A strip yield model implementation by the present authors is applied to predict fatigue crack growth observed in structural steel specimens under various constant and variable amplitude loading conditions. Attention is paid to the model calibration using the constraint factors in view of the dependence of both the crack closure mechanism and the material stress-strain response on the load history. Prediction capabilities of the model are considered in the context of the incompatibility between the crack growth resistance for constant and variable amplitude loading.

The paper contains the tatigue tests results for specimens made of three cast irons under proportional and non-proportional variable amplitude tension with torsion. The experimental data for long fatigue life have been compared with those calculated according to the algorithm with use of the modified criterion of the maximum normal stress in the critical plane. In the considered algorithm the Palmgren-Miner hypothesis of damage cumulation seems to he useless whereas the Serensen-Kcgaycv hypothesis gives satisfactory results. Applying the method of fatigue damage cumulation we obtain the critical plane direction which agrees with the experimental fracture plane very well.