Hostname: page-component-6587cd75c8-vj8bv Total loading time: 0 Render date: 2025-04-24T00:52:02.324Z Has data issue: false hasContentIssue false
  • English
  • Français

The Eftect of Jet Noise on Aircraft Structures

Published online by Cambridge University Press:  07 June 2016

B. L. Clarkson
B. L. Clarkson*
Affiliation:
Department of Aeronautical Engineering, The University of Southampton
Get access

Summary

The present state of knowledge on the problem of fatigue failure due to vibrations excited by jet noise is reviewed. It is concluded that it should currently be possible to make reasonable estimates of the stress levels set up in a structure by jet noise but, in general, the resultant fatigue life of the components cannot be estimated with any confidence.

Type
Research Article
Information
Aeronautical Quarterly , Volume 10 , Issue 2 , May 1959 , pp. 103 - 126
Copyright
Copyright © Royal Aeronautical Society. 1959

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.)

Article purchase

Temporarily unavailable

References

1. Liepmann, H. W. On the Application of Statistical Concepts to the Buffeting Problem. Journal of the Aeronautical Sciences, December 1952.CrossRefGoogle Scholar
2. Powell, A. The Problem of Structural Failure due to Jet Noise. A.R.C. 17,514, March 1955.Google Scholar
3. Powell, A. On the Fatigue Failure of Structures due to Vibrations Excited by Random Pressure Fields. General Theory. A.R.C. 17,925, October 1955.Google Scholar
4. Powell, A. On Structural Vibrations Excited by Random Pressures. Douglas Report S.M.22795. To be published. Google Scholar
5. Thompson, W. T. and Barton, M. V. Response of Mechanical Systems to Random Excitation. Journal of Applied Mechanics, July 1957.CrossRefGoogle Scholar
6. Foxwell, J. H. and Franklin, R. E. Acoustic Effects in the Vibrations of Structures. A.R.C. 19,495, August 1957.Google Scholar
7. Foxwell, J. H., and Franklin, R. E. The Vibrations of a Thin-Walled Stiffened Cylinder in an Acoustic Field. The Aeronautical Quarterly, Vol. X, February 1959.Google Scholar
8. Richards, E. J. Research on Aerodynamic Noise from Jets and Associated Problems. Journal of the Royal Aeronautical Society, May 1953.CrossRefGoogle Scholar
9. Powell, A. Survey of Experiments on Jet Noise. Aircraft Engineering, January 1954.CrossRefGoogle Scholar
10. Richards, E. J., Greatrex, F. B., Lilley, G. M., Warren, C. H. E., Fleming, N. and Hayhurst, J. D. Symposium. Aeronautical Acoustics—In Particular Jet Noise. Journal of the Royal Aeronautical Society, April 1954.Google Scholar
11. Laurence, J. C. Intensity, Scale and Spectra of Turbulence in Mixing Region of Free Subsonic Jet. N.A.C.A. Report 1292, 1956.Google Scholar
12. Hubbard, H. H. and Lassiter, L. W. Experimental Studies of Jet Noise. Journal of the Acoustical Society of America, May 1953.Google Scholar
13. Greatrex, F. B. Jet Noise. Fifth International Aeronautical Congress, Los Angeles, 1955. Institute of the Aeronautical Sciences, 1956.Google Scholar
14. Franklin, R. E. The Estimation of Fluctuating Pressures in the Near Field of a Jet. (Interim Report.) A.R.C. 17,987, November 1955.Google Scholar
15. Howes, W. L. and Mull, H. R. Near Noise Field of a Jet Engine Exhaust. I. Sound Pressures. N.A.C.A. T.N. 3763, October 1956.Google Scholar
16. Lighthill, M. J. On Sound Generated Aerodynamically, Part I. Proc. Roy. Soc, Vol. 211, A, 1952.Google Scholar
17. Lighthill, M. J. On Sound Generated Aerodynamically, Part II. Proc. Roy. Soc, Vol. 222, A, 1954.Google Scholar
