Turning the free edge of an unstiffened flange inwards or outwards to
form a 'lip', can substantially improve the local buckling resistance
of a member. The lip is the most common type of edge stiffener used in
cold-rolled, thin-walled sections. In this paper the behaviour of pla
te elements of thin-walled sections stiffened by compound lips (i.e. l
ips which are folded twice to form 'lips on the lips) is examined both
theoretically and experimentally. An outline of a series of tests on
compound edge-stiffened thin-walled sections of various geometries is
given and some load-end compression displacement paths are compared wi
th the theoretical predictions. Reasonably good agreement is obtained
between the experimental and theoretical results. Comparisons of the t
heoretical predictions with experimental results of other researchers
are also presented in this paper.