An FEA (finite element analysis) program employing a new scheme for crack g
rowth analysis is developed and a prediction method for crack growth life i
s proposed. The FEA program consists of the subroutines for the automatic e
lement re-generation using the Delaunay Triangulation technique, the elemen
t configuration in the near-tip region being provided by a super-element, e
lasto-inelastic stress analyses, prediction of crack extension path and cal
culation of fatigue life. The FEA results show that crack extension rate an
d path are controlled by a maximum opening stress range, Delta sigma theta
(max), at a small radial distance of r = d, where d is chosen to be a grain
diameter's distance, 3.5 mum, in solder material. The experimentally obtai
ned crack extension rate is found to be related to doe,,, in FEA as da/dN =
beta[Delta sigma (theta max) - gamma](alpha), where alpha = 2.0, beta = 4.
5 x 10(-9) mm(5)/N-2 and gamma = 98 MPa are determined for all test conditi
ons. The calculated values of crack extension life by the FEA using the abo
ve equation are in good agreement with the experimental ones and are indepe
ndent of the joint types.