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The Noise of Rotorcraft and other VTOL Aircraft— A Review

Published online by Cambridge University Press:  04 July 2016

I. C. Cheeseman
I. C. Cheeseman*
Affiliation:
Department of Aeronautics and Astronautics, The University, Southampton
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Extract

The need to understand the mechanism of generation and to be able to predict the noise of aircraft has increased enormously in the present decade. The questions which the aircraft designer now poses to the noise engineer are much more difficult to answer than was the case in 1964 when rotorcraft noise was discussed by this Section. For example in the case of conventional transport aircraft at the beginning of this decade it was only necessary to show that on take off the peak noise did not exceed 110 PNdB at a predetermined monitoring point at certain airfields. With the advent of noise certification it is now necessary to know the complete noise time history of the aircraft for points under the take off path, at the side and on the approach before the aircraft flies or the engine is made. The increased emphasis on noise research and the resulting developments in the theory and practice is not surprising.

Type
Research Article
Information
The Aeronautical Journal , Volume 75 , Issue 726 , June 1971 , pp. 406 - 412
Copyright
Copyright © Royal Aeronautical Society 1971 

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References

1. Baker, CD, Development of Air Transport in the 1970's. 18th Convegno Internazionale delle Communicazioni, Genoa, October, 1970.Google Scholar
2. Helicopter and V/STOL noise generation and suppression. National Academy of Sciences and Engineering Report, July, 1968.Google Scholar
3. Davidson, I. M. and Hargest, T. J. Helicopter Noise. Journal of the Royal Aeronautical Society Vol 69, May, 1965.Google Scholar
4. Yudin, E. Y. On the Vortex Sound from Rotating Rods. NACA T.M. 1136,1947.Google Scholar
5. Stuckey, T. J. and Goddard, J. O. Investigation and prediction of Helicopter Noise: 1 Wessex Whirl Tower Results. J Sound and Vib. Vol 5, 50.Google Scholar
6. Leverton, J. W. Helicopter Noise. AGARD Conf Ottawa, June, 1968.Google Scholar
7. Schlegel, R. G. and Bausch, W. E. Helicopter Rotor Noise Prediction and Control. J Amer Hel Soc, July, 1969.Google Scholar
8. Leverton, J. W. Helicopter Noise, ISAV Memo 167, November, 1966.Google Scholar
9. Wright, S. E. Sound Radiation from a Lifting Rotor, J Sound and Vib Vol 9, No. 2, 1969.Google Scholar
10. Lowson, M. W. and Ollerhead, J. B. Helicopter Rotor Noise, J Sound and Vib Vol 9, No. 2, 1969.Google Scholar
11. Sheeman, J. A Tabulation of Helicopter Rotor Differential Pressures, Stresses and Motions as Measured in Flight. NASA TM TMX-952, 1964.Google Scholar
12. Leverton, J. W. Helicopter Blade Slap. J Sound and Vib. Vol 4(3), 1966.Google Scholar
13. Leverton, J. W. and Taylor, F. W. Helicopter Blade Slap, US Army Scientific Symposium, June, 1966.Google Scholar
14. Leverton, J. W. Helicopter Noise—Blade Slap. NASA CR 1221, October, 1968.Google Scholar
15. Gustafson, F. B. Powered Lift Research at Langley Field. Journal of the Royal Aeronautical Society Vol 67, p. 371, 1963.Google Scholar
16. Smith, M. J. T. and House, M. E. Internally Generated Noise from Gas Turbine Engines. Measurement and Predic tion, ASME paper 66. GT/N-43, 1965.Google Scholar
17. Tyler, J. M. and Sofrin, T. C. Axial Flow Compressor Noise Studies. Trans SAE Vol 70, p. 309, 1962.Google Scholar
18. Mather, J. S. B., Fisher, M. J. and Savidge, J. New Obser vations on Tone Generation in Fans: Symposium on Aero dynamic Noise, Loughborough, September, 1970.Google Scholar
19. Barry, B. and Moore, C. J. Subsonic Fan Noise. Symposium on Aerodynamic Noise, Loughborough, September, 1970.Google Scholar
20. Hauterkeuser, E. G. and Sternfeld, H. Jr. Subjective Response to Synthesized Flight Noise Signature of Several Types of V/STOL Aircraft. NASA CR-1118, August, 1968.Google Scholar
21. Robinson, D. W. The Noise Pollution Concept. BAS. Preprint 70/101, July, 1970.Google Scholar
22. Wilde, C. L. and Coplen, J. F. Lift Turbo Fans. Journal of the Royal Aeronautical Society Vol 69, p. 553, 1965.Google Scholar
23. West, R. G. Fan Lift in VTOL Design. The Aeronautical Journal of the Royal Aeronautical Society Vol 73, p. 657, 1969.Google Scholar
24. Pickerell, D. J. High Speed VTOL Transports. The Powerplant Designer's Problems. RAeS Symposium on Short Range Transport, 1969.Google Scholar
25. Nordstran, D. C. and Miller, D. S. Noise Predictions and Economic Effects of Boeing-Nacelle Modifications. Progress of NASA research relating to noise alleviation of large subsonic jet aircraft, 1968.Google Scholar