When a component is subjected to variable-amplitude loading, if the fundame
ntal stress-life cycle relationship and an accumulation rule are given, the
n the fatigue damage or fatigue life of the component can be calculated and
/or estimated. In the present paper, random vibration theory is incorporate
d into the analysis of the above problem. Several formulas are thus derived
. Experimental work is then carried out to verify the derived formulas. Com
parison is made among the results calculated based on different formulas, d
ifferent accumulation rules and different random loading. It is concluded t
hat the derived formulas do provide us with quick prediction of the fatigue
damage or fatigue life when a component is subjected to variable-amplitude
loading that has a certain random nature. (C) 1999 Elsevier Science Ltd. A
ll rights reserved.