An experimental study was carried out on woven fabric/epoxy composites
focusing on their mechanical properties under uniaxial tensile, flexu
ral, compressive, short beam shear and Mode I interlaminar fracture lo
ading conditions. Composites with fiber glass and Kevlar 49 woven fabr
ics and with different fabric constructions and microfiber additives w
ere investigated. The interlaminar fracture behavior was characterized
using double cantilever beam (DCB) test and the fracture mechanism wa
s analyzed by means of scanning electron microscopy (SEM). The mechani
cal properties were evaluated in uniaxial tension, three-point flexure
, compression and short beam shear. The effects of the reinforcing fab
ric structure and microfiber additives to the matrix on the mechanical
behavior and failure mechanisms of the composites were analyzed.