An experimental technique for time-resolved characterization of the mechani
cal response and induced damage of fiber-reinforced composite laminates dur
ing low-velocity, transverse impact is presented. The configuration uses a
three-point bend fixture in a split Hopkinson pressure bar (SHPB) apparatus
for controlled loading and real-time diagnosis. The full histories of cont
act force, displacement and energy absorption of the specimen during impact
are measured. The materials analyzed are IM7/K3B, a graphite-fiber polyimi
de-matrix composite, and S2 glass/5250-4, a glass-fiber bismaleimide-matrix
composite. Experiments conducted characterize the responses of the materia
ls over a range of impact energy. The initial peak force sustained by the s
pecimen is found to be constant over the range of impact energy studied. A
monotonic relation is observed between the amount of energy absorbed by the
specimens and the post-impact tensile strength of the materials. For the s
ame amount of energy dissipated through damage, the glass fiber composite r
etains a higher percentage of its tensile strength than the graphite-fiber
composite. Postmortem X-ray radiography and ultrasonic tests are used to as
sess the extent and effects of damage. The mean square amplitude of the tra
nsverse vibratory response of an impacted specimen decreases with increasin
g impact-induced damage quantified in terms of dissipated energy. A similar
correlation is observed between the through-thickness wave speed of an imp
acted specimen and the dissipated energy.