Small explosive charges were placed on the surface or stood off from carbon
fibre and glass fibre laminates. Surface charges produced circular holes s
urrounded by a delaminated area. The holes increased in size with increased
explosive amount. For charges stood off the amount of damage was a functio
n of impulse as well as peak pressure. Damage associated with the attachmen
t of the laminate occurred at lower peak pressures (0.5 MPa) than previousl
y reported. The extent of damage was less for adhesively bonded laminates t
han for clamped laminates. Damage was in the form of fibre breakage as well
as interply delamination. (C) 1999 Elsevier Science Ltd. All rights reserv
ed.