A method is described for predicting barely visible impact damage in r
ealistic composite structures. It avoids a three-dimensional finite el
ement analysis by 'embedding' coupon tests as a calibrator in the fini
te element model of the larger actual structure. Predictions are then
made for all the dynamic responses including force and strain historie
s. A theoretical method is devised for predicting threshold fracture l
oads. This strategy is successfully validated by tests for carbon comp
osite structures, and then extended to glass and Kevlar laminated plat
es with varying degrees of success.