A theoretical analysis is performed for the effect of strain hardening on f
atigue crack closure in plane stress and plane strain conditions based on a
modified strip yield model. It is shown that the effect of the strain hard
ening exponent n on the opening stress ratio is small, less than 1.3% in pl
ane stress and about 10% in plane strain, respectively, for n>3. Comparing
with available finite element results and experimental data in both stress
states shows good agreement. When the opening stresses in plane stress and
plane strain are applied to deal with fatigue crack growth data in very thi
n and;thick plates respectively, the data for different stress ratios colla
pse into a single curve. (C) 1999 Elsevier Science Ltd. All rights reserved
.