Effect of repeated impacts on the response of plain-woven hybrid composites

The repeated low-velocity impact responses of hybrid plain-woven composite panels were studied by drop-weight experiments. Non-hybrid S2-glass-fiber/toughened epoxy and IM7 graphite fiber/toughened epoxy as well as hybrid S2-glass–IM7 graphite fiber/toughened epoxy composite panels were impacted repeatedly using a pressure-assisted Instron-Dynatup 8520 instrumented drop-weight impact tester. During the low-velocity impact tests, the time histories of impact forces, absorbed impact energies and panel central deflections were recorded. The relations between the impact force and central deflection, whose slope represented the dynamic contact stiffness, were then constructed. The damaged specimens were inspected visually and using the ultrasonic C-Scan method. The effects of hybridization and lay-up sequence on the repeated drop-weight impact responses of woven composites were investigated. It was observed that damage accumulations could be slowed down using hybridization. It was also witnessed that the lay-up configuration of a hybrid composite had a significant influence on damage accumulation rate. The hybrid specimens with glass–epoxy skins survived the double number of successive impacts compared to hybrid specimens with graphite–epoxy skins.