It is generally recognized that fiber-reinforced laminated composites
are susceptible to damage resulting from low-velocity impacts, Over re
cent years, many strategies have been devised to increase tile fractur
e toughness of resin matrix materials with the aim of improving the co
mposite's overall resistance to impact damage. One popular strategy fo
r enhancing the fracture toughness of thermosets involves increasing t
he molecular weight between crosslinks, which, in turn, enhances the r
esins ductility. in this paper, we investigate the efficiency of this
toughening approach with regard to resisting damage in composite lamin
ates subjected to low-velocity impacts. A mechanistic study shows that
at least two distinct processes occur during an impact event. First,
the laminate experiences a local failure, which resembles a Hertzian f
racture process followed by subsequent delamination between the plies,
Hertzian fracture occurs once ata critical threshold level initiates
laminate damage through the development of a spatially configured arra
y of matrix microcracks, which resemble that of a Hertzian cone togeth
er with radial cracks. Further damage accumulates in the laminate by i
nter-ply delamination with the size of delaminated area increasing coi
ncident with the impact load. Systematic changes in resin. crosslink d
ensity show that both damage initiation and accumulation are affected.
However, the maximum resistance far damage initiation occurs al a muc
h higher crosslink density than that measured for damage accumulation.