The fretting fatigue behavior of Ti-6Al-4V under both constant amplitude an
d variable amplitude loadings was investigated. Constant amplitude fretting
fatigue tests were conducted at a frequency of 200 Hz as well as at 1 Hz,
while the variable amplitude loading combined the interaction of these two
frequencies. The axial load ratios ranged from nominal values of 0.1 to nom
inal values of 0.8. Fretting fatigue lives at the higher frequency were fou
nd to be less than those from tests conducted at the lower frequency with a
larger difference being noted at higher axial load ratios. In general, fre
tting fatigue resistance for the variable amplitude loading conditions fell
within the scatter band of the 200 Hz constant amplitude fretting fatigue
tests. Miner's linear damage summation model provided a reasonable, yet sli
ghtly unconservative, prediction of the variable amplitude loading tests. (
C) 1999 Elsevier Science Ltd. All rights reserved.