A B S T R A C T In this paper, compact tension specimens with tilted cracks under monotonic fatigue loading were tested to investigate I + III mixed mode fatigue crack propagation in the material of No. 45 steel with the emphasis on the mode transformation process. It is found that with the crack growth, I + III mixed mode changes to Mode I. Crack mode transformation is governed by the Mode III component and the transformation rate is a function of the relative magnitude of the Mode III stress intensity factor. However, even in the process of the crack mode transformation the fatigue crack propagation is controlled by the Mode I deformation. a x = crack length in horizontal direction (mm) a y = crack length in vertical direction (mm) A = material components ( • /mm) B = thickness of CT specimen (mm) M = material components C = material components ( • /mm) |dθ/da x | = change rate of the angle θ da/dN = fatigue crack propagation rate (mm/cycle) H = width of the notch (mm) W = width of CT specimen (mm) β = tilt angle ( • ) K I = alternating amplitude of Mode I stress intensity factor (MPa·m 1/2 ) K III = alternating amplitude of Mode III stress intensity factor (MPa·m 1/2 ) K e = alternating amplitude of effective stress intensity factor (MPa·m 1/2 ) θ = instantaneous value of the tilt angle β ( • ) σ s = yield strength (MPa) σ b = tensile strength (MPa)