High cycle fatigue (HCF) failures in materials used in rotating components
of gas turbine engines have often been found to be attributable to fatigue
loading on materials which have sustained damage from other sources. Damage
can be present in the form of initial material or manufacturing defects, o
r can develop during service operation. Three major sources of in-service d
amage have been identified which can alter the HCF resistance individually
or in conjunction with one another: low cycle fatigue (LCF), foreign object
damage (FOD), and fretting. Methodologies for treating such damage in esta
blishing material allowables are considered. Some recent results on the eff
ects of damage on the Haigh (Goodman) diagram and a discussion of the life
management aspects of HCF are presented. (C) 1999 Published by Elsevier Sci
ence Ltd. All rights reserved.