In this paper a discrete-layer shear deformation laminated plate theor
y is used to analyse steady-state thermal stresses in laminated plates
. Both the in-plane displacements and the temperature rise are assumed
to be piecewise linear across the thickness. By the assumption that t
he transverse shear strains across any two layers are linearly depende
nt on each other, the theory contains the same dependent variables as
first-order shear deformation theory. The set of governing differentia
l equations is of the twelfth order which does not depend on the numbe
r of layers. No shear correction factors are required. The thermal ben
ding of simply supported, symmetric and antisymmetric cross-ply plates
is calculated. Numerical results of the present theory for thermal st
resses and deflections are compared with those obtained using the clas
sical, first-order and higher-order shear deformation plate theories.