Fatigue crack growth and the fracture resistance curve (R-curve) were investigated in a polycrystalline alumina (AD90) and a silicon carbide whisker-reinforced alumina composite (Al,O,-SiC,) at room temperature in air using a combined loading technique for stabilizing crack growth, and a surface film technique for monitoring crack length. Fatigue crack growth was evaluated successfully with those experimental techniques. Load shedding tests were performed until the crack became dormant, in order to determine the threshold stress intensity factor Kth. Subsequently, the specimens were used for quasi-static crack growth tests under a monotonic loading condition. The R-curves were determined in this experiment; however, fracture resistance did not increase markedly with crack growth. Detailed observations of the crack growth behaviour revealed that the flat R-curve was attributed to the shielding effect of the fatigue crack tip wake. Thus, the fatigue precrack introduced by the load shedding test was not regarded as an ideal crack for determining the R-curve. Fractographic observations were performed to investigate the mechanistic difference between fatigue and quasi-static crack growth. It was found that the cyclic loading produced fretting damage in the wake region and it reduced the shielding effect of the fatigue cracks. Based on the experimental results, the relationship between the fatigue crack growth and the R-curve is discussed as is the significance of Kth as a material parameter. NOMENCLATURE a =crack length a, =notch length a,, = crack length when Kth is achieved B = specimen thickness E = Young's modulus COD = crack opening displacement da/dt =crack growth rate with time da/dN = crack growth rate with cycles H = specimen height K = stress intensity factor Kf, =fatigue fracture toughness at which fatigue crack growth becomes unstable K,, = fracture toughness K,,, = maximum stress intensity factor K,,, = minimum stress intensity factor K , = fracture toughness with maximum shielding effect K,h =threshold stress intensity factor 1 = distance from the tensile load line to the compressive load line m, C =Paris law constants N = number of cycles P, = compressive load applied to the ligament of specimen W = specimen width Aa = crack extension us = tensile strength oc = compressive strength uF = flexure strength P,,, = maximum tensile load applied at the loading holes 837 838 TAKESHI OCAWA et at.