Degradation of the residual strength of a glass-fiber-reinforced polyester
composite of a lay-up typical of the wind rotor blade material is studied a
t low-cycle fatigue. A gradual reduction of the residual strength is observ
ed as expected for GRP, accompanied by an increasing scatter of strength. T
he residual strength model based on the strength-life equal rank assumption
yields an accurate approximation of experimental data. The strength reduct
ion at a stress level corresponding to high-cycle fatigue (N > 10(6) cycles
) appears to correlate Hell with the test results at higher stress levels,
which indicates that the strength degradation at the design str-ess level c
an be evaluated using low-cycle tests. Assuming that the parameters of the
strength degradation model do not depend on the applied stress level, the r
esidual strength data obtained in low stress level tests of comparatively s
hort duration can be used to estimate the average fatigue life at the same
stress thus reducing the total test time.