Detailed finite element calculations are carried out in order to study the
mechanical response of a compliant layer sandwiched between a rigid cylindr
ical Aat punch and a rigid substrate. Two cases of practical interest are c
onsidered: one in which the layer is perfectly bonded to the punch and the
substrate and one in which the interface between the punch and the layer is
frictionless. The substrate is assumed to be perfectly bonded to the adhes
ive layer in both cases. Analytic expressions are obtained for the stresses
away from the edges, and the effect of lateral constraint is examined. The
compliances of the loading systems for both cases are obtained numerically
, and accurate analytic expressions are determined based on these numeric r
esults. The nature of the stress fields near the contact edge are explored,
and their connections with the energy release rate are determined. The rel
evance of these calculations to two recent adhesion tests is discussed. (C)
2000 John Wiley & Sons, Inc.