Mechanical behaviour of cracked glass bridged by an elastomeric ligament is
central to properties of cracked glass/polymer laminates and other composi
tes. We present a theoretical and experimental study of a glass/polymer/gla
ss laminate with single aligned cracks in each glass plate, subjected to te
nsile loading. The test involves stable delamination at the interface betwe
en the polymer and substrate. The force required to maintain increasing str
ain rises to a steady state value. Crack propagation is accompanied by larg
e polymer deformation. The polymer has been modeled as an isothermal hypere
lastic material. Exact results in the limit of large crack extension relate
the steady-stare force to a measure of interfacial fracture energy and ela
stic material properties. These have been used to extract glass/polymer adh
esion from experimentally measured steady-state force. Force-displacement r
elationships have also been derived for the limiting case of small crack le
ngths. Together, the results represent a force-displacement model for a cra
cked glass/polymer laminate, which can be used to build models for multiply
cracked laminates. Finite element simulations of the experiment using cohe
sive elements to model the interface have been used to model the entire for
ce-displacement response. (C) 2000 Acta Metallurgica Inc. Published by Else
vier Science Ltd. All rights reserved.