Prediction of notched specimen behaviour at ambient and high temperatures in Ti6246

Life prediction methods are essential in the selection of materials for high performance applications. These design criteria allow safe lives to be predicted for areas of geometrical discontinuity where localized increases in stress lead to the early initiation and propagation of fatigue cracks under cyclic loading. This paper explains two methods for predicting the initiation life of a double edged notch specimen (Kt = 1.9), and applies them to the α + β titanium alloy Ti6246 over a range of temperatures. The Coffin–Manson equation is effective for fully reversed cyclic behaviour. However a Walker strain-based parameter was found to be more appropriate when mean stresses are introduced. The analysis encompasses traditional analytical approaches which are limited in relation to the determination of the stresses and strains at the notch root and a finite element analysis based on ABAQUS®. The FEA is used to characterize loop generation at the notches and to optimize the stress and strain conditions in the critical root positions. The main focus of the paper, however, is high temperature behaviour where creep and environmental damage impact on fatigue crack development. The limitations of the modelling approach under these conditions are discussed.