Creep-fatigue tests of low-carbon and medium-nitrogen type 316 stainless st
eel including elastic follow-up were carried out and the effect of elastic
follow-up on the creep-fatigue life was discussed. Crack growth was observe
d throughout the Life and it was faster in elastic follow-up tests than in
strain-controlled tests. Creep-fatigue life prediction was made by estimati
ng inelastic strain behavior during displacement holding. The ductility exh
austion rule gave good life prediction, whereas the time fraction rule was
non-conservative as the failure life became longer. The ductility exhaustio
n rule is recommended for estimating creep damage under conditions of creep
-fatigue loading with elastic follow-up. (C) 2001 Elsevier Science Ltd. ALI
rights reserved.