Hostname: page-component-78c5997874-s2hrs Total loading time: 0 Render date: 2024-11-06T07:15:20.303Z Has data issue: false hasContentIssue false

Generalised Stress-Strain Data for Aluminium Alloys and certain other Materials

Published online by Cambridge University Press:  28 July 2016

Anthony J. Barrett
Affiliation:
Technical Department, Royal Aeronautical Society
Maureen E. Michael
Affiliation:
Technical Department, Royal Aeronautical Society

Extract

In many engineering problems it is necessary, from time to time, to deduce from only a few characteristic values data which would ideally be obtained from a complete stress-strain curve. For instance many handbooks, used in design offices and published by materials manufacturers and others, contain values of Young's modulus and minimum guaranteed, or typical, values of various proof stresses for materials. From these, estimates of strain, tangent modulus or ratio of stress to tangent modulus appropriate to known stress values may be required, or various processes involving integration of the stress-strain curve may have to be carried out. Even when a complete stress-strain curve is available from a special test, the differentiation and integration of it, which may have to be repeated several times, are timeconsuming processes. Also, in analytical work involving the use of materials beyond the limit of proportionality, it is desirable to have available a generalised mathematical form of the stress-strain curve in order that the results obtained may be applied to a wide range of actual materials simply by the substitution of appropriate coefficients. These and many other applications will be familiar to the reader.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1955

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.)

References

1.Royal Aeronautical Society. Structures Data Sheets 00.02.01, 02 and 03. June 1948 and October 1951.Google Scholar
2. Nicholls, A. C. (1954). Empirical Formulae for the Determination of Stress Curves. Journal of the Royal Aeronautical Society, October 1954.CrossRefGoogle Scholar
3. Rameerg, W. and Osgood, W. R. (1943). Description of Stress–Strain Curves by Three Parameters. N.A.C.A. T.N.902, April 1943.Google Scholar
4. Barrett, Anthony J. (1953). The Bending of Some Common Beam Sections into the Plastic Range. Journal of the Royal Aeronautical Society, February 1953.CrossRefGoogle Scholar
5. Durham, R. J. (1953). Stress–Strain Curves for Some Noral Wrought Alloys. Aluminium Laboratories Research Bulletin No. 2, June 1953.Google Scholar
6. Lego, K. L. C. and Wright, J. H. (1954). Note on Proposed Revised R.Ae.S. Data Sheets for Stress-Strain Curves. Short Bros. & Harland Note S.D. No. 2, September 1954.Google Scholar
7. Barrett, Anthony J. (1953). Unsymmetrical Bending and Bending Combined with Axial Loading of a Beam of Rectangular Cross Section into the Plastic Range. Journal of the Royal Aeronautical Society, August 1953.CrossRefGoogle Scholar