Machine components normally experience fatigue cycling during operation. Fa
ilure of these components is mostly due. to fatigue. So, it is important to
know the fatigue damage behavior and fatigue life of the material before s
electing these steels for making different machine components. The En-8-gra
de (equivalent to SAE/AISI 1040) steel is generally used as a machine compo
nent in the annealed or hardened-and-tempered condition. The fatigue life (
fatigue/endurance limit) is also dependent upon the tensile properties of a
ny material. By suitable heat treatment, one can manipulate the tensile pro
perties of any steel. The present work reports the effect of fatigue damage
in En-8-grade heat-treated steel (annealed and hardened and tempered), und
er different cyclic loading conditions at room temperature (25 degreesC), o
n the impact and dynamic fracture-toughness properties. The results indicat
e higher fracture toughness and impact toughness in hardened-and-tempered s
teel than in annealed steel. Cyclic hardening and softening occurs in both
the hardened-and-tempered as well as the annealed steel. With the increase
of peak stress and number of fatigue cycles, the K-1D and CVN values decrea
se in hardened-and-tempered steels. The results are discussed in, terms of
dislocations, slip bands, and their density, microstructure, and fracture m
orphology.