The low cycle fatigue (LCF) behavior of two aluminum-lithium alloys wa
s investigated. Efforts were aimed at understanding the effects of mic
rostructure on the cyclic stress-strain behavior and methods by which
different microstructures accommodate plastic strain. These goals were
achieved by analyzing the cyclic response and the deformed microstruc
ture of each alloy. Direct-chill cast and rolled X2095 exhibited immed
iate cyclic softening followed by a plateau region. Strain was distrib
uted in a homogeneous manner throughout the microstructure. Mechanical
ly alloyed and forged AA5091 (formerly referred to as 905XL) also defo
rmed in a homogeneous manner, but the cyclic response was characterize
d by initial softening followed by gradual hardening. Over-strain loop
s were applied during some of the LCF tests, the purpose of which was
to simulate the strain history of the material ahead of a growing fati
gue crack during a tensile overload. The over-strain response suggeste
d that the intrinsic material response does not contribute to crack re
tardation in X2095 or AA5091.