The high cycle fatigue (HCF) behavior of NiAl-0.28Fe (Ni-50.3 mol%Al-0
.28 mol%Fe) was determined at four temperatures between 673 K and 928
K, below and above its ductile to brittle transition temperature, DBTT
, (=730 K) obtained from tensile tests. Fracture and surface slip band
-characteristics were examined using an optical microscope and a scann
ing electron microscope. The fatigue resistance of NiAl-0.28Fe decreas
ed significantly with increasing temperature, due to a creep-fatigue i
nteraction above the DBTT. Below the DBTT cracks initiated at or near
the surface with fatigue zones and overload zones consisted of a mixtu
re of intergranular and transgranular fracture paths. Above the DBTT c
rack initiation occurred internally at or near microvoids (without obs
erved fatigue zones), leading to transgranular fracture paths. Cross s
lip and wavy slip were exhibited in tensile and HCF specimens below an
d above the DBTT. NiAl-0.28Fe displayed higher fatigue resistance than
Astroloy (powder metallurgy nickel-based superalloy) and Ni3Al+B in t
he range 673 K to 823 K.