NASA NTRS · 19870032345
Fatigue crack propagation rate model based on a dislocation mechanism
Abstract
It has been noted that the crack propagation exponent p for most metals usually varies between values of 2 and 4, and that the motion of dislocations plays an important part in determining the exponent p. Attention is presently given to the significance of the exponent p in terms of the motion of dislocations, in view of the theory of thermally activated plastic flow and the cumulative plastic strain concept for a failure criterion.
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Mazumdar, P. K., Jeelani, S.. 1986-10-01. Fatigue crack propagation rate model based on a dislocation mechanism. https://ntrs.nasa.gov/citations/19870032345
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