exit conditions on the performance of combustor-dump diffusers. Journal of Aircraft, 1978, 15, No. 8.Google Scholar
23. Stevens, S. J., Harasgama, S. P. and Wray, P. The influence of curved wakes on the performance of combustor pre-diffusers. July 1981. AIAA Paper No. 81-1387.Google Scholar
24. Stevens, S. J. and Harasgama, S. P. The influence of curved compressor outlet guide vanes on the performance of a combustor pre-diffuser. Dept. of Transport Technology Report No. TT 79R03, Loughborough University of Technology.Google Scholar
25. Stevens, S. J. and Williams, G. J. The influence of inlet conditions on the performance of annula diffusers. ASME Journal of Fluids Engineering, 1980, 102, No. 3.Google Scholar
26. Jasusa, A. K. Plain-jet airblast atomisation of alternative liquid petroleum fuels under high ambient air pressure conditions. 1982. ASME 82-GT-32.Google Scholar
27. Reason, B. R. and Siew, A. H. A new approach to journal bearing design. Conference Proceedings AGARD No. 323, Problems in Bearings and Lubrication, 31st May/3rd June 1982.Google Scholar