The damage and failure behaviour of the precipitation hardenable aluminium
wrought alloy AA7075 is studied in tension tests under quasi-static and dyn
amic loading conditions up to strain rates of (epsilon) over dot less than
or equal to 5500 s(-1). The results determined at room temperature are comp
ared with that received at an elevated temperature of 150 degreesC. Using d
ifferent heat treatment conditions the influence of size, volume fraction a
nd distribution of particles on the fracture strain can be determined. Expe
riments with unnotched tensile specimens allow the investigation of the mat
erial behaviour, which can be described by a constitutive model in case of
high speed deformation. In addition to the increased strain rate sensitivit
y and the adiabatic character of the deformation process with high strain r
ates, successive structural damage has to be taken into account for a formu
lation of the material law under tensile loading. Using differently notched
tension bars the state of stress is varied and the influence of multiaxial
ity on the elongation at fracture can be investigated. Combining experiment
s and finite element simulation the failure criterion for ductile fracture
will be formulated and the influence of an increased strain rate and temper
ature on the local plastic deformation at fracture as a function of degree
of multiaxiality can be determined. Applying the failure criterion the loca
tion of crack initiation in notched bars resulting in ductile fracture can
be determined.