The suitability of applying the overlapping grid method to parallel computa
tion of steady and unsteady compressible inviscid flows with three-point bl
ock-tridiagonal implicit schemes is addressed in this paper. An easily usab
le interface treatment is constructed and analyzed for both steady and unst
eady problems. The performance of the method, such as convergence rate and
time accuracy, can be controlled through the overlapping width. The method
needs no iteration at each time step or modification of the Thomas algorith
m for the solution of the implicit parts. In both steady and unsteady cases
a very good absolute parallel efficiency is demonstrated for bidimensional
subsonic and transonic flow computations. (C) 2000 Academic Press.