The present study focuses on the determination of the buckling load and pos
t-buckling behaviour of simply supported laminated composite rectangular pa
nels loaded in shear. The nonlinear structural response is studied with a n
on-linear finite element approach. In order to determine the accuracy of th
e procedure, several tests have been performed comparing the finite element
solutions for isotropic and laminated composite rectangular panels with ex
isting ones, adopting different sequences of lamination and different lengt
h to width ratios. The analysis then considers the behaviour of laminates p
roduced with innovative thermoplastic matrix composites developed in the fr
ame of a national research program. (C) 1999 Elsevier Science Ltd. All righ
ts reserved.