Mixed-mode, high-cycle fatigue-crack growth thresholds are reported for through-thickness cracks (large compared to microstructural dimensions) in a Ti±6Al±4V turbine blade alloy with a bimodal microstructure. Speci®cally, the eect of combined mode I and mode II loading, over a range of phase angles b tanÿ1
DKII=DKI from 0° to 82°
DKII=DKI 0±7), is examined for load ratios (ratio of minimu...