The growth rate of fatigue cracks in two single crystal nickel base superalloys, CMSX-6 and SRR99, along the (001) planes are presented and rationalised in terms of two interacting crack propagation mechanisms: one attributed to crack tip plastic blunting and the other attributed to the brittle failure of the oxide scales. The role of the oxide scale is twofold as it also wedges the crack and modifies the blunting term through a crack closure effect. On the other hand, a positive effective stress intensity range is required to fracture the oxide scale. Fatigue tests were carried out at different temperatures (500 to lO5O0C), frequencies (0.001 to 20Hz), cycle waveforms and load ratios (0 to 0.9), with starter crack lengths of abut 100 pm. The model predictions match the crack growth rates obtained for both materials. Even though both materials are nickel base superalloys, they have very different oxidation behaviours. CMSX-6 has an improved oxidation resistance over SRR99, however, because of the twofold nature of the oxidation process, which material provides the better life expectancy depends on the applied test temperature and loading cycle. NOMENCLATURE a = size of the major defect in the oxide scale d = twice the compacted oxide scale thickness A, B, C, = constants (da/dN) = crack growth per cycle (da/dN),*, =fatigue component of crack growth per cycle (da/dN)oi&tion = oxidation component of crack growth per cycle (da/dN),,, = creep component of crack growth per cycle (da/dt),,,,, = oxidation crack growth rate Do = constant in oxide growth law e = oxide scale thickness E = Young's modulus f = cycle frequency K = stress intensity factor KCL = stress intensity factor at crack closure K E = oxide fracture toughness K-, K,, = maximum and minimum stress intensity factors n =hardening exponent no = constant in fatigue crack growth law n* =blunting coefficient Q = activation energy in oxide growth law R = minimum to maximum load ratio (also gas constant = 8.314 J/mol K) t = time = time to failure of the oxide scale t , = cycle period t* = estimate of tfd, T = absolute temperature a = constant in oxide growth law 6 = crack opening displacement 771 112 J. M. MART~NEZ-ESNAOLA et al. AK, AKeR = stress intensity factor range and effective stress intensity factor range v = Poisson's ratio rrWc = cyclic yield stress u,, = yield stress