Biaxial bending of panel components is a loading situation which exist
s in engineering structures. The behaviour of composite plates subject
ed to biaxial flexing has yet to be studied in detail. In the present
investigation, static and cyclic biaxial bending were applied to recta
ngular carbon-fibre/epoxy-resin simply-supported laminated plates with
three geometric aspect ratios. Series damage mechanism studies, mainl
y by NDT methods, and mechanical property evaluations were carried out
. It was found that various damage modes could occur below about 20% o
f the ultimate load/deflection levels. This damage, mainly matrix crac
ks and delamination, developed during fatigue. The amount of damage in
dicated by the area of the damage zone was mainly dependent on the len
d level, but not on the aspect ratios. Despite their low monotonic loa
d-bearing ability, plates with a higher aspect ratio could have a high
er resistance to biaxial bending fatigue.