The linear development of Gortler vortices in a curved compressible mi
xing layer is studied. It has been shown both experimentally and theor
etically that the curved mixing layer can support a centrifugal mode,
which is believed to be similar to the Gortler vortex mode. This study
follows the corresponding incompressible study of Otto, Jackson, and
Hu, and attempts to demonstrate the effects compressibility has on the
growth of such modes [J. Fluid Mech. 315, 85 (1996)]. The ultimate do
wnstream fate of the modes is studied in the high Taylor/Gortler numbe
r regime. The problem of the third boundary condition inherent to the
mixing layer model is addressed using the set of boundary conditions f
or both subsonic and supersonic flows derived by Ting [J. Math. Phys.
28, 153 (1959)]. A class of modes is discussed that have no counterpar
t in the uniform temperature incompressible case. (C) 1997 American In
stitute of Physics.