This gaper presents the results of a study of the effects of positive stres
s ratios on the propagation of long and short fatigue cracks in mill anneal
ed Ti-6Al-4V. Differences between the long fatigue crack growth rates at po
sitive stress ratios (R = K-min/K-max = 0.02-0.8) are attributed largely to
the effects of crack closure, Microstructurally short fatigue cracks are s
hown to grow at stress intensity factor ranges below the long crack fatigue
threshold. Anomalously high fatigue crack growth rates and crack retardati
on are also shown to occur in the short crack regime. Differences between t
he long and the short crack behavior at low stress ratios are attributed to
lower levels of crack closure in the short crack regime. (C) 2000 Elsevier
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