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Cyclic plasticity models and application in fatigue analysis
Authors:I. Kalev
Affiliation:

National Research Council—NASA Dryden Research Associate, NASA Dryden Flight Research Center, Edwards, CA 93523, U.S.A.

Abstract:An analytical procedure for prediction of the cyclic plasticity effects on both the structural fatigue life to crack initiation and the rate of crack growth is presented. The crack initiation criterion is based on the Coffin-Manson formulae extended for multiaxial stress state and for inclusion of the mean stress effect. This criterion is also applied for the accumulated damage ahead of the existing crack tip which is assumed to be related to the crack growth rate. Three cyclic plasticity models, based on the concept of combination of several yield surfaces, are employed for computing the crack growth rate of a cracked plane stress panel under several cyclic loading conditions.
Keywords:
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