Impact loading of three point bend specimens is modeled as a lumped ma
ss-spring system with two degrees of freedom. The model gives all the
forces involved in the impact process, viz. load measured by the tup i
nstrumentation, contact force and the force experienced by the specime
n. With a simplifying assumption of applicability of static crack-tip
field solutions, the dynamic stress intensity factor (SIF) is computed
from the beam force. Dynamic fracture toughness is obtained from the
SIF at fracture initiation. The model explains the typical features of
tup load and beam response records observed in instrumented Charpy te
sting. The model predictions are compared with results of experiments
conducted on aluminum 6061 T6 and polymethylmethacrylate (PMMA).