The effect of thermal loads on imperfectly bonded laminated composite shell
s is studied. The interfacial imperfections necessitate that conditions req
uiring the continuity of surface tractions and displacements between adjoin
ing faces be suitably modified, and interfacial damage properly accounted f
or. Both mechanical and thermal interfacial imperfections are characterized
by interfacial parameters in the non-lineal equations of motions. Results
are presented for two static linear problems. (C) 2001 Elsevier Science Ltd
. All rights reserved.