Extensive and full range mechanical testing of 55Ni45Ti nitinol alloy
wire up to failure over a wide range of testing temperatures is report
ed. Thermomechanical properties are obtained including: initial modulu
s, secondary modulus, critical martensitic start and finish stresses,
plastic flow stress, recovery strain limit, failure stress and plastic
modulus. The data is correlated with the Brinson constitutive model m
odified to account for full range loading. The ratio of austenite to m
artensite moduli was found to be 5.8 and the secondary modulus (stress
-induced martensite) was found to be smaller by a factor of two when c
ompared to the modulus of (stress-free) thermally induced martensite.
The influence of the initial temperature treatment of the nitinol was
shown to be pronounced within the transformation range. Reasonably acc
urate correlation is obtained with the modified Brinson constitutive m
odel although there is some discrepancy in critical stress predictions
which is partially attributed to experimental scatter.