18. Gerrard, J. H. Investigation of Noise Produced by a Subsonic Air Jet. Journal of the Aeronautical Sciences, September 1956.Google Scholar
19. Powell, A. On the Mechanism of Choked Jet Noise. Proceedings of the Physical Society, B, 66, p. 1039, 1953.CrossRefGoogle Scholar
20. Richards, E. J. Noise Research in the United Kingdom. Canadian Aeronautical Institute Preprint 7/7, May 1957.Google Scholar
21. Fowell, L. R. and Korbacher, G. K. Review of Aerodynamic Noise. Institute of Aero- physics, Toronto, Review 8.Google Scholar
22. Wolfe, M. O. W., Franklin, R. E., Mead, D. J., Clarkson, B. L. and Hetzel, K. W. Jet Efflux. A Symposium. Journal of the Royal Aeronautical Society, February 1957.Google Scholar
23. Richards, E. J., Mead, D. J., Franklih , R. E., Maclachlan, K. R. and others. Notes of the Conference on Aeronautical Acoustics, March 1957. Southampton University. Unpublished.Google Scholar
24. Callaghan, E. E., Howes, W. L., Coles, W. D., Conger, C. C. and Berg, D. F. Near Noise Field of a Jet Engine Exhaust. II. Cross Correlation of Sound Pressures. N.A.C.A. T.N. 3764, September 1956.Google Scholar
25. Foxwell, J. H. and Frankun, R. E. Pressure Fluctuation Near a Cold, Small-Scale Air Jet. A.R.C. 20,182, April 1958.Google Scholar
26. Foxwell, J. H. and Franklin, R. E. Correlation in the Random Pressure Field Close to a Jet. A.R.C. 20,264, June 1958.Google Scholar
27. Arnold, R. N. and Warburton, G. B. Flexural Vibrations of the Walls of Thin Cylindrical Shells having Freely Supported Ends. Proc. Roy. Soc, Vol. 197, 1949.Google Scholar
28. Arnold, R. N. and Warburton, G. B. Flexural Vibrations of Thin Cylinders. Proceedings of the Institution of Mechanical Engineers (A), Vol. 167, 1953.Google Scholar
29. Miller, P. R. Free Vibrations of a Stiffened Cylindrical Shell. A.R.C. 19,338, May 1957.Google Scholar
30. Mead, D. J. The Internal Damping due to Structural Joints. A.R.C. 19,870, January 1958.Google Scholar
31. Mead, D. J. The Effect of a Damping Compound on Jet Efflux Excited Vibrations. Part I: The Structural Damping due to the Compound. A.R.C. 20,155, July 1958.Google Scholar
32. Mead, D. J. The Effect of a Damping Compound on Jet Efflux Excited Vibrations. Part II: The Reduction of Vibration and Stress Level due to the Compound. A.R.C. 20,263, November 1958.Google Scholar
33. Junger, M. C. The Outgoing Wave in Cylindrical Co-ordinates. Journal of the Acoustical Society of America, Vol. 25, 1953.Google Scholar
34. Miles, J. W. Structural Fatigue under Random Loading. Journal of the Aeronautical Sciences, November 1954.Google Scholar
35. Eringen, A. C. Response of Beams and Plates to Random Loads. Journal of Applied Mechanics, March 1957.Google Scholar
36. Lassiter, L. W., Hess, R. W. and Hubbard, H. H. Experimental Study of the Response of Simple Panels to Intense Acoustic Loading. Journal of the Aeronautical Sciences, January 1957.Google Scholar
37. Kirchmann, E. J. and Greenspon, J. E. Non-Linear Response of Aircraft Panels in Acoustic Noise. Journal of the Acoustical Society of America, July 1957.Google Scholar
38. Freudenthal, A. M. and Heller, R. A. Accumulation of Fatigue Damage. Presented at the Conference, Fatigue in Aircraft Structures, Columbia University, 1956. Academic Press Inc., New York.Google Scholar
39. Miner, M. A. Cumulative Damage in Fatigue. Journal of Applied Mechanics, Vol. 12, 1945.Google Scholar
40. Rice, S. O. Mathematical Analysis of Random Noise. Bell System Technical Journal, Vol. 24, 1945.CrossRefGoogle Scholar