Creep-fatigue interaction behaviour of a Nimonic PE-16 superalloy has been
studied in solution-annealed condition and two double-aged conditions (micr
ostructures with gamma' of 18nm and 35nm diameters) at 923 K. Tests were ca
rried out over various strain amplitudes with hold times of 1 and 10 min. d
uration introduced in peak tension and compression strain. The cyclic stres
s response of the alloy was characterized by an initial hardening, a soften
ing and a saturation regime. Further, at 923 K, the cyclic stress response
was found to increase with increase in the duration of the hold. Tension ho
ld was observed to be more damaging than compression hold, and the fatigue
life decreased with increase in the duration of the hold in tension. Accele
rated intergranular crack initiation and propagation reduced fatigue life u
nder hold times in tension. Moreover, oxidation was found to reduce fatigue
life under long hold periods.