“…Critical plane models became popular in recent years because of their success in predicting fatigue life for various engineering materials and under different loading conditions. Models such as Fatemi-Socie [31], Smith-Watson-Topper [28,29] and Jiang [27] have been used to analyse various multiaxial loading paths, different materials on both specimen's and component's levels [25,26,32,[45][46][47][48][49][50]. However, there are studies indicating that the predictions of cracking orientations may not necessarily be in agreement with the critical plane predicted by the models even though fatigue predictions are considered reasonable, generally between ±2Â scatter bands.…”