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Loading and Heating of a Simple Structure with Linear Work Hardening

Published online by Cambridge University Press:  04 July 2016

E. H. Mansfield*
Affiliation:
Royal Aircraft Establishment, Farnborough

Summary:

An analysis is made of the stresses and strains in a loaded two-bar tie when one of the bars is subjected to heating. The material of the bars is assumed to possess linear work hardening characteristics, i.e. a constant tangent modulus in the plastic range, and these characteristics are assumed to be independent of temperature. The following cycles of loading and heating are considered: load-heat-cool-unload, load-heat-unload-cool, heat-load-unload-cool, heat-load-cool-unload, and it is shown how, and when, these cycles produce differing stresses and strains and, in particular, differing residual stresses and strains. The effect of repeated applications of these cycles, when incremental shake-down may occur, is also considered.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1963

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References

1.Parkes, E. W. (1960). Effects of repeated thermal loading. Aircraft Engineering 222-9, August 1960.Google Scholar