The mechanical behaviour of AISI 329 steel has been investigated for ageing times up to 20,000 h at temperatures of 475,425, 375, 325 and 275°C. The study has concentrated on the changes in the response to cyclic strains, in the low-and the high-cycle fatigue regimes, and in the resistance to fatigue crack propagation as a function of temperature and time of ageing.It is shown that ageing increases the fatigue resistance in the high-cycle fatigue regime, but the opposite occurs in the low-cycle fatigue regime. Ageing increases the LEFM threshold stress intensity factor range for fatigue crack propagation which reaches high values in these alloys, and is influenced by the fatigue load ratio. Crack closure contributes to the LEFM threshold stress intensity factor range for crack propagation only in the annealed condition of the AISI 329 steel. NOMENCLATURE a = crack length b, c = fatigue strength and ductility exponent, respectively K,, = closure stress intensity factor N , = number of cycles to failure A& = crack tip opening displacement E, E' = Young's modulus and Young's modulus in plane strane, respectively /? = constant
AK,= stress and effective stress intensity factor ranges, respectively AK,,, = threshold stress intensity factor range Acr = stress range E; = fatigue ductility coefficient of = fatigue limit u; = fatigue strength coefficient by, cr; = yield stress and cyclic yield strength, respectively