An elastic-plastic finite element analysis is performed to investigate deta
iled closure behavior of fatigue cracks and the numerical results are compa
red with experimental results. The finite element analysis performed under
plane stress using 4-node isoparametric elements can predict fatigue crack
closure behavior. The mesh of constant element size along crack surface can
not predict the opening level of fatigue crack. The crack opening level fo
r the constant mesh size increases linearly from initial crack growth. The
crack opening level for variable mesh size, is almost flat after crack tip
has passed the monotonic plastic zone. The prediction of crack opening leve
l using the variable mesh size proportioning the reversed plastic zone size
with the opening stress intensity factors presents a good agreement with t
he experimental data regardless of stress ratios.