The stress state found in a thin, power-law hardening ductile layer bo
nded between a pair of rigid adherends and subjected to a shear loadin
g is investigated. Within the context of a work-hardening plasticity t
heory, a stress singularity of type Kr(delta) (delta < 0) exists at th
e point where the interface between one of the rigid adherends and the
ductile layer intersects the stress-free edge. The intensity of this
singularity (i. e., K) has been calculated for a plane strain conditio
n using a technique that combines results of an asymptotic analysis of
the stress singularity with those of a detailed finite element analys
is. A dead-soft aluminum layer is considered first with emphasis place
d on an assessment of the region dominated by the plastic stress singu
larity. Results for a fully plastic layer with negligible elastic stra
ins are presented next. The relation defining the.fully plastic, free-
edge stress intensity factor for a shear loading depends only on a cha
racteristic shear stress, layer thickness, and the layer's hardening e
xponent.