The fracture and fatigue properties of a newly developed bulk metallic glas
s alloy, Zr41.2Ti13.8Cu12.5 Ni10Be22.5 (at, pct), have been examined. Exper
imental measurements using conventional fatigue precracked compact-tension
C(T) specimens (similar to 7-mm thick) indicated that the fully amorphous a
lloy has a plane-strain fracture toughness comparable to polycrystalline al
uminum alloys. However, significant variability was observed and possible s
ources are identified. The fracture surfaces exhibited a vein morphology ty
pical of metallic glasses, and, in some cases, evidence for local melting w
as observed. Attempts were made to rationalize the fracture toughness in te
rms of a previously developed micromechanical model based on the Taylor ins
tability, as well as on the observation of extensive crack branching and de
flection. Upon partial or complete crystallization, however, the alloy was
severely embrittled, with toughnesses dropping to similar to 1 MPa root m.
Commensurate with this drop in toughness was a marginal increase in hardnes
s and a reduction in ductility (as measured via depth-sensing indentation e
xperiments). Under cyclic loading, crack-propagation behavior in the amorph
ous structure was similar to that observed in polycrystalline steel and alu
minum alloys. Moreover, the crack-advance mechanism was associated with alt
ernating blunting and resharpening of the crack tip. This was evidenced by
striations on fatigue fracture surfaces. Conversely, the (unnotched) stress
/life (S/N) properties were markedly different. Crack initiation and subseq
uent growth occurred quite readily, due to the lack of microstructural barr
iers that would normally provide local crack-arrest points. This resulted i
n a low fatigue limit of similar to 4 pet of ultimate tensile strength.