To evaluate the inplane and antiplane T-stresses easily by a suitable appli
cation of the conservation integral without solving the boundary value prob
lem, the relation between the J-based mutual integral and the T-stresses is
derived explicitly for anisotropic bimaterial subject to inplane and antip
lane loading. The universal relation between the T-stresses of the specimen
s with and without a sandwiched layer is also derived and it holds true reg
ardless of the specimen size and loading condition if the layer thickness i
s sufficiently small. In order to show its usefulness, some basic problems
for interface crack including the interaction of an interface crack and a p
oint singularity are solved. In particular, a detailed computation is illus
trated for antiplane T-stress, in which the inplane and antiplane deformati
ons are decoupled. (C) 2001 Elsevier Science Ltd. All rights reserved.