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Stress Distribution Around a Central Crack in a Plate Loaded in Tension; Effect of Finite Width of Plate

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Published online by Cambridge University Press:  04 July 2016

J.R. Dixon
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Abstract

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Type
Technical Notes
Information
The Aeronautical Journal , Volume 64 , Issue 595 , July 1960 , pp. 439 - 440
Copyright
Copyright © Royal Aeronautical Society 1960

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References

1.Frost, N. E. and Dugdale, D. S. (1958). The Propagation of Fatigue Cracks in Sheet Specimens. J. Mech. Phys. Solids, 6, 1958.Google Scholar
2.Inglis, C. E. (1913). Stresses in a Plate due to the Presence of Cracks and Sharp Corners. Trans. Inst. Nav. Arch., 55, Part I, 1913.Google Scholar
3.Dixon, J. R. (1956). Institution of Physics (Stress Analysis Group) and Royal Aeronautical Society, Joint Conference, Cranfield, September 1956: Discussion on Crack Propagation. Unpublished.Google Scholar
4.Dixon, J. R. (1959). Photoelasticity Can Help the Designer. Engineering Materials and Design, 2 (12), Dec. 1959.Google Scholar