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Structural Safety

Published online by Cambridge University Press:  28 July 2016

A. G. Pugsley*
Affiliation:
University of Bristol

Extract

The present preoccupation of aircraft designers and users with fatigue problems, brought to a head by the Comet disasters, has rendered the notion of the finite life of an aeroplane a commonplace to the man in the street, and has made the assessment of probabilities of failure and the collection of statistics regarding loads and structural properties a matter of detailed concern for all designers. This was not always so. In 1939, when Fairthorne and I essayed a first paper on airworthiness statistics it received practically no attention and publication was delayed for years until after the 1939–45 War. Even in 1942, an exploratory “ Philosophy of Aeroplane Strength ” brought smiles to the faces of practical designers rather than the real interest that the “new slant,” as some said, of its probability approach raised in a few scientists.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1955

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References

1. Pugsley, A. G. and Fairthorne, R. A. (1939). Note on Airworthiness Statistics. A.R.C., London, R. & M. 2224, 1939.Google Scholar
2. Pugsley, A. G. (1942). A Philosophy of Aeroplane Strength. A.R.C., London, R. & M. 1906, 1942.Google Scholar
3. Walker, P. B. (1953). Estimation of the Fatigue Life of a Transport Aircraft. Journal of the Royal Aeronautical Society, London, Vol. 57, October, 1953.Google Scholar
4. Pugsley, A. G. (1951). Concepts of Safety in Structural Engineering. Journal of Institution of Civil Engineers, London, Vol. 36, 1951.Google Scholar
5. Prot, M. (1948). La Securité des Constructions. 3rd Congress, International Association of Bridge and Structural Engineering, Liège, 1948.Google Scholar
6. Johnson, A. I. (1953). Strength, Safety and Economical Dimensions of Structures. Meddelander 12, Inst, of Byggnadsstatik, Roy. Inst. of Technology, Stockholm, 1953.Google Scholar
7. Freudenthal, A. M. (1947). The Safety of Structures. Trans. American Society of Civil Engineers, New York, Vol. 112, 1947.Google Scholar
8. Freudenthal, A. M. (1954). Safety and the Probability of Structural Failure. Proceedings American Society of Civil Engineers, New York, Vol. 80, 1954.Google Scholar
9. Pugsley, A. G. (1947). The Behaviour of Structures under Repeated Loads. Journal of the Royal Aeronautical Society, London, Vol. 51, 1947.Google Scholar
10. Freudenthal, A. M. and Gumbel, E. S. (1953). On the Statistical Interpretation of Fatigue Tests. Proceedings of the Royal Society, London, A., Vol. 216, 1953.Google Scholar
11. Prot, M. (1948). L'essai de Fatigue sous Change Progressive. Rev. Metall., Paris, 12, 1948.Google Scholar
12. Freudenthal, A. M. (1954). A Random Fatigue Testing Procedure and Machine. Proc. American Society for Testing Materials, New York, Vol. 54, 1954.Google Scholar
13. McAdam, D. J. (1927). Corrosion-Fatigue of Non-Ferrous Metals. Proc. American Society for Testing Materials, New York, Vol. 27, II, 1927.Google Scholar
14. Gough, H. J. and Sopwith, D. G. (1935). Some Further Experiments on Atmospheric Action in Fatigue. Journal of Institute of Metals, London, Vol. LVI, 1935.Google Scholar
15. McAdam, D. J. and Clyne, R. W. (1934). Influence of Chemically and Mechanically Formed Notches on Fatigue of Metals. Bureau of Standards, Journal of Research, Washington, Vol. 13, 1934.Google Scholar
16. Gerard, I. J. and Sutton, H. (1935). Corrosion-Fatigue Properties of Duralumin with and Without Protective Coverings. Journal of Institute of Metals, London, Vol. LVI, 1935.Google Scholar
17. Inglis, N. P. and Larke, E. C. (1954). Corrosion-Fatigue Properties of an Aluminium-Magnesium-Silicon Alloy in the Unprotected, Anodized and Painted Conditions. Journal of Institute of Metals, London, Vol. 83, December, 1954.Google Scholar
18. Loveless, E. and Boswell, A. C. (1954). The Problem of Thermal Stresses in Aircraft Structures. Aircraft Engineering, London, Vol. XXVI, April, 1954.Google Scholar
19. Parkes, E. W. (1954). Wings under Repeated Thermal Stress. Aircraft Engineering, London, Vol. XXVI, December, 1954.Google Scholar
20. Freudenthal, A. M. (1954). Effect of Rheological Behavior on Thermal Stresses. Journal of Applied Physics, New York, Vol. 25, September, 1954.Google Scholar
21. Report on Structural Safety (1955). Journal of the Institution of Structural Engineers, Vol. 23, May 1955.Google Scholar