Dimensional changes in the form of necking and bulging occur in the shape of cylindrical and hourglass commercially pure aluminum specimens subjected to axial push-pull cyclic loading. The present report deals with the effect of these changes on the resistance to deformation and fracture by fatigue. It is found that the change in shape due to instability affects the stress range response of the material during cycling. The control of shape permits a steady-state response with cycling regardless of the prior state of strain in the material. With an appropriate correction for the shape constraint effect, the steady-state stress range achieved is the same with or without shape control. Frequent removal of the surface material to control the specimen profile during cycling leads to a stabilized hysteresis loop and an indeterminate extension in the fatigue life.
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December 1963
This article was originally published in
Journal of Basic Engineering
Research Papers
Geometrical Effects in Strain Cycled Aluminum
M. H. Raymond,
M. H. Raymond
General Electric Research Laboratory, Schenectady, N. Y.
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L. F. Coffin
L. F. Coffin
General Electric Research Laboratory, Schenectady, N. Y.
Search for other works by this author on:
M. H. Raymond
General Electric Research Laboratory, Schenectady, N. Y.
L. F. Coffin
General Electric Research Laboratory, Schenectady, N. Y.
J. Basic Eng. Dec 1963, 85(4): 548-554 (7 pages)
Published Online: December 1, 1963
Article history
Received:
August 27, 1962
Online:
November 3, 2011
Citation
Raymond, M. H., and Coffin, L. F. (December 1, 1963). "Geometrical Effects in Strain Cycled Aluminum." ASME. J. Basic Eng. December 1963; 85(4): 548–554. https://doi.org/10.1115/1.3656909
